Ceramic to metal seal
Abstract
This record has no abstract on file.
Term
Term ended
Expired 27 July 1988, 38.2 years ago.
- Priority and filed
- Granted
- Expired
- Today
8 claims: 6 independent, 2 dependent
- 1What we claim is:1. A metal to ceramic seal which consists essentially of a ductile brazing alloy interposed between the metal and ceramic, said alloy consisting essentially of a single phase ductile alloy within the range of 48 alo—52 alo of titanium with a member selected from the group consisting of Fe, and Co and mixtures thereof.
- 3A metal to ceramic seal which consists essentially of a ductile brazing alloy interposed between the metal and ceramic, said alloy consisting essentially of a single phase ductile alloy within the range of 48 a/o—52 a/o of zirconium with a member selected from the group consisting of Ru, Rh and Pd and mixtures thereof.
- 4A metal to ceramic seal which consists essentially of a ductile brazing alloy interposed between the metal and ceramic, said alloy consisting essentially of a single phase ductile alloy within the range of 48 a/o—52 a/o of hafnium with a member selected from the group consisting of Os, Ir, Pt and mixtures thereof.
- 5A method of bonding a metal member and a nonmetallic refractory body which consists essentially of interposing therebetween a preform of a single phase ductile alloy within the range of 48 a/o—52 alo of titanium with a member selected from the group consisting of Fe and Co, and mixtures thereof, then melting only said alloy under nonoxidizing conditions, and thereafter cooling the assembly whereby said alloy forms a tight high temperature resistant bond between 10 the metal member and the refractory body.
- 7A method of bonding metal member and a nonmetallic refractory body which consists essentially of interposing therebetween a preform of a single phase ductile alloy within the range of 48 alo—52 a/o of zirconium with a member 2θ selected from the group consisting of Ru, Rh, Pd and mixtures thereof, then melting only said alloy under nonoxidizing conditions, and thereafter cooling the assembly whereby said alloy forms a tight high temperature resistant bond between the metal member and refractory body.
- 8A method of bonding a metal member and a nonmetallic refractory body which consists essentially of interposing therebetween a preform of a single phase ductile alloy within the range of 48 a/o—52 a/ο of hafnium with a member selected from the group consisting of Os, Ir, Pt and mixtures 30 thereof, then melting only said alloy under nonoxidizing conditions, and thereafter cooling the assembly whereby said alloy forms a tight high temperature resistant bond between the metal member and the refractory body. ^0-1050 '5/69) UNITED STATES PATENT OFFICE CERTIFICATE OF CORRECTION atent No. 3, 594,895 Dated July 27, 1971 Inventor(s) Russell J, Hill and Rowland M. Cannon It is certified that error appears in the above-identified patent and that said Letters Patent are hereby corrected as shown below:Column 2, line 58, for 10. 4xl016 °C11 read---10.4-6 °C-1___;and Column 3, line 1 through line 3 should read---In the same fashion a 50 a/o zirconium-palladium braze alloy washer and a 50 a/o hafniumiridium braze alloy washer formed a good seal between a tantalum cup and an alumina tube. ---. r Signed and sealed this 12th day of September 1972. (SEAL) Attest: EDWARD M.FLETCHER,JR Attesting Officer ROBERT GOTTSCHALK Commissioner of Patents
Independent claims6
48 paragraphs in 2 sections, as filed
United States Patent ii 3,594,895
<td> [72]</td><td> Inventors</td><td> Russell J. Hill 20 Marie Drive, R.F.C. No. 3, Wilmington, Mass. 01887;</td>
<td></td><td></td><td> Rowland M. Cannon, Jr., 1S1 Highland Ave., Arlington, Mass. 02174</td>
<td> (21]</td><td> Appl. No.</td><td> 748,227</td>
<td> [22]</td><td> Filed</td><td> July 29,1968</td>
<td> [45]</td><td> Patented</td><td> July 27,1971</td>
<td> [54]</td><td colspan="2"> CERAMIC TO METAL SEAL 8 Claims, No Drawings</td>
[52] U-S. Cl........................................................ 29/473.1,
29/195,29/504
[51] Int. CL........................................................B23k 31/02
[50] Field of Search............................................ 29/473.1,
472.7,504,195
[56|
References Cited
UNITED STATES PATENTS
<td> 2,857,663</td><td> 10/1958</td><td> Beggs........................</td><td> 29/473.1</td>
<td> 2,859,512</td><td> 11/1958</td><td> Dijksterhuis etal.......</td><td> 29/473.1</td>
<td> 3,091,028</td><td> 5/1963</td><td> Westbrook et al..........</td><td> 29/473.1</td>
<td> 3,395,993</td><td> 8/1968</td><td> Bristow......................</td><td> ... 29/473.1 X</td>
Primary Examiner—John F. Campbell
Assistant Examiner—Ronald J. Shore
Attorneys—Charles M. Hogan and Abraham Ogman
ABSTRACT: This disclosure is directed to metal to refractory seals wherein a ductile 50 atomic percent alloy of a group 1VZ> metal with a group VIII metal of the same period is used to braze ceramic to metal. A preferred example is sealing Tantalum or Niobium to alumina with a 50 a/o Ti-Ni alloy braze.
