Multiple anchor delivery tool

Description of equivalent WO 2012014201 A2

MULTIPLE ANCHOR DELIVERY TOOL

CROSS-REFERENCES TO RELATED APPLICATIONS

0003The present application claims the priority of and is a continuation-in-part of US Patent Application 12/843,412 to Cabiri et al., entitled, "Multiple anchor delivery tool" filed on July 26, 2010 which is incorporated herein by reference.

FIELD OF THE APPLICATION

0005Some embodiments of the present invention relate in general to surgical tools, and more specifically to surgical tools for delivering tissue anchors.

BACKGROUND OF THE APPLICATION

0007Ischemic heart disease causes mitral regurgitation by the combination of ischemic dysfunction of the papillary muscles, and the dilatation of the left ventricle that is present in ischemic heart disease, with the subsequent displacement of the papillary muscles and the dilatation of the mitral valve annulus. Dilation of the annulus of the mitral valve prevents the valve leaflets from fully coapting when the valve is closed. Mitral regurgitation of blood from the left ventricle into the left atrium results in increased total stroke volume and decreased cardiac output, and ultimate weakening of the left ventricle secondary to a volume overload and a pressure overload of the left atrium.

SUMMARY OF THE APPLICATION

0009In some embodiments of the present invention, a tissue anchor deployment system comprises an anchor deployment tool and a plurality of tissue anchors. The anchor deployment tool comprises a flexible outer tube, a flexible inner shaft, which is positioned within the flexible outer tube, and a rotating deployment element, which is coupled to the distal end of the shaft. The anchor deployment tool is configured to provide an anchor storage area. The storage area initially stores the plurality of tissue anchors, such that the flexible inner shaft passes through channels that pass through each of the anchors, and the anchors are within the flexible outer tube. The rotating deployment element is configured to directly engage the anchors in the anchor storage area one at a time, advance each of the anchors while engaged in a distal direction, and deploy each of the anchors through the distal end of the outer tube and into tissue of a subject. Typically, the anchor deployment tool is configured to provide steering functionality to a distal anchor manipulation area of the anchor deployment tool between the anchor storage area and the distal tube end.

0010For some applications, the anchor deployment tool is configured such that, as the rotating deployment element advances each of the anchors in the distal direction, only the single anchor currently being advanced is within the distal anchor manipulation area of the anchor deployment tool. For some applications, the anchor deployment tool is configured to deploy each of the anchors into the tissue in a direction parallel to a central longitudinal axis of the outer tube through the distal tube end, and parallel to a central longitudinal axis of the anchor.

0011For some applications, the rotating deployment element is configured to pass through one or more of the anchors without engaging the anchors when the rotating deployment element is withdrawn in a proximal direction within the outer tube, and to directly engage one of the anchors when the rotating deployment element is advanced in the distal direction against the one of the anchors. Typically, the rotating deployment element is configured to assume a radially-compressed state when passing through the one or more of the anchors without engaging the anchors, and to assume a radially-expanded state when engaging the one of the anchors.

0012For some applications, the anchor deployment tool further comprises an anchor restraining mechanism in a vicinity of the distal anchor storage end. The mechanism is configured to temporarily restrain at least the distal-most anchor currently stored in the anchor storage area from advancing in the distal direction.

0013For some applications, each of the anchors comprises a helical tissue coupling element, and a tool-engaging head, fixed to one end of the tissue coupling element. The tool-engaging head is shaped so as to define an engaging opening that is at least partially non-circular, and that passes entirely through the tool-engaging head along the axis. The end of the tissue coupling element is fixed to the tool-engaging head near an outer perimeter of the tool-engaging head, such that the tissue coupling element does not block the engaging opening. The tissue coupling element and the tool-engaging head together define a channel along an entire length of the tissue anchor, which channel is sized and shaped such that a right circular cylinder could be placed within the channel, coaxial with the tissue anchor, and along the entire length of the tissue anchor. The cylinder typically has a diameter of at least 1 mm, such as at least 2 mm.

0014For some applications, the rotating deployment element is capable of unscrewing an already-deployed anchor from the tissue, withdrawing the anchor in a proximal direction, and subsequently redeploying the anchor into the tissue. For some applications, to enable such redeployment, the rotating deployment element is configured to selectively assume (a) a locked state, in which the rotating deployment element engages one of the anchors, such that the rotating deployment element can withdraw the anchor in the proximal direction, and (b) an unlocked state, in which the rotating deployment element does not engage the anchor.

0015For some applications, the anchor deployment system is used to deploy anchors for coupling an annuloplasty ring to tissue of a native cardiac valve of the subject, such as a mitral valve. For example, the annuloplasty ring may comprise a sleeve having a lumen, and the anchor deployment tool may be configured to be removably positioned within the lumen of the sleeve, and, while so positioned, to deploy the anchors from the distal tube end through a wall of the sleeve into the tissue. Alternatively applications for the anchor deployment system include delivery of anchors via a working channel of an endoscope, such as to mount and secure a support mesh for treating a hernia.

0016There is therefore provided, in accordance with an application of the present invention, apparatus including:

0017a plurality of tissue anchors, which are shaped so as to define respective channels along entire longitudinal lengths of the anchors; and

0018an anchor deployment tool, which includes:

0019a flexible outer tube, which has a distal tube end;

0020a flexible inner shaft, which is positioned within the flexible outer tube, and has a distal shaft end; and

0021a rotating deployment element, which is coupled to the distal shaft end,

0022wherein the anchor deployment tool is configured to provide an anchor storage area, having a distal anchor storage area end, the anchor storage area being configured to initially store the plurality of tissue anchors, such that the flexible inner shaft passes through the channels of the anchors, and the anchors are within the flexible outer tube, and

0023wherein the rotating deployment element is configured to directly engage the anchors in the anchor storage area one at a time, advance each of the anchors while engaged in a distal direction, and deploy each of the anchors through the distal tube end and into tissue of a subject.

0024Typically, the anchor deployment tool is configured such that, as the rotating deployment element advances each of the anchors in the distal direction, only the single anchor currently being advanced is within a distal anchor manipulation area of the anchor deployment tool between the distal anchor storage area end and the distal tube end.

0025For some applications, the anchor deployment tool is configured to deploy each of the anchors into the tissue in a direction parallel to a central longitudinal axis of the outer tube through the distal tube end, and parallel to a central longitudinal axis of the anchor.

0026For some applications, the anchor storage area has a distal anchor storage end at a distance of between 1 and 90 cm from the distal tube end, such as between 5 and 25 cm.

0027For some applications, the anchor deployment tool is configured to provide steering functionality to a distal anchor manipulation area of the anchor deployment tool between the distal anchor storage area end and the distal tube end. For some applications, the flexible outer tube is configured to provide the steering functionality to the distal anchor manipulation area. Alternatively or additionally, the flexible inner shaft is configured to provide the steering functionality to the distal anchor manipulation area.

0028For some applications, the rotating deployment element is configured to pass through one or more of the anchors without engaging the anchors when the rotating deployment element is withdrawn in a proximal direction within the outer tube, and to directly engage one of the anchors when the rotating deployment element is advanced in the distal direction against the one of the anchors. Typically, the rotating deployment element is configured to assume a radially-compressed state when passing through the one or more of the anchors without engaging the anchors, and to assume a radially-expanded state when engaging the one of the anchors.

0029For some applications, the anchor deployment tool further includes a spring, which is arranged to apply a distally-directed force to a proximal-most one of the anchors stored within the anchor storage area, which force advances the anchors remaining in the anchor storage area in the distal direction, when the rotating deployment element advances a distal-most one of the anchors out of the anchor storage area in the distal direction. Alternatively, for some applications, the anchor storage area is configured to provide a plurality of anchor storage locations, the anchors are initially stored in respective ones of at least a portion of the anchor storage locations, and when the rotating deployment element advances a distal-most one of the anchors out of the anchor storage area in the distal direction, the anchors remaining in the anchor storage area remain in their respective initial anchor storage locations.

0030For some applications, the plurality of anchors includes at least 6 anchors.

0031For some applications, the anchor deployment tool further includes an anchor restraining mechanism in a vicinity of the distal end of the anchor storage area, which mechanism is configured to temporarily restrain at least a distal-most one of the anchors currently stored in the anchor storage area from advancing in the distal direction.

