Engine start system with quadrature AC excitation

BACKGROUND OF THE INVENTION

0001The present invention relates to engine start systems and, more particularly, to engine start systems that may use a readily available constant frequency power source such as an auxiliary power unit (APU) or external ground power.

0002Using electric, brushless starter-generators for main engine start and for power generation can save aircraft weight and improve operating economics as part of the new more electric architecture (MEA) systems architectures. The starter-generator has to provide high starting torque to start the main engine. Conventional main engine starter-generator systems involve the use of high power inverters to provide a controllable variable frequency power source which adds cost, weight and complexity while decreasing the reliability of the system.

0003Many aircraft include starter-generator systems to supply relatively constant frequency AC power. Many of the starter-generator systems installed in aircraft include three separate brushless starter-generators, namely, a permanent magnet starter-generator (PMG), an exciter, and a main starter-generator. The PMG includes a rotor having permanent magnets mounted thereon, and a stator having a plurality of windings. When the PMG rotor rotates, the permanent magnets induce AC currents in PMG stator windings. These AC currents are typically fed to a regulator or a control device, which in turn outputs a DC current to the exciter.

0004The exciter typically includes single-phase (e.g., DC) stator windings and multi-phase (e.g., three-phase) rotor windings. The DC current from the regulator or control device is supplied to exciter stator windings, and as the exciter rotor windings that has a different number of poles or vice versa. This can lead to complexity in design and implementation.

0005<patcit id="pcit0001" dnum="US7064455B"><text>U.S. Patent No. 7,064,455 to Lando </text></patcit>employs rotor windings of the exciter and the main starter-generator disposed on the same primary shaft, with a permanent magnet starter-generator (PMG) disposed about an associated secondary shaft, for determining the rotational speed of the primary shaft. The rotors of the exciter and main starter-generator employ three-phase windings. However, this design offers no improvement over the complexity inherent in such three-phase windings.

0006European Patent No. <patcit id="pcit0002" dnum="EP1560317A2"><text>EP1560317A2</text></patcit> describes a synchronous electric machine having a rotor member and a stator member having a stator core. The electric machine further includes a main machine having a DC rotor field winding mounted on the rotor member and a dual AC/DC excitation system for the synchronous machine. The excitation system includes a rotatable polyphase armature winding in electrical communication with a rectifier assembly for conducting direct current to the rotor field winding of the main machine, and a plurality of DC salient poles and at least one AC salient pole, both included in the stator core. Respective AC salient poles of the at least one AC salient pole are disposed between adjacent DC salient poles of the plurality of DC salient poles. A plurality of DC field coils are disposed on respective DC salient poles of the plurality of DC salient poles, where the DC field coils are connected together to constitute at least one DC field winding. The at least one AC field coil is disposed respectively on the at least one AC salient pole. At least one AC field coil is connected together to constitute at least one alternate current field winding. A magnetic axis of respective AC field coils is disposed in electromagnetic space-quadrature relation with respect to magnetic axes of adjacent DC field coils. When the respective AC field coils are energized, an alternating current is induced in the polyphase armature winding for providing excitation to the main machine.

0007The patents mentioned above concern generation mode only and have no provision to be a starter. Hence, it can be seen that there is a need for a system and method of starting a main engine from a starter-generator that is relatively small, lightweight, less complex, and more reliable, as compared to current systems and methods, and that does not rely on specified numbers of exciter and main starter-generator poles.

SUMMARY OF THE INVENTION

0008The present invention in its various aspects is as set out in the appended claims. In one aspect of the present invention, an engine starting system comprises a main starter-generator having a main starter-generator rotor, the main starter-generator rotor having main starter-generator rotor windings wound thereupon; an exciter having an exciter rotor and an exciter stator, the exciter rotor having exciter rotor windings wound thereon; wherein the exciter rotor is configured to provide two phase excitation current to the main starter-generator rotor windings.

0009These two phase windings on either the exciter rotor, the main generator rotor, or both, may be configured to be shifted by a value chosen from a range of from 80 electrical degrees to 100 electrical degrees in time and space, with a choice of 90 windings that has a different number of poles or vice versa. This can lead to complexity in design and implementation.