3,594,895
CERAMIC TO METAL SEAL
The present invention relates to the bonding of nonmetallic refractory members to metal members, and more particularly 3 to a temperature resistant, oxidation resistant metal to ceramic seal capable of use in cesium environments.
The problems involved in obtaining satisfactory ceramic to metal seals are well known, and various brazing alloys have been suggested by workers in the art, as in, for example, U.S. 'θ Pats. Nos. 3,091,028 and 2,857,663. Such seals are important to satisfactory operation of high power electron tube devices and are notably so in devices employing metal vapors or liquid therein such as arc devices and thermionic converters.
A common prior art method of making such seals involves first placing a layer of metal on the surface of the ceramic body or member then brazing the metal body or member to the metallized ceramic with the aid of a fusible metallic shim therebetween. Any of the several diverse metal to metal inter- 20 faces present in the so sealed structure may have a brittle intermetallic phase in the metal junction due to interaction between metal, braze, and metallized ceramic. Besides the high failure rate, the joint or seal as a whole may be weak due to the various intermetallic phases present. Eliminating the 25 metallizing step and brazing directly to the ceramic body offers promise for more facile sealing techniques, even better seals. The braze metal must then be some material which reacts strongly with the ceramic in order to achieve the desired bond. Yet, the high chemical reactivity of such a braze 30 metal may cause the braze also to react strongly with the metal member. Thus, if a pure metal braze is employed, the solution resulting from dissolution of the metal body and the braze metal has a progressively lower melting point than the pure braze metal and substantial, even complete, dissolution of the 35 metal body can result if the completed seal is subjected to high operating temperatures. On the other hand, if a eutectic braze is employed, the metal from the metal body which dissolves therein often forms a brittle intermetallic phase between itself and one or both of the braze constituents. <sup>4</sup>θ
In any event, an upper operating limit of about 500° C. is commonly set for the ultimate equipment sealed by conventional brazing alloys and the heretofore employed ceramic to metal sealing techniques.
An object of the present invention is to provide an improved <sup>45 </sup>bond for joining nonmetallic refractory bodies to metallic members.
A further object of the invention is to provide a ceramic to metal seal having good compatibility with a cesium environment and operation at elevated temperatures.
Still another object of the invention is to provide a high quality ceramic to metal seal employing a ductile metal braze.
Further objects and the advantages of the present invention will be apparent from the description thereof which follows. j
Briefly stated, the practice of the present invention comprises forming the seal with a 50 atomic percent alloy of one member selected from the group IVb metals and the other member selected from the group VIII metals of the same period. More specifically, the alloys contemplated for the /,0 braze material are the 50 alo alloys of: titanium with iron, cobalt, nickel or mixtures thereof; hafnium with osmium, iridium, platinum, or mixtures thereof; zirconium with rhodium, ruthenium, palladium, or mixtures thereof.
Most significant in terms of the ceramic to metal seal is that 05 this group of 50 atomic percent alloys or intermetallic compounds are ductile and have a significant homogeneity range on either side of the 50 a/o. They remain ductile within this range of homogeneity. Thus, the Ti-Ni system has a homogeneity range of 46—53 a/o Ti. The other systems have 70 similar, but not necessarily identical homogeneity ranges. For further description of the alloys per se reference is made to a series of articles by F. E. Wang or F. E. Wang et al. in Journal of Applied Physics, Vol. 36, p. 3232 (1965); Vol. 38, p. 822 (1967); and Vol. 29, p. 2192 (1968). Attention is directed 75 also to U;S. Pat. No. 3,174,851 for description of the 50 a/o Ti-Ni alloy.
While reference has been made above to 50 a/o, the ductile alloy brazes contemplated for practice of this invention may be of any specific composition within their homogeneity range. Therefore, within the context of this invention a general reference to these alloy brazes as 50 a/o ductile alloys should be taken as a reference to include the entire range of homogeneity. As a practical matter the braze alloy composition should be held within somewhat narrower limits than the entire homogeneity range, 50 a/o±2 a/o being preferred.