0032For some applications, each of the anchors has a central longitudinal axis, and includes:

0033a helical tissue coupling element, having proximal and distal ends; and a tool-engaging head, fixed to the proximal end of the tissue coupling element, which tool-engaging head is shaped so as to define a non-circular engaging opening that passes entirely through the tool-engaging head along the axis,

0034wherein the tissue coupling element and the tool-engaging head together define the channel of the tissue anchor along an entire length of the tissue anchor, which channel is sized and shaped such that a right circular cylinder could be placed within the channel, coaxial with the tissue anchor, and along the entire length of the tissue anchor, and wherein the rotating deployment element of the anchor deployment tool is configured to removably engage the tool-engaging head.

0035For some applications, the cylinder has a diameter of at least 1 mm, such as at least 2 mm.

0036For some applications, the apparatus further includes an annuloplasty ring, which includes a sleeve having a lumen, and the anchor deployment tool is configured to be removably positioned within the lumen of the sleeve, and, while so positioned, to deploy the anchors from the distal tube end through a wall of the sleeve into the tissue.

0037For some applications, the distance between the distal anchor storage end and the distal tube end is between 5 and 25 cm.

0038For some applications, the anchor deployment tool further includes a hemostasis valve, which includes a distal port to which a proximal end of the flexible outer tube is sealingly coupled. The flexible inner shaft passes through the valve, which maintains a seal around the inner shaft, while allowing the inner shaft to slide distally and proximally through the valve.

0039For some applications, the rotating deployment element is capable of unscrewing an already-deployed one of the anchors from the tissue, withdrawing the anchor in a proximal direction, and subsequently redeploying the anchor into the tissue.

0040For some applications, the rotating deployment element includes a locking mechanism that is configured to selectively assume (a) a locked state, in which the locking mechanism, even upon withdrawal of the rotating deployment element in a proximal direction, prevents disengagement of the rotating deployment element from one of the anchors which the rotating deployment element engages, and (b) an unlocked state, in which the locking mechanism does not prevent disengagement of the rotating deployment element from the anchor upon the withdrawal of the rotating deployment element in the proximal direction.

0041There is further provided, in accordance with an application of the present invention, apparatus including a tissue anchor, which has a central longitudinal axis, and which includes: a helical tissue coupling element, having proximal and distal ends; and a tool-engaging head, fixed to the proximal end of the tissue coupling element, which tool-engaging head is shaped so as to define a non-circular engaging opening that passes entirely through the tool-engaging head along the axis,

0042wherein the tissue coupling element and the tool-engaging head together define a channel along an entire length of the tissue anchor, which channel is sized and shaped such that a right circular cylinder could be placed within the channel, coaxial with the tissue anchor, and along the entire length of the tissue anchor.

0043For some applications, the cylinder has a diameter of at least 1 mm, such as at least 2 mm.

0044For some applications, the proximal end of the tissue coupling element is fixed to the tool-engaging head near an outer perimeter of the tool-engaging head, such that the tissue coupling element does not block the engaging opening. For some applications, a distance between (a) a center of the proximal end of the tissue coupling element and (b) the outer perimeter of the tool-engaging head is no more than 30% of a width of the tool-engaging head.

0045For some applications, a portion of the helical tissue coupling element, at the proximal end which is fixed to the tool-engaging head, is generally straight and oriented at angle of between 0 and 15 degrees with the central longitudinal axis. There is still further provided, in accordance with an application of the present invention, apparatus including:

0046at least one tissue anchor; and

0047an anchor deployment tool including a deployment element, which is:

0048configured to directly engage the at least one anchor and advance the anchor while engaged in a distal direction, and deploy the anchor into tissue of a subject, and

0049capable of disengaging the already-deployed anchor from the tissue, withdrawing the anchor in a proximal direction, and subsequently redeploying the anchor into the tissue.

0050For some applications, the at least one tissue anchor includes a plurality of tissue anchors, and the anchor deployment tool is configured provide an anchor storage area having a distal anchor storage area end, the anchor storage area being configured to initially store the plurality of tissue anchors.

0051For some applications:

0052the anchor deployment tool includes a flexible outer tube which has a distal tube end,

0053the anchor storage area is disposed within the flexible outer tube,

0054the deployment element is slidably advanceable within a lumen of the flexible outer tube and through the anchor storage area, and

0055the anchor deployment tool is shaped so as to provide a distal anchor manipulation area between the distal anchor storage area end and the distal tube end.

0056For some applications, each one of the plurality of anchors is shaped so as to define respective channels along entire longitudinal lengths of the anchors, and the deployment element includes a flexible shaft which passes through the channels of the anchors.

0057For some applications, the deployment element is configured to directly engage the anchors in the anchor storage area one at a time, advance each one of the anchors while engaged in a distal direction, and deploy each one of the anchors through the distal tube end and into tissue of the subject.

0058For some applications, the deployment element includes a rotating deployment element.

0059For some applications, the rotating deployment element is ( 1 ) configured to deploy the at least one anchor into the tissue of the subject by screwing the anchor into the tissue, and (2) capable of unscrewing the already-deployed anchor from the tissue.

0060For some applications, the at least one anchor includes at least one helical anchor and the rotating deployment element is configured to screw the helical anchor into the tissue.

0061For some applications, the deployment element includes a locking mechanism that is configured to selectively assume (a) a locked state, in which the locking mechanism, even upon withdrawal of the deployment element in the proximal direction, prevents disengagement of the deployment element from the at least one anchor which the deployment element engages, and (b) an unlocked state, in which the locking mechanism does not prevent disengagement of the deployment element from the anchor upon the withdrawal of the deployment element in the proximal direction.

0062For some applications, the deployment element includes two or more radially- expandable engagement elements configured to, in a radially-expanded state thereof, engage the anchor, and the locking mechanism includes a pin configured in the locked state to maintain the engagement elements in the radially-expanded state.

0063For some applications, the anchor includes a tool-engaging head having an engaging surface defining an opening configured for receiving the two or more radially-expandable engagement elements, and the two or more radially-expandable engagement elements are configured to engage the engaging surface of the anchor in the radially-expanded state.

0064For some applications, the two or more radially-expandable engagement elements are configured to, in a radially-compressed state thereof, disengage the anchor.

0065For some applications, the pin is advanceable between the two or more radially-expandable engagement elements, and the pin is configured to maintain the two or more radially-expandable engagement elements in their radially-expanded state when disposed between the two or more radially-expandable engagement elements.

0066For some applications, the pin is removable from between the two or more radially-expandable engagement elements in order to allow the two or more radially- expandable engagement elements to assume the radially-compressed state. There is further provided, in accordance with some applications of the present invention, the following inventive concepts:

00671. A method including:

0068providing an anchor deployment tool, which includes a flexible outer tube, a flexible inner shaft, which is positioned within the flexible outer tube, and a rotating deployment element, which is coupled to a distal shaft end of the flexible inner shaft; providing a plurality of tissue anchors, which are shaped so as to define respective channels along entire longitudinal lengths of the anchors, and which are initially stored within an anchor storage area provided by the anchor deployment tool, such that the flexible inner shaft passes through the channels of the anchors, and the anchors are within the flexible outer tube; and

0069using the rotating deployment element, directly engaging the anchors in the anchor storage area one at a time, advancing each of the anchors while engaged in a distal direction, and deploying each of the anchors through the distal tube end and into tissue of a subject.

00702. The method according to inventive concept 1 , wherein advancing each of the anchors includes advancing each of the anchors in the distal direction such that only the single anchor currently being advanced is within a distal anchor manipulation area of the anchor deployment tool between the distal anchor storage area end and the distal tube end.

00713. The method according to inventive concept 1 , wherein deploying includes deploying each of the anchors into the tissue in a direction parallel to a central longitudinal axis of the outer tube through the distal tube end, and parallel to a central longitudinal axis of the anchor.

00724. The method according to inventive concept 1 , wherein deploying includes steering a distal anchor manipulation area of the anchor deployment tool between the distal anchor storage area end and the distal tube end.

00735. The method according to any one of inventive concepts 1 -4, wherein directly engaging, advancing, and deploying the anchors includes:

0074directly engaging, advancing, and deploying a first one of the anchors into the tissue at a first site; and

0075thereafter, directly engaging, advancing, and deploying a second one of the anchors into the tissue at a second site, different from the first site.

00766. The method according to inventive concept 5, wherein directly engaging the second anchor includes: withdrawing the rotating deployment element in a proximal direction within the outer tube, such that the rotating deployment element passes through one or more of the anchors without engaging the anchors; and

0077directly engaging the second anchor by advancing the rotating deployment element in the distal direction against the second anchor.