0010<patcit id="pcit0003" dnum="US7064455B"><text>U.S. Patent No. 7,064,455 to Lando </text></patcit>employs rotor windings of the exciter and the main starter-generator disposed on the same primary shaft, with a permanent magnet starter-generator (PMG) disposed about an associated secondary shaft, for determining the rotational speed of the primary shaft. The rotors of the exciter and main starter-generator employ three-phase windings. However, this design offers no improvement over the complexity inherent in such three-phase windings.

0011Both patents mentioned above concern generation mode only and have no provision to be a starter. Hence, it can be seen that there is a need for a system and method of starting a main engine from a starter-generator that is relatively small, lightweight, less complex, and more reliable, as compared to current systems and methods, and that does not rely on specified numbers of exciter and main starter-generator poles.

SUMMARY OF THE INVENTION

0012In one aspect of the present invention, an engine starting system comprises a main starter-generator having a main starter-generator rotor, the main starter-generator rotor having main starter-generator rotor windings wound thereupon; an exciter having an exciter rotor and an exciter stator, the exciter rotor having exciter rotor windings wound thereon; wherein the exciter rotor is configured to provide two phase excitation current to the main starter-generator rotor windings. These two phase windings on either the exciter rotor, the main generator rotor, or both, may be configured to be shifted by a value chosen from a range of from 80 electrical degrees to 100 electrical degrees in time and space, with a choice of 90 choice of 90 electrical degrees being one exemplary embodiment. The connections between main rotor and exciter rotor windings can be made in the same phase sequence or opposite phase sequence.

0013In another aspect of the invention, an engine starting system comprises a shaft, wherein sufficient rotation of the shaft starts the engine; a main starter-generator stator with a plurality of main stator windings wound thereon; a main starter-generator rotor mounted on the shaft and disposed at least partially within the main starter-generator stator, the main starter-generator rotor having a plurality of main starter-generator rotor windings wound thereon to generate an air gap flux when they are electrically excited; an exciter rotor mounted on the shaft, the exciter rotor having a plurality of exciter rotor windings wound thereon; an exciter stator surrounding at least a portion of the exciter rotor, the exciter stator having a plurality of exciter stator windings wound thereon; and an exciter controller electrically coupled to the exciter stator windings, the exciter controller configured to provide electrical excitation to the exciter stator windings.

0014In still another aspect of the invention, an aircraft starter-generator system to start an aircraft gas turbine engine as the prime mover comprises a housing; a drive shaft rotationally mounted within the housing and transmitting power to the prime mover; a main starter-generator stator mounted within the housing and having a plurality of main starter-generator stator windings wound thereon; a main starter-generator rotor mounted on the drive shaft and disposed within the main starter-generator stator, the main starter-generator rotor having a plurality of main starter-generator rotor windings wound thereon configured to receive a two-phase excitation current, wherein the main starter-generator rotor windings generate an air gap flux upon electrical excitation thereof; an exciter rotor mounted on the drive shaft, the exciter rotor having a plurality of exciter rotor windings wound thereon, the exciter rotor windings electrically connected to the main starter-generator rotor; an exciter stator surrounding the exciter rotor, the exciter stator having a plurality of exciter stator windings wound thereon, the exciter stator windings configured, upon electrical excitation thereof, to electrically excite the exciter rotor windings, wherein interaction between currents in the main starter-generator rotor windings and the main starter-generator stator windings, which can be powered by a readily available constant frequency power source such as APU or external ground power, creates a starting torque to turn the shaft to start the engine, and voltage supplied to the exciter stator winding controls the current in the main starter-generator rotor and the starting torque. It will be also appreciated that the starter-generator described therein can provide starting torque to start an engine by powering the main stator windings only with a constant frequency power source without powering the exciter stator windings.

0015These and other features, aspects and advantages of the present invention will become better understood with reference to the following drawings, description and claims.