When the IVfc—VIII ductile 50 a/o alloys are used as brazes to join ceramic bodies to metal members, they perform in a beneficial and perhaps unique manner. The molten alloy reacts with the ceramic to form a hermetic joint, eliminating need for preliminary metallizing of the ceramic. Moreover, the braze reacts only slightly with the metal member in the seal assembly. Any intermetallic reaction products between the braze alloy and the metal member are not precipitated as a brittle intermetallic phase. After the seal has been formed no subsequent conditioning steps are needed. These ductile 50 a/o alloy brazes have general applicability to the many refractory ceramics usually joined to metal members, including for example, alumina, zirconia, magnesia yttria, sapphire. They have, also, general applicability to the metals usually joined to ceramics for electronic uses, including for example, tantalum, niobium, the group VIII metals. Importantly, they can be used at elevated temperatures, e.g. to 800° C.
One exemplary instance of a preferred embodiment of practice according to the invention is formation of a seal between a niobium member or a tantalum member and a high purity alumina body with a ductile 50 a/o alloy of titanium-nickel.
Use of these ductile 50 a/o alloy brazes permits seal fabrication by relatively uncomplicated techniques. According to one method, the ceramic body and the metal member to be joined are juxtaposed with a shim or wire of the chosen intermetallic alloy placed between them. This assembly is then heated, e.g. in a vacuum furnace or by radio frequency induction heating in an argon atmosphere to the melting point of the chosen alloy, at which point the molten alloy reacts with and wets the ceramic body and also brazes to the metal member. The braze material remains as a single phase ductile intermetallic alloy. Thereafter the assembly is cooled as rapidly as the ceramic will allow. The joint is ready for use without further conditioning. It is airtight, heat and oxidation resistant and stable for use over extended periods of time; it may be employed in a cesium environment,
For further understanding of the invention more detailed specific examples of the practice thereof is now presented.
A nickel titanium alloy of exactly 50 a/o employed as the braze alloy had the following properties:
Density Melting point Electrical resistivity (room temperature) Expansion coefficient Ultimate tensile strength Yield strength Young’s Modulus Tensile elongation
6.45 g./cc. l250<sup>e</sup>C. 80 /ifiem.
10.4X10'· °C. 140,000 p.s.i.
81,000 p.s.i. 11X10· p.s.i. up to 15 percent
A washer (0.005 inches thick) of the alloy was placed at the bottom of a tantalum cup and a high purity alumina tube was placed on top the washer. The so assembled cup, washer and tube was heated inductively in a stream of commercial grade argon to a temperature just above 1250° C. to melt the washer. The assembly was then cooled in the argon stream and removed, with the whole heating, melting and cooling process taking about 5 minutes. Examination of the cooled assembly showed that very little dissolution of the tantalum had taken place during the brief period the braze was molten and that an airtight satisfactory seal was formed.
3,594,895
In the same fashion a 50 alo hafnium-iridium braze alloy washer formed a good seal between a tantalum cup and an alumina tube.
Sealed assemblies, sealed by the 50 alo Ti-Ni, braze alloy in the manner described above were fully fabricated and tested 5 for temperature resistance in the presence of cesium. They proved satisfactory at elevated temperatures up to 800° C.
In the same fashion a tantalum tube was brazed to magnesia with the above 50 alo Ti-Ni alloy. In this instance the differential expansion between magnesia and tantalum caused the magnesia to crack upon cooling, but the seal itself appears satisfactory.
Contents2
Every citation, both ways
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4 priority claims, no other members on record
Priority claims4
| Document | Office | Kind | Date |
|---|---|---|---|
| 74822768 | United States of America | A | |
| 74822768 | United States of America | A | |
| 748227 | – | – | – |
| US19680748227 | – | – | – |
Numbers
- Publication, DOCDB
- 3594895
- Publication, EPODOC
- US3594895
- Application
- 748227
- Application, DOCDB
- 3594895D
- Application, EPODOC
- USD3594895
Titles
- English
- CERAMIC TO METAL SEAL
Classification
- CPC, 22
- B23K35/3033
- B23K35/3046
- B23K35/3093
- B23K35/32
- C04B37/026
- C04B2235/6567
- C04B2235/667
- C04B2237/122
- C04B2237/126
- C04B2237/127
- C04B2237/30
- C04B2237/34
- C04B2237/343
- C04B2237/348
- C04B2237/403
- C04B2237/76
- C04B2237/765
- Y10T428/12618
- Y10T428/12806
- Y10T428/12812
- Y10T428/12819
- Y10T428/12875
- IPC, 3
- B23K35 30
- B23K35 32
- C04B37 02