00787. The method according to any one of inventive concepts 1-4, wherein withdrawing includes withdrawing the rotating deployment element such that the rotating deployment element assumes a radially-compressed state when passing through the one or more of the anchors without engaging the anchors, and wherein engaging includes engaging the second anchor when the rotating deployment element assumes a radially-expanded state.

00798. The method according to any one of inventive concepts 1 -4, wherein providing the plurality of anchors includes providing at least 6 anchors.

00809. The method according to any one of inventive concepts 1 -4, wherein deploying includes deploying each of the anchors into cardiac tissue of the subject.

008110. The method according to inventive concept 9, wherein deploying includes removably positioning the anchor deployment tool within a lumen of a sleeve of an annuloplasty ring, and, while so positioned, to deploying the anchors from the distal tube end through a wall of the sleeve into the tissue.

00821 1 . The method according to any one of inventive concepts 1 -4, wherein providing the anchor deployment tool includes providing the anchor deployment tool in which the anchor storage area has a distal anchor storage end at a distance of between 1 and 90 cm from the distal tube end.

008312. The method according to inventive concept 1 1 , wherein providing the anchor deployment tool includes providing the anchor deployment tool in which the distance between the distal anchor storage end and the distal tube end is between 5 and 25 cm.

008413. The method according to any one of inventive concepts 1 -4, further including, using the rotating deployment element, unscrewing an already-deployed one of the anchors from the tissue, withdrawing the anchor in a proximal direction, and subsequently redeploying the anchor into the tissue.

008514. The method according to inventive concept 13,

0086I 1 wherein the rotating deployment element includes a locking mechanism that is configured to selectively assume a locked state, in which the locking mechanism, even upon withdrawal of the rotating deployment element in the proximal direction, prevents disengagement of the rotating deployment element from the anchor,

0087wherein the method further includes causing the locking mechanism to assume the locked state, and

0088wherein withdrawing the anchor includes withdrawing the anchor in the proximal direction while the rotating deployment element is in the locked state.

008915. A method including:

0090providing a tissue anchor, which has a central longitudinal axis, and which includes a helical tissue coupling element having proximal and distal ends, and a tool engaging head, fixed to the proximal end of the tissue coupling element, which tool- engaging head is shaped so as to define a non-circular engaging opening that passes entirely through the tool-engaging head along the axis, wherein the tissue coupling element and the tool-engaging head together define a channel along an entire length of the tissue anchor, which channel is sized and shaped such that a right circular cylinder could be placed within the channel, coaxial with the tissue anchor, and along the entire length of the tissue anchor; and

0091coupling the tissue anchor to tissue of a subject, by rotating the tissue coupling element into the tissue.

009216. The method according to inventive concept 1 , wherein a distance between (a) a center of the proximal end of the tissue coupling element and (b) an outer perimeter of the tool-engaging head is no more than 30% of a width of the tool-engaging head, and wherein coupling includes:

0093coupling a sheet to the tissue using the tissue anchor;

0094sensing increased resistance to rotation of the tissue coupling element when the sheet resists the rotation; and

0095responsively the sensed increased resistance, ceasing rotating the tissue coupling element into the tissue. 17. A method including:

0096providing at least one anchor; providing an anchor deployment tool having a deployment element, using the deployment element, directly engaging the at least one anchor, advancing the anchor while engaged in a distal direction, and deploying the anchor into tissue of a subject; and

0097subsequently, using the deployment element, disengaging the already- deployed anchor from the tissue, withdrawing the anchor in a proximal direction, and subsequently redeploying the anchor into the tissue.

009818. The method according to inventive concept 17, wherein providing the at least one anchor includes providing a plurality of anchors and wherein providing the anchor deployment tool includes providing an anchor storage area having a distal anchor storage area; and

0099wherein the method further includes initially storing the plurality of tissue anchors in the anchor storage area.

010019. The method according to inventive concept 18, wherein:

0101providing the anchor deployment tool includes providing the anchor deployment tool having a flexible outer tube which has a distal tube end, and the anchor storage area is disposed within the flexible outer tube,

0102the method further includes:

0103slidably advancing the deployment element within a lumen of the flexible outer tube and through the anchor storage area, and

0104providing a distal anchor manipulation area in the anchor deployment tool which is between the distal anchor storage area end and the distal tube end.

010520. The method according to inventive concept 19, wherein:

0106each one of the plurality of anchors is shaped so as to define a respective channel along an entire longitudinal length of the anchor, and

0107the deployment element includes a flexible shaft; and

0108the method further includes passing the a flexible shaft through the channels of the anchors.

010921 . The method according to inventive concept 19,wherein engaging the at least one anchor includes directly engaging the anchors in the anchor storage area one at a time, advancing the anchor while engaged in a distal direction, and deploying the anchor through the distal tube end into tissue of a subject.

011022. The method according to inventive concept 17, wherein providing the anchor deployment tool having the deployment element includes providing the anchor deployment tool having a rotating deployment element.

011123. The method according to inventive concept 22, wherein using the deployment element includes rotating the rotating deployment element to deploy the anchor into the tissue of the subject by screwing the anchor into the tissue, and subsequently unscrewing the already-deployed anchor from the tissue.

011224. The method according to inventive concept 23, wherein the at least one anchor includes at least one helical anchor and wherein rotating the deployment element includes screwing the helical anchor into the tissue.

011325. The method according to inventive concept 17,

0114wherein the deployment element includes a locking mechanism that is configured to selectively assume a locked state, in which the locking mechanism, even upon withdrawal of the deployment element in the proximal direction, prevents disengagement of the deployment element from the anchor,

0115wherein the method further includes causing the locking mechanism to assume the locked state, and

0116wherein withdrawing the anchor includes withdrawing the anchor in the proximal direction while the deployment element is in the locked state.

011726. The method according to inventive concept 25,

0118wherein the deployment element includes two or more radially-expandable engagement elements configured to, in a radially-expanded state thereof, engage the anchor,

0119wherein the locking mechanism includes a pin, and

0120wherein causing the locking mechanism to assume the locked state includes using the pin to maintain the engagement elements in the radially-expanded state. 27. The method according to inventive concept 26,

0121wherein the at least one anchor includes a tool-engaging head having an engaging surface defining an opening configured for receiving the two or more radially-expandable engagement elements, and

0122wherein engaging the at least one anchor includes engaging the engaging surface of the anchor by facilitating maintaining of the two or more radially- expandable engagement elements in the radially-expanded state thereof by positioning the pin between the two or more radially-expandable engagement elements.

012328. The method according to inventive concept 27, wherein disengaging the already-deployed anchor includes disengaging the anchor by facilitating radial compression of the two or more radially-expandable engagement elements from the radially-expanded state thereof by removing

0124the pin from between the two or more radially-expandable engagement elements in order to allow the two or more radially-expandable engagement elements to assume the radially-compressed state.

0125The present invention will be more fully understood from the following detailed description of embodiments thereof, taken together with the drawings, in which:

BRIEF DESCRIPTION OF THE DRAWINGS

0127Figs. I A-B are schematic illustrations of an anchor deployment system, in accordance with an application of the present invention;

0128Figs. 2 and 3A-B are schematic illustrations showing the assembly of components of the anchor deployment system of Figs. 1A-B, in accordance with an application of the present invention;

0129Figs. 4A-D are schematic illustrations of the deployment of a single anchor into tissue using an anchor deployment tool of the anchor deployment system of Figs. 1A-B, in accordance with an application of the present invention;

0130Figs. 5A-B are schematic illustrations of an alternative configuration of the anchor deployment system of Figs. 1A-B, in accordance with an application of the present invention; Figs. 6A-C are schematic illustrations of an anchor of the anchor deployment system of Figs. 1 A-B from three different views, in accordance with an application of the present invention;

0131Figs. 7A and 7B are schematic illustrations of a rotating deployment element of the anchor deployment system of Figs. 1A-B in radially-expanded and radially- compressed states, respectively, in accordance with an application of the present invention;

0132Figs. 8A and 8B are schematic illustrations of the rotating deployment element of Figs. 7A-B engaging a tool-engaging head of the anchor of Figs. 6A-C, with the element in locked and unlocked states, respectively, in accordance with an application of the present invention;

0133Figs. 9A-I are schematic illustrations of a procedure for implanting an annuloplasty ring to repair a mitral valve, in accordance with an application of the present invention; and

0134Fig. 10 is a schematic illustration of a procedure for implanting an annuloplasty ring to repair a tricuspid valve, in accordance with an application of the present invention.