BRIEF DESCRIPTION OF THE DRAWINGS

0016<ul id="ul0001" list-style="none" compact="compact"><li><figref idref="f0001">FIG. 1</figref> is a functional block diagram of an exemplary high speed starter-generator system according to an embodiment of the present invention;</li><li><figref idref="f0002">FIG. 2</figref> is a functional block diagram of an exemplary high speed starter-generator system according to an alternative embodiment of the present invention;</li><li><figref idref="f0003">FIG. 3</figref> is a schematic representation of an embodiment of the high speed starter-generators of <figref idref="f0001">FIGS. 1</figref> and <figref idref="f0002">2</figref>;</li><li><figref idref="f0004">FIG. 4</figref> is a schematic representation of another embodiment of the high speed starter-generators of <figref idref="f0001">FIGS. 1</figref> and <figref idref="f0002">2</figref>; and</li><li><figref idref="f0005">FIG. 5</figref> is a flow chart describing a method according to the present invention.</li></ul>

DETAILED DESCRIPTION OF THE INVENTION

0017The following detailed description is of the best currently contemplated modes of carrying out the invention. The description is not to be taken in a limiting sense, but is made merely for the purpose of illustrating the general principles of the invention, since the scope of the invention is best defined by the appended claims.

0018Broadly, the present invention provides a system and methods that may use a readily available constant frequency power source, such as the APU or external ground power supply, to start the main engine of an aircraft. These systems and methods, together with intelligent excitation control and novel starter-generator design, may allow for tailoring of the torque-speed profile of the starter-generator. For example, in one embodiment of the present invention, the main starter-generator stator winding may be connected to a constant frequency (CF) power source to create a rotating field in the main starter-generator air gap. This flux, in turn, may induce current on the main rotor winding, which may be a closed circuit formed by main rotor field winding and exciter armature winding. The interaction between the main rotor current and the air gap flux may give rise to the starting torque to start the main engine. The voltage supplied to the exciter stator field winding may be adjusted to modify the induced voltage and current on the rotor circuit to control the rotor current and starting torque. The present invention may be useful to start a main engine of, for example, an aircraft, a ground vehicle, an industrial generator and the like.

0019A traditional synchronous wound rotor starter-generator typically has a single phase winding on the main rotor that creates a flux field that is locked to the rotor rotation. The present invention may create a rotor winding scheme using two phase windings that are in quadrature with each other and are controlled in a manner that allows the air gap flux to rotate at a speed that is synchronous with the stator power frequency. More specifically, the starter-generator described herein may employ the use of two-phase current to transfer energy from the exciter rotor to the main starter-generator rotor, whereas in the prior art, three-phase current is used between the exciter rotor and the main starter-generator rotor. By using two-phase instead of three-phase power transfer between the rotors, a simple winding scheme for the rotor poles can be used, with the phase windings being in quadrature with each other, which greatly reduces the complexity of the general construction of the starter-generator.

0020Turning now to the description and with reference first to <figref idref="f0001">FIG. 1</figref>, a functional schematic block diagram of an exemplary high speed starter-generator system 100 for use with, for example, an aircraft gas turbine engine, is shown. This exemplary starter-generator system 100 may include a permanent magnet starter-generator (PMG) 110, an exciter 120, a main starter-generator 130, and an exciter controller 140. It will be appreciated that the starter-generator system 100 may also include one or more additional components, sensors, or controllers. However, a description of these additional components, sensors, and controllers, if included, is not necessary for a description of the invention, and will therefore not be further depicted or described.

0021In the depicted embodiment, a PMG rotor 112 of the PMG 110, an exciter rotor 124 of the exciter 120, and a main starter-generator rotor 132 of the main starter-generator 130 may be mounted on a common drive shaft 150. The drive shaft 150 may provide a rotational drive force to a prime mover 160, such as an an aircraft gas turbine engine, which may cause the PMG rotor 112, the exciter rotor 124, and the main starter-generator rotor 132 to all rotate at the same rotational speed.

0022By connecting the windings of a main starter-generator stator 134 to a constant frequency (CF) power source (such as an APU or external power, not shown, but connect via a power line), a rotating field in an air gap of the main starter-generator 130 may be created. This air gap flux may induce current on the winding of the main starter-generator rotor 132. Interaction between the current in the winding of the main starter-generator rotor 132 and air gap flux may give rise to the starting torque to start the main engine (not shown) via the prime mover 160.