DETAILED DESCRIPTION OF APPLICATIONS

0136Figs. 1 A-B are schematic illustrations of an anchor deployment system 20, in accordance with an application of the present invention. Anchor deployment system 20 comprises an anchor deployment tool 30, which is configured to deliver a plurality of anchors 32 to respective sites within a body of a subject, and to couple the anchors to tissue at the sites. For some applications, tool 30 is configured to deploy anchors 32 to cardiac sites within the heart, such as in a vicinity of a valve annulus. Tool 30 comprises a flexible outer tube 34, within which is positioned a flexible inner shaft 36. Tool 30 further comprises a rotating deployment element 38, coupled to a distal shaft end 39 of inner shaft 36.

0137As shown in Fig. 1 A, tool 30 (e.g., flexible outer tube 34) is configured to provide an anchor storage area 40, which is configured to initially store the plurality of anchors 32. The anchors are positioned within outer tube 34 such that inner shaft 36 passes through respective longitudinal channels of the anchors, as described hereinbelow with reference to Figs. 6A-C. A distal anchor storage end 41 of anchor storage area 40 is typically at distance of at least 1 cm from a distal tube end 42 of outer tube 34, such as at least 3 cm or at least 5 cm, to enable flexibility and manipulation of the tool end. Distal anchor storage end 41 is typically at a distance of no more than 90 cm from distal tube end 42, such as no more than 25 cm, to maintain the comfort and stability level of the user. For some applications, distal anchor storage end 41 is at a distance of between 3 cm and 25 cm from distal tube end 42, such as between 5 cm and 25 cm. Tool 30 typically comprises a spring 44, which is arranged to apply a distally-directed force to the proximal-most anchor within anchor storage area 40, thereby holding the anchors within the storage area, and advancing the remaining anchors distal ly as each of the anchors is separately deployed.

0138The portion of tool 30 between distal anchor storage area end 41 and distal tube end 42 of outer tube 34 serves as a distal anchor manipulation area 50 of tool 30. Anchor manipulation area 50 is typically flexible and steerable. Typically, only one anchor at a time is deployed through anchor manipulation area 50 and into the tissue of the subject, such that no more than exactly one anchor is within anchor manipulation area 50 at any given time. As a result, anchor manipulation area 50 retains its flexibility. Because the anchors are typically rigid, when more than one of the anchors are longitudinally contiguously positioned within tool 30, the area of the tool in which the anchors are positioned becomes fairly stiff, substantially losing the flexibility it would otherwise have. Thus, while anchor storage area 40 is fairly rigid, anchor manipulation area 50 remains flexible because it only contains exactly one anchor at a given time. The stiffness of the area of the tool in which the anchors are positioned also may enable the user to better control the exact location of distal-most anchor 32 currently stored in anchor storage area 40.

0139The steering functionality of distal anchor manipulation area 50 typically allows the area near the distal end of tool 30 to be positioned with six degrees of freedom. For some applications, flexible outer tube 34 is configured to provide the steering functionality to distal anchor manipulation area 50. Flexible outer tube 34 comprises one or more steering wires, the pulling and releasing of which cause deflection of distal tube end 42, using deflection techniques known in the catheter art. Alternatively or additionally, flexible inner shaft 36 is configured to provide the steering functionality to distal anchor manipulation area 50. Flexible inner shaft 36 comprises one or more steering wires for deflecting the distal end of the inner shaft. Still further alternatively or additionally, a separate flexible tube is provided for providing the steering functionality. The separate tube is positioned within flexible outer tube 34 or around the outer tube, and comprises one or more steering wires for deflecting the distal end of the inner shaft. The curvature of the tool may be pre- shaped, or bendable by application of an external force (such as a conventional colonoscope) or using an internal or external wire (configuration not shown). For some applications, the steering functionality is provided by a combination of more than one of flexible outer tube 34, flexible inner shaft 36, and the separate flexible tube, e.g., by (a) flexible outer tube 34 and flexible inner shaft 36, (b) flexible outer tube 34 and the separate flexible tube, (c) flexible inner shaft 36 and the separate flexible tube, or (d) all of flexible outer tube 34, flexible inner shaft 36, and the separate flexible tube.

0140For some applications, an external control handle is provided for controlling tool 30. The control handle comprises circuitry for manipulating the steering wires to provide the steering functionality.

0141For some applications, flexible inner shaft 36 comprises stainless steel SS 304, itinol, PEEK®, polyester, or another polymer. For some applications, outer tube 34 comprises stainless steel SS 304, Nitinol, PEEK®, polyester, or another polymer. For some applications, flexible inner shaft 36 has a diameter of at least 0.8 mm, no more than 3 mm, and/or between 0.8 and 3 mm, such as between 1 and 2 mm. For some applications, outer tube 34 has an outer diameter of at least 2 mm, no more than 4 mm, and/or between 2 and 4 mm, e.g., 3 mm or 3.2 mm. For some applications, outer tube 34 has an inner diameter of at least 1.5 mm, no more than 3.5 mm, and/or between 1.5 and 3.5 mm, e.g., 2.6 mm.

0142For some applications, anchor deployment tool 30 further comprises a hemostasis valve 80, as shown in Fig. IB. Hemostasis valve 80 minimizes leakage of blood, and entrance of air (thereby reducing the risk of air emboli), during a percutaneous procedure performed using system 20. A proximal end of flexible outer tube 34 is sealingly coupled to a distal port of valve 80. Inner shaft 36 passes through valve 80, which maintains a seal around the inner shaft, while allowing the inner shaft to slide distally and proximally through the valve during deployment of anchors 32, as described hereinbelow with reference to Figs. 4A-D. Valve 80 optionally comprises a side port 82 for flushing the system, as is known in the hemostasis valve art. For other applications, the anchor deployment tool does not comprise the hemostasis valve.

0143Reference is made to Figs. 2 and 3A-B, which are schematic illustrations showing the assembly of components of anchor deployment system 20, in accordance with an application of the present invention. Typically, spring 44 is positioned around a proximal portion of flexible inner shaft 36. A distal end 58 of the spring applies a force in a distal direction against the proximal end of the proximal-most anchor 32 (right-most in the figures) stored in anchor storage area 40. The plurality of anchors 32 are initially positioned end-to-end longitudinally contiguously around flexible inner shaft 36 within anchor storage area 40. By way of example, Fig. 2 shows five anchors 32. Typically, system 20 is configured to store between 6 and 20 anchors 32, such as between 8 and 16 anchors 32.

0144As shown in the blow-up of Fig. 2, and described in more detail hereinbelow with reference to Figs. 6A-C, each of anchors 32 comprises a helical tissue coupling element 60, and a tool-engaging head 62, fixed to one end of the tissue coupling element. Rotating deployment element 38 is configured to removably engage tool- engaging head 62, as described in more detail hereinbelow with reference to Figs. 4A- D and 6A-C.

0145For some applications, tool 30 provides an anchor restraining mechanism 70 in a vicinity of distal anchor storage area end 41. Anchor restraining mechanism 70 is configured to temporarily restrain at least the distal-most anchor 32 currently stored in anchor storage area 40 from advancing in a distal direction as another one of the anchors is deployed through anchor manipulation area 50 and into the tissue of the subject. Optionally, anchor restraining mechanism 70 is also configured to temporarily restrain at least the distal-most anchor 32 from withdrawing in a proximal direction as inner shaft 36 is withdrawn in the proximal direction to load a subsequent one of the anchors.

0146For some applications, as shown in the blow-up of Fig. 3 A, anchor restraining mechanism 70 comprises one or more distal tabs 72 for temporarily restraining the distal-most anchor 32 currently stored in anchor storage area 40 from advancing in the distal direction. The distal tabs may be cut out of flexible outer tube 34, as shown, or they may be provided as separate elements coupled to the outer tube. The distal tabs apply a force in a radially-inward direction against a distal portion of anchor 32, gently squeezing against the distal portion. The force is sufficient to prevent distal motion of distal-most anchor 32 and the other anchors currently stored in anchor storage area 40, which otherwise would be advanced distally by the force applied on the proximal-most anchor 32 by spring 44. However, the force is insufficient to prevent distal advancement of distal-most anchor 32 when the anchor is engaged and advanced distally by rotating deployment element 38, as described hereinbelow with reference to Figs. 4A-B. For some applications, anchor restraining mechanism 70 comprises two distal tabs 72, typically on opposite sides of the outer tube (typically axially aligned with each other), as shown, while for other applications, the anchor restraining mechanism comprises exactly one distal tab, or three or more distal tabs, e.g., three or four distal tabs (typically axially aligned with one another).

0147For some applications, anchor restraining mechanism 70 comprises a set 73 of one or more proximal tabs 74 for temporarily restraining the distal-most anchor 32 currently stored in anchor storage area 40 from withdrawing in the proximal direction. The proximal tabs may be cut out of flexible outer tube 34, as shown, or they may be provided as separate elements coupled to the outer tube. The distal ends of the proximal tabs engage the proximal end of the tool-engaging head of distal-most anchor 32. For some applications, set 73 comprises two proximal tabs 74, typically on opposite sides of the outer tube (typically axially aligned with each other), as shown, while for other applications, the set comprises exactly one proximal tab, or three or more proximal tabs, e.g., three or four proximal tabs (typically axially aligned with one another).

0148Reference is made to Figs. 4A-D, which are schematic illustrations of the deployment of a single one of anchors 32 into tissue using anchor deployment tool 30, in accordance with an application of the present invention. As shown in Fig. 4A, the anchor to be deployed is the distal-most one of the anchors stored in anchor storage area 40, and is initially restrained in the anchor storage area by anchor restraining mechanism 70. Flexible inner shaft 36 is advanced in a distal direction until rotating deployment element 38 directly engages tool-engaging head 62 of the anchor (by "directly engages," it is meant that rotating deployment element 38 comes in direct contact with the anchor, rather than indirect contact via one or more of the other anchors). Rotating deployment element 38 assumes its radially-expanded state, as described hereinbelow with reference to Fig. 7A, to enable this engagement.

0149As shown in Fig. 4B, flexible inner shaft 36 is advanced in the distal direction, until rotating deployment element 38 brings the anchor into contact with tissue 90 of a subject at a first site. For example, the tissue may be cardiac tissue. Typically, anchor deployment tool 30 is configured such that, as rotating deployment element 38 advances each of the anchors in the distal direction, only the single anchor 32 currently being advanced is within distal anchor manipulation area 50. Rotating deployment element 38 is rotated, in order to screw helical tissue coupling element 60 of the anchor into the tissue. For some applications, rotating deployment element 38 is rotated by rotating flexible inner shaft 36. For other applications, rotating deployment element 38 is rotated by rotating an additional rotation shaft provided within flexible inner shaft 36, which additional shaft is coupled to rotating deployment element 38. Rotation of rotating deployment element 38 typically rotates only the anchor currently engaged by the deployment element, while the other anchors still stored in the storage area typically are not rotated.

0150Typically, anchor 32 is deployed from distal tube end 42 of outer tube 34 of tool 30 into cardiac tissue 90 in a direction parallel to a central longitudinal axis 92 of outer tube 34 through distal tube end 42, and/or parallel to central longitudinal axis 100 of anchor 32, as described hereinbelow with reference to Figs. 6A-C.

0151Also as shown in Fig. 4B, the evacuation of the distal-most anchor from anchor restraining mechanism 70 frees up the anchor restraining mechanism for the next distal-most anchor remaining in anchor storage area 40. Spring 44 distally advances all of anchors 32 remaining in anchor storage area 40, until the next distal- most anchor is positioned within anchor restraining mechanism 70.

0152As shown in Fig. 4C, after the anchor has been coupled to tissue 90, rotating deployment element 38 is disengaged from the anchor by withdrawing the rotating deployment element in a proximal direction. As the rotating deployment element passes through the next anchor in the proximal direction, the rotating deployment element is squeezed by the engaging opening of tool-engaging head 62 of the next anchor, causing the rotating deployment element to assume its radially-compressed state, as described hereinbelow with reference to Fig. 7B.

0153As shown Fig. 4D, anchor deployment tool 30 is repositioned to deploy a second anchor 32 at a second site of tissue 90, different from the first site. Such repositioning is typically accomplished using the steering functionality of distal anchor manipulation area 50, as described hereinabove. The steps of the deployment method are repeated, until as many anchors 32 as desired have been deployed, at respective sites, e.g., a first site, a second site, a third site, a fourth site, etc.

0154Reference is made to Figs. 5A-B, which are schematic illustrations of an alternative configuration of anchor deployment system 20, in accordance with an application of the present invention. In this configuration, anchor restraining mechanism 70 typically comprises one or more distal tabs 72, as in the configuration described hereinabove with reference to Figs. 2, 3A-B, and 4A-D. Unlike in the configuration described hereinabove with reference to Figs. 2, 3A-B, and 4A-D, in this configuration anchor restraining mechanism 70 comprises a plurality of sets 73 of proximal tabs 74, labeled 73A, 73B, 73C, ... in Figs. 5A-B. Each set of proximal tabs 74 engages exactly one anchor 32. For example, the distal ends of proximal tabs 74 of set 73A engage the proximal end of the tool-engaging head of distal-most anchor 32, and the distal ends of proximal tabs 74 of set 73B engage the proximal end of the tool-engaging head of second-to-distal-most anchor 32.

0155Sets 73 thus provide respective anchor storage locations. Therefore, the anchor restraining mechanism comprises a number of sets 73 greater than or equal to the number of anchors 32 initially stored in anchor storage area 40. For some applications, anchor restraining mechanism 70 comprises between 6 and 20 sets 73, such as between 8 and 16 sets 73. For some applications, each of sets 73 comprises two proximal tabs 74, typically on opposite sides of the outer tube (typically axially aligned with each other), as shown, while for other applications, each of the sets comprises exactly one proximal tab, or three or more proximal tabs, e.g., three or four proximal tabs (typically axially aligned with one another).

0156For some applications, each of sets 73 (except the proximal-most set 73) additionally functions as a distal tab 72 for the anchor proximally adjacent to the set. For example, set 73A, in addition to engaging distal-most anchor 32A, also prevents distal motion of second-to-distal-most anchor 32.

0157Unlike in the configuration described hereinabove with reference to Figs. 2, 3A-B, and 4A-D, in the present configuration each of anchors 32 remains in place in its initial, respective anchor storage location in anchor storage area 40, until the anchor is individually advanced out of anchor storage area 40 during deployment by anchor deployment tool 30. Spring 44 is thus typically not provided in this configuration. Deployment of the anchors is typically performed as described hereinabove with reference to Figs. 4A-D, except:

0158· at the step described with reference to Fig. 4B, spring 44 does not

0159distally advance the remaining anchors (as mentioned above, spring 44 is typically not provided in this configuration); and

0160• at the step described with reference to Fig. 4C, anchor deployment tool

016130 is withdrawn further proximally, until the anchor deployment tool reaches the next remaining anchor 32 in anchor storage area 40. The next anchor, as mentioned above, has remained in its original location even after deployment of more distally positioned anchor(s) 32.

0162Reference is now made to Figs. 6A-C, which are schematic illustrations of one of anchors 32 from three different views, in accordance with an application of the present invention. As described above, each of anchors 32 comprises helical tissue coupling element 60, and tool-engaging head 62, fixed to one end of the tissue coupling element (the proximal end of the tissue coupling element, opposite the distal end that first penetrates the tissue). Anchor 32 comprises a hard material, such as metal, e.g., steel, Nitinol, or stainless steel SS316LVM. Anchor 32 may be manufactured from a single piece of material, or coupling element 60 and tool- engaging head 62 may be manufactured from separate pieces of material and fixed together.

0163Typically, helical tissue coupling element 60 has an inner diameter D l of at least 1.5 mm, no more than 2.5 mm, and/or between 1.5 and 2.5 mm, e.g., 1.8 mm, along an entire length thereof along a central longitudinal axis 100 of anchor 32 (although inner diameter D l is shown as being constant along the entire length of coupling element 60, the inner diameter optionally varies along the length of the coupling element). Inner diameter D l is sufficiently large to allow passage through helical tissue coupling element 60 of flexible inner shaft 36 and rotating deployment element 38, optionally even when rotating deployment element 38 is in its radially- expanded state, as described hereinbelow with reference to Fig. 7A. An outer diameter D2 of helical tissue coupling element 60 may be, for example, at least 2.4 mm, no more than 5 mm, and/or between 2.4 and 5 mm, e.g., 2.4 mm.

0164Tool-engaging head 62 is shaped so as to define an engaging opening 102 that passes entirely through the tool-engaging head along axis 100. The engaging opening is typically at least partially non-circular, in order to engage rotating deployment element 38. For example, as shown in Figs. 6A-C, engaging opening 102 may be shaped so as to define a proximal non-circular internal engaging surface 66, and a distal circular non-engaging surface 64. Proximal engaging surface 66 is shaped to engage rotating deployment element 38, such that rotation of the deployment element rotates tool-engaging head 62 and anchor 32. For example, proximal engaging surface 66 may be rectangular (e.g., square), teethed (e.g., defining a plurality of squares with which rotating element 38 can engage, for applications in which engaging elements 120A and 120B together have a square cross-sectional shape), star- shaped, polygonal (e.g., octagonal), or any other appropriate non-circular shape.

0165A portion of deployment element 38 may pass partially or completely through distal non-engaging surface 64, without engaging this surface. The non-engaging surface may serve as a shoulder, which pushes against tissue 90, providing resistance when the anchor has been sufficiently screwed into the tissue. Optionally, deployment element 38 does not pass entirely through distal non-engaging surface 64, such that the deployment element does not press against or into the tissue. Alternatively, the deployment element may protrude slightly from the distal non- engaging surface 64, as shown in Figs. 8A-B, when no force is applied to the deployment clement by the tissue. Optionally, when the anchor is pressed against the tissue, inner spaces in the tool-engagement head 62 of the anchor al low the deployment element to sink into the anchor, and not press against the tissue.

0166Engaging opening 102 typically has a cross-sectional area (perpendicular to axis 1 00) of at least 0.8 mm2, such as at least 1.2 mm2. The area is sufficiently large to allow passage through engaging opening 102 of flexible inner shaft 36 and rotating deployment element 38, when the rotating deployment element assumes its radially- compressed state by being withdrawn in a proximal direction (from tissue coupling element 60 toward tool-engaging head 62), as described hereinbelow with reference to Fig. 7B.

0167For some applications, the anchor is used to couple a sheet of material, such as a fabric, to tissue 90. For these applications, because the tissue coupling element is fixed near the edge of the tool-engaging head, the sheet resists further rotation of the anchor once the anchor is fully screwed into the tissue and the tool-engaging head contacts the sheet. Such resistance prevents accidental over-rotation of the anchor, which could tear the tissue or the sheet, in contrast, in anchors in which the tissue coupling element is fixed at or near the center of the tool-engaging head, the sheet does not resist rotation of the anchor after the anchor has been fully screwed into the tissue and the tool-engaging head contacts the sheet. For some applications, the surgeon or a sensor sense increased resistance to rotation of the tissue coupling element when the sheet resists the rotation, and, responsively the sensed increased resistance, the surgeon ceases rotating the tissue coupling element into the tissue

0168For some applications, anchor deployment system 20 comprises a torque- limiting element, as is known for conventional screwdrivers, to prevent over- application of torque. Alternatively or additionally, for some applications, anchor deployment system 20 comprises a sensor (e.g., a torque transducer), for measuring the resistance to rotation of anchor 32. When the measured resistance exceeds a threshold value, the system generates a signal alerting the surgeon, and/or discontinues rotation of inner shaft 36. The increased resistance is typically caused by the sheet, as described above, and/or the non-engaging surface (shoulder) of the anchor head, as described above.

0169For some applications, a proximal-most portion 106 of helical tissue coupling element 60, at the end which is fixed to tool-engaging head 62, is generally straight and oriented generally parallel to axis 100, i.e., at angle of between 0 and 1 5 degrees with the axis, such as 0 degrees. Proximal-most portion 106 typically has a length of between 0.5 and 2 mm, such as about 1 mm. The outer perimeter of tool -engaging head 62 is typically circular, and an outer diameter D3 of tool-engaging head 62 may be, for example, at least 2 mm, no more than 7 mm, and/or between 2 and 7 mm, such as between 2.5 and 5 mm, e.g., 2.4 mm, 2.5 mm, or 3 mm.

0170The outer diameter of anchor 32 is typically equal to outer diameter D3 of tool-engaging head 62, or, alternatively, to outer diameter D2 of coupling element 60. The outer diameter of anchor 32 may be, for example, at least 2 mm, no more than 7 mm, and/or between 2 and 7 mm, such as between 2.5 and 5 mm. The entire length of anchor 32, measured along axis 100, is typically at least 2.5 mm, no more than 6 mm, and/or between 2.5 and 6 mm, such as between 3 and 4.5 mm.

0171The proximal end of tissue coupling element 60 is typically fixed to tool- engaging head 62 near the outer perimeter of the tool-engaging head, such that the tissue coupling element does not block engaging opening 102. For example, as labeled in the top-view of the anchor in Fig. 6C, the tissue coupling element may be fixed to the tool-engaging head such that one or more of the following dimension characterize the anchor:

0172• a distance D5 between (a) a center 1 10 of the proximal end of tissue

0173coupling element 60 and (b) an outer perimeter of tool-engaging head 62 is no more than 20% of a width D3 of tool-engaging head 62 (the width is a diameter for applications in which the head is circular), such as no more than 10% of width D3. For example, distance D5 may be between 0.1 and 0.3 mm, e.g., 0.2 mm;

0174• a distance D6 between (a) a most radially-inward portion 1 12 of the

0175proximal end of tissue coupling element 60 (i.e., the portion of the proximal end that is closest to central longitudinal axis 100 of the anchor) and (b) the outer perimeter of tool-engaging head 62 is no more than 40% of width D3 of tool-engaging head 62 (the width is a diameter for applications in which the head is circular), such as no more than 30% of width D3, or no more than 20% of width D3. For example, distance D6 may be between 0.3 and 0.5 mm, e.g., 0.4 mm;

0176and/or • a distance between (a) a most radially-outward portion 1 14 of the proximal end of tissue coupling element 60 (i.e., the portion of the proximal end that is furthest from central longitudinal axis 100 of the anchor) and (b) the outer perimeter of tool-engaging head 62 is no more than 10% of width D3 of tool-engaging head 62 (the width is a diameter for applications in which the head is circular), such as no more than 5% of width D3, e.g., 0. For example, distance D6 may be between 0 and 0.1 mm, e.g., 0 mm.

0177Anchor 32, including both helical tissue coupling element 60 and tool- engaging head 62, is thus shaped so as to provide a channel along the entire length of the anchor, through which flexible inner shaft 36 can pass, and through which rotating deployment element 38 can pass when in its radially-compressed state, as described hereinabove with reference to Figs. 1 A-4D. More generally, as shown in Fig. 6B, the channel is sized and shaped such that a right circular cylinder 104 could be placed within the channel, coaxial with anchor 32 (i.e., the axis of the cylinder coincides with central longitudinal axis 100 of anchor 32), and along the entire length of the tissue anchor, the cylinder having a diameter D4 of at least 1 mm, such as at least 2 mm. Typically, diameter D4 is between 0.05 and 1 mm greater than diameter D3 of tool- engaging head 62. It is to be understood that cylinder 104 is an abstract geometric shape, rather than an element of an embodiment of the invention, and, as such, is perfectly cylindrical, i.e., is not shaped so as to define any grooves or other surface or internal anomalies. No portion of anchor 32 intersects central longitudinal axis 100.

0178Reference is made to Figs. 7A and 7B, which are schematic illustrations of rotating deployment element 38 in radially-expanded and radially-compressed states, respectively, in accordance with an application of the present invention. For some applications, rotating deployment element 38 is shaped so as to define at least two prongs 124A and 124B that extend in a distal direction from a proximal base 122 of the deployment element. Engagement elements 120A and 120B extend in a distal direction from prongs 124A and 124B, respectively. The engagement elements are typically male, and, for example, may together have a cross-sectional shape that is rectangular, e.g., square. Optionally, rotating deployment element 38 comprises more than two prongs and two engagement elements, e.g., three or four of each. Rotating deployment element 38 is typically configured to assume a radially- expanded state as its resting state, as shown in Fig. 7A. In this expanded state, engagement elements 120A and 120B, as well as prongs 124A and 124B, are positioned apart from one another. In this state, the engagement elements are shaped and sized to engage tool-engaging head 62 of anchor 32, as shown, for example, in Fig. 4B.

0179As shown in Fig. 7B, the rotating deployment element 38 assumes a radially- compressed state, when the engagement elements and prongs are squeezed together, such as by passing through the engaging opening of tool-engaging head 62 of anchor 32, as described hereinabove with reference to Fig. 4C.

0180Reference is now made to Figs. 8A and 8B, which are schematic illustrations of rotating deployment element 38 engaging tool-engaging head 62 of anchor 32, with the element 38 in locked and unlocked states, respectively, in accordance with an application of the present invention. In accordance with this application, rotating deployment element 38 comprises a locking mechanism 128, which is configured to selectively assume locked and unlocked states. When locking mechanism 128 assumes the locked state, the locking mechanism prevents disengagement of rotating deployment element 38 from the anchor which rotating deployment element 38 currently engages anchor. This locking allows deployment element 38 to proximally withdraw anchor 32 if necessary, without coming disengaged therefrom. Disengagement is thus prevented even upon withdrawal of the rotating deployment element in the proximal direction. When the locking mechanism assumes the unlocked state, the locking mechanism does not prevent disengagement of the rotating deployment element from the anchor upon withdrawal of rotating deployment element 38 in the proximal direction. The rotating deployment element thus can be disengaged and withdrawn from the anchor in a proximal direction. It is noted that even when the locking mechanism assumes the unlocked state, the rotating deployment element generally does not disengage from the anchor unless the rotating deployment element is withdrawn in the proximal direction. As mentioned above with reference to Fig. 7 A, rotating deployment element 38 is typically configured to assume a radially-expanded state as its resting state. In this radially-expanded state, engagement elements 120A and 120B are positioned apart from each other, and engage tool-engaging head 62 of anchor 32.

0181For some applications, locking mechanism 128 comprises a pin 130. In order to cause the locking mechanism to assume the locked position, pin 130 is advanced distally between engagement elements 120A and 120B. The pin holds the engagement elements in their radially-expanded state, as described hereinabove with reference to Fig. 7A, thereby preventing the engagement elements from assuming the radially-compressed state shown in Fig. 7B and disengaging from the anchor. In the radially-expanded state, the engagement elements engage proximal engaging surface 66 of tool-engaging head 62 of anchor 32. In order to cause locking mechanism 128 to assume the unlocked state, pin 130 is withdrawn proximally from between engagement elements 120A and 120B. As a result, the engagement elements may assume the radially-compressed state shown in Fig. 7B when deployment element 38 is withdrawn in the proximal direction. In the radially-compressed state, the engagement elements do not engage the tool-engaging head of the anchor.

0182Providing this selective, actively-controllable engagement and release of the anchor allows rotating deployment element 38 to be used to unscrew an already- deployed anchor from the tissue, and/or to proximally withdraw an anchor, without deployment element 38 unintentionally disengaging from the anchor head. Such unscrewing or proximal withdrawal may allow an anchor to be repositioned if it is initially coupled to the tissue in an incorrect location. Rotating deployment element 38 is capable of performing this redeployment for both (a) the anchor that has been most recently deployed into the tissue, and to which the deployment element 38 is still coupled, and (b) an anchor that was previously deployed, and from which deployment element 38 has already been decoupled (and, optionally, even after another anchor has subsequently been deployed). In the latter case, deployment element 38 re-engages the anchor that is to be redeployed.

0183Reference is now made to Figs. 9A-I, which are schematic illustrations of a procedure for implanting an annuloplasty ring 222 to repair a mitral valve 230, in accordance with an application of the present invention. This procedure is one exemplary procedure that can be performed using anchor deployment system 20. Annuloplasty ring 222 is used to repair a dilated valve annulus of an atrioventricular valve, such as mitral valve 230. For some applications, the annuloplasty ring is configured to be placed only partially around the valve annulus (e.g., to assume a C-shape), and, once anchored in place, to be contracted so as to circumferentially tighten the valve annulus. The annuloplasty ring comprises a flexible sleeve 226 and a plurality of anchors 32. Anchor deployment tool 30 is advanced into a lumen of sleeve 226, and, from within the lumen, deploys the anchors through a wall of the sleeve and into cardiac tissue, thereby anchoring the sleeve around a portion of the valve annulus. For some application, annuloplasty ring 222 is implemented using techniques described in US Application 12/437, 103, filed May 7, 2009 which published as US 2010/0286767, and/or US Application 12/689,635, filed January 19, 2010 which published as US 2010/0280604, both of which are assigned to the assignee of the present application and are incorporated herein by reference. For some application, annuloplasty ring 222 comprises a contracting mechanism 243. The contracting mechanism comprises a rotatable structure, such as a spool, arranged such that rotation of the rotatable structure contracts the implant structure. The implant further comprises a longitudinal member, such as a wire, which is coupled to the contracting mechanism. A rotation tool is provided for rotating the rotatable structure. The tool is configured to be guided along (e.g., over, alongside, or through) the longitudinal member, to engage the rotatable structure, and to rotate the rotatable structure in response to a rotational force applied to the tool.

0184As shown in Fig. 9A, the procedure typically begins by advancing a semi-rigid guidewire 202 into a right atrium 220 of the patient. The procedure is typically performed with the aid of imaging, such as fluoroscopy, transesophageal echo, and/or echocardiography.

0185As show in Fig. 9B, guidewire 202 provides a guide for the subsequent advancement of a sheath 204 therealong and into the right atrium. Once sheath 204 has entered the right atrium, guidewire 202 is retracted from the patient's body. Sheath 204 typically comprises a 14-20 F sheath, although the size may be selected as appropriate for a given patient. Sheath 204 is advanced through vasculature into the right atrium using a suitable point of origin typically determined for a given patient. For example: • sheath 204 may be introduced into the femoral vein of the patient, through an inferior vena cava 223, into right atrium 220, and into a left atrium 224 transseptally, typically through the fossa ovalis;

0186• sheath 204 may be introduced into the basilic vein, through the

0187subclavian vein to the superior vena cava, into right atrium 220, and into left atrium 224 transseptally, typically through the fossa ovalis; or

0188• sheath 204 may be introduced into the external jugular vein, through

0189the subclavian vein to the superior vena cava, into right atrium 220, and into left atrium 224 transseptally, typically through the fossa ovalis.

0190For some applications of the present invention, sheath 204 is advanced through inferior vena cava 223 of the patient (as shown) and into right atrium 220 using a suitable point of origin typically determined for a given patient.

0191Sheath 204 is advanced distally until the sheath reaches the interatrial septum, and guidewire 202 is withdrawn, as shown in Fig. 9C.

0192As shown in Fig. 9D, a resilient needle 206 and a dilator (not shown) arc advanced through sheath 204 and into the heart. In order to advance sheath 204 transseptally into left atrium 224, the dilator is advanced to the septum, and needle 206 is pushed from within the dilator and is allowed to puncture the septum to create an opening that facilitates passage of the dilator and subsequently sheath 204 therethrough and into left atrium 224. The dilator is passed through the hole in the septum created by the needle. Typically, the dilator is shaped to define a hollow shaft for passage along needle 206, and the hollow shaft is shaped to define a tapered distal end. This tapered distal end is first advanced through the hole created by needle 206. The hole is enlarged when the gradually increasing diameter of the distal end of the dilator is pushed through the hole in the septum.

0193The advancement of sheath 204 through the septum and into the left atrium is followed by the extraction of the dilator and needle 206 from within sheath 204, as shown in Fig. 9E.

0194As shown in Fig. 9F, annuloplasty ring 222 (with anchor deployment tool 30 therein) is advanced through sheath 204 into left atrium 224. As shown in Fig. 9G, a distal end 25 1 of sleeve 226 is positioned in a vicinity of a left fibrous trigone 242 of an annuius 240 of mitral valve 230. (It is noted that for clarity of illustration, distal end 251 of sleeve 226 is shown schematically in the cross- sectional view of the heart, although left trigone 242 is in reality not located in the shown cross-sectional plane, but rather out of the page closer to the viewer.) Alternatively, the tip is positioned in a vicinity of a right fibrous trigone 244 of the mitral valve (configuration not shown). Further alternatively, the distal tip of the sleeve is not positioned in the vicinity of either of the trigones, but is instead positioned elsewhere in a vicinity of the mitral valve, such as in a vicinity of the anterior or posterior commissure. The steering functionality of anchor manipulation area 50 typically allows the area near the distal end of the deployment tool to be positioned with six degrees of freedom. Once positioned at the desired site near the selected trigone, deployment tool 30 deploys a first anchor 32 through the wall of sleeve 226 into cardiac tissue near the trigone, using the techniques described hereinabove with reference to Figs. 4A-C.

0195As shown in Fig. 9H, deployment tool 30 is repositioned along annuius 240 to another site selected for deployment of a second anchor 32. Typically, the first anchor is deployed most distally in the sleeve (generally at or within a few millimeters of the distal tip of the sleeve), and each subsequent anchor is deployed more proximally, such that the sleeve is gradually pulled off (i.e., withdrawn from) the deployment tool in a distal direction during the anchoring procedure. The already- deployed first anchor 32 holds the anchored end of sleeve 226 in place, so that the sleeve is drawn from the site of the first anchor towards the site of the second anchor. Typically, as the sleeve is pulled off (i.e., withdrawn from) the deployment tool, the deployment tool is moved generally laterally along the cardiac tissue, as shown in Fig. 9H. Deployment tool 30 deploys the second anchor through the wall of the sleeve into cardiac tissue at the second site. Depending on the tension applied between the first and second anchor sites, the portion of sleeve 226 therebetween may remain tubular in shape, or may become flattened, which may help reduce any interference of the ring with blood flow. The techniques described hereinabove with reference to Fig. 4D, followed again by those described with reference to Figs. 4A-C, are used to provide and deploy the second and subsequent anchors one at a time at the selected sites, respectively.

0196As shown in Fig. 91, deployment tool 30 (as shown in Figs. 4A-D) is repositioned along the annulus to additional sites, at which respective anchors are deployed, until the last anchor is deployed in a vicinity of right fibrous trigone 244 (or left fibrous trigone 242 if the anchoring began at the right trigone). Alternatively, the last anchor is not deployed in the vicinity of a trigone, but is instead deployed elsewhere in a vicinity of the mitral valve, such as in a vicinity of the anterior or posterior commissure. A rotation tool or anchor driver is used to rotate the spool of contracting mechanism 240, in order to tighten ring 222.

0197Alternatively, annuloplasty ring 222 is implanted by right or left thoracotomy, mutatis mutandis.

0198Reference is made to Fig. 10. For some applications of the present invention, annuloplasty ring 222 is used to treat an atrioventricular valve other than the mitral valve, i.e., tricuspid valve 231 , using tool 30 (as shown in Figs. 4-A-D) in a similar method as described hereinabove with reference to Figs. 9A-I, in accordance with some applications of the present invention.

0199For these applications, ring 222 and other components of system 20 described hereinabove as being placed in the left atrium are instead placed in the right atrium 220. Fig. 10 shows accessing right atrium 220 through superior vena cava 225 by way of illustration and not limitation. Components of system 20 may be advanced into the right atrium through inferior vena cava 223.

0200Although annuloplasty ring 222 is described hereinabove as being placed in an atrium, for some application the ring is instead placed in either the left or right ventricle.

0201Accordingly, it is noted that, annuloplasty ring 222 and other components of system 20 described hereinabove and methods shown in the application can be used on any cardiac valve (e.g., the mitral, tricuspid, aortic, and/or pulmonary). It is further noted that the scope of the present invention includes the use system 20 (or subcomponents thereof) and methods described hereinabove on any suitable tissue of the subject (e.g., stomach tissue, urinary tract, and prostate tissue).

0202In an application of the present invention, anchor deployment system 20 is used in combination with mitral valve repair system 400, described with reference to Figs. 17A-F, 18A-B, 19A-E, and 20A-B of International Application PCT/IL2009/000593, filed June 15, 2009, which published as PCT Publication WO 10/004546, and which is incorporated herein by reference. Instead of passing anchors through the lumen of the catheter from a site outside the body of the patient, as described with reference to Fig. 20B, the anchors are stored in anchor storage area 40 of anchor deployment tool 30.

0203For some applications, techniques described herein are practiced in combination with techniques described in one or more of the references cited in the specification, all of which are incorporated herein by reference.

0204Additionally, the scope of the present invention includes embodiments described in the following applications, which are incorporated herein by reference. In an embodiment, techniques and apparatus described in one or more of the following applications are combined with techniques and apparatus described herein:

0205• PCT Publication WO 06/097931 to Gross et al., entitled, "Mitral Valve

0206treatment techniques," filed March 15, 2006;

0207• US Provisional Patent Application 60/873,075 to Gross et al., entitled,

0208"Mitral valve closure techniques," filed December 5, 2006;

0209• US Provisional Patent Application 60/902, 146 to Gross et al., entitled,

0210"Mitral valve closure techniques," filed February 16, 2007;

0211· US Provisional Patent Application 61/001 ,013 to Gross et al., entitled,

0212"Segmented ring placement," filed October 29, 2007;

0213• PCT Patent Application PCT/IL07/001503 to Gross et al., entitled,

0214"Segmented ring placement," filed December 5, 2007; US Patent Application 1 1/950,930 to Gross et al., entitled, "Segmented ring placement," filed December 5, 2007, which published as US Patent Application Publication 2008/0262609;

0215US Provisional Patent Application 61/132,295 to Gross et al., entitled, "Annuloplasty devices and methods of delivery therefor," filed June 16, 2008;

0216US Patent Application 12/341 ,960 to Cabiri, entitled, "Adjustable partial annuloplasty ring and mechanism therefor," filed December 22,

02172008, which published as US Patent Application Publication 2010/0161047;

0218US Provisional Patent Application 61 /207,908 to Miller et al., entitled, "Actively-engageable movement-restriction mechanism for use with an annuloplasty structure," filed February 1 7, 2009;

0219US Patent Application 12/435,291 to Maisano et al., entitled, "Adjustable repair chords and spool mechanism therefor," filed May 4,

02202009, which published as US Patent Application Publication 2010/0161041 ;

0221US Patent Application 12/437, 103 to Zipory et al., entitled, "Annuloplasty ring with intra-ring anchoring," filed May 7, 2009, which published as US Patent Application Publication 2010/0286767;

0222PCT Patent Application PCT/TL2009/000593 to Gross et al., entitled, "Annuloplasty devices and methods of delivery therefor," filed June 15, 2009, which published as PCT Publication WO 10/004546;

0223US Patent Application 12/548,991 to Maisano et al., entitled, "Implantation of repair chords in the heart," filed August 27, 2009, which published as US Patent Application Publication 2010/0161042;

0224US Patent Application 12/608,316 to Miller et al., entitled, "Tissue anchor for annuloplasty ring," filed October 29, 2009, which published as US Patent Application Publication 201 1/0106247; • US Provisional Patent Application 61/265,936 to Miller et al., entitled, "Delivery tool for implantation of spool assembly coupled to a helical anchor," filed December 2, 2009;

0225• PCT Patent Application PCT/IL2009/001209 to Cabiri et al., entitled,

0226"Adjustable annuloplasty devices and mechanisms therefor," filed December 22, 2009, which published as PCT Publication WO 2010/073246

0227• US Patent Application 12/689,635 to Zipory et al., entitled, "Over-wire

0228rotation tool," filed January 19, 2010, which published as US Patent Application Publication 2010/0280604;

0229• US Patent Application 12/689,693 to Hammer et al., entitled,

0230"Deployment techniques for annuloplasty ring," filed January 1 9, 2010;

0231• US Patent Application 1 2/706,868 to Miller et al., entitled, "Activcly- engageable movement-restriction mechanism for use with an annuloplasty structure," filed February 17, 2010 which published as US Patent Application Publication 2010/021 1 166;

0232• PCT Patent Application PCT/IL2010/000357 to Maisano et al.,

0233entitled, " Implantation of repair chords in the heart," filed May 4, 2010, which published as PCT Publication WO 2010/128502;

0234• PCT Patent Application PCT/1L2010/000358 to Zipory et al., entitled,

0235"Deployment techniques for annuloplasty ring and over-wire rotation tool," filed May 4, 2010 which published as PCT Publication WO2010/128503 ; and/or

0236• US Regular Application 12/785,717 to Miller et al., entitled,

0237"Adjustable artificial chordeae tendineae with suture loops," filed May 24, 2010.

0238It will be appreciated by persons skilled in the art that the present invention is not limited to what has been particularly shown and described hereinabove. Rather, the scope of the present invention includes both combinations and subcombinations of the various features described hereinabove, as well as variations and modifications thereof that are not in the prior art, which would occur to persons skilled in the art upon reading the foregoing description.