0023After engine start, the starter-generator system 100 may operate as a starter-generator. It will be appreciated that as the PMG rotor 112 rotates, the PMG 110 may generate and supply AC power to the exciter controller 140 from a PMG stator 114. In response, the exciter controller 140 may be electrically coupled to an exciter stator 122 of the exciter 120 to supply AC power to the exciter stator 122. In turn, this may induce the exciter rotor 124 to supply an induced alternating current to the main starter-generator rotor 132. As the main starter-generator rotor 132 rotates, it may induce AC current in a main starter-generator stator 134, which may be, in turn, supplied to one or more loads.

0024Before proceeding further, it will be appreciated that although the starter-generator system 100 described above is implemented with a PMG 110, the starter-generator system 100 could alternatively be implemented with other devices in place of the PMG 110, which respond to the rotational speed of the drive shaft 150. In such an alternative embodiment, as shown in <figref idref="f0002">FIG. 2</figref>, the starter-generator system 100 may include a speed sensor 202 rather than the PMG 110. The speed sensor 202, which may be implemented using any one of numerous types of rotational speed sensors, may be configured to sense the rotational speed of the drive shaft 150 and supply a speed signal (NCS) representative of the rotational speed of the drive shaft 150 to the exciter controller 140. The exciter controller 140 may use this speed signal NCS to modulate an energy source (not shown) that is independent of the starter-generator system 100, e.g. another generator associated with the prime mover but decoupled from the shaft or a battery-operated generator. Although the exciter controller 140 in this alternative embodiment may also supply AC power to the exciter stator 122, it may do so in response to the speed signal from the speed sensor 202 rather than in response to the AC power supplied from the PMG 110, the frequency of which may be indicative of the rotational speed of drive shaft 150. In yet another embodiment (not shown), the exciter controller 140 may use a frequency signal from main generator stator windings 404 to determine the correct input frequency to the exciter stator windings 406 to achieve the predetermined constant output frequency at the main generator 130. In all embodiments, however, it should be noted that the signal supplied to the exciter controller 140, regardless of whether it is the AC power signal from the PMG 110 or the speed signal from the speed sensor 202, may be representative of shaft rotational speed.

0025Referring now to <figref idref="f0003">FIG. 3</figref>, it may be seen, for example, that the exciter rotor 124 and the main starter-generator rotor 132 may be configured differently from conventional brushless AC starter-generator systems, and the exciter stator 122 and main starter-generator stator 134 may also be configured differently from conventional brushless AC generator systems. In particular, the exciter rotor 124 and the main starter-generator rotor 132 may be implemented with two phase exciter rotor windings 402 and two phase main rotor windings 408 respectively. These two phase windings may be configured to be shifted by a value in a range of from 80 electrical degrees to 100 electrical degrees in time and in space, with 90 electrical degrees being an exemplary amount (resulting in the phase windings being in quadrature with each other). Conversely, the exciter stator 122 may be implemented with three phase exciter stator windings 406 as shown in <figref idref="f0003">Fig. 3</figref> or two phase exciter stator windings 406 as shown in <figref idref="f0004">Fig. 4</figref>, while the main starter-generator stator 134 may be implemented with standard three phase main stator windings 404. It will be appreciated that core of the exciter stator 122 can be configured to use either slotted cylindrical poles or salient poles. Another difference from conventional brushless AC generator systems may be that there may be no rotating rectifier assemblies coupled between the exciter rotor 124 and the main rotor 132. Rather, the exciter rotor windings 402 may be directly coupled to the main rotor windings 408.

0026The exciter controller 140 may be implemented, at least in part, as a power converter circuit that is configured, in response to the signal supplied to it from either the PMG 110 or main starter-generator stator windings 404, to supply variable-frequency, three-phase excitation to the exciter stator windings 406, as shown in <figref idref="f0003">FIG. 3</figref>, with either a relatively positive or negative phase sequence or to supply a DC current in the synchronous operating mode. Alternatively, the exciter controller 140 may be implemented to supply variable frequency, two-phase excitation to the exciter stator windings 406, as shown in <figref idref="f0004">FIG. 4</figref>. In either case, the exciter rotor windings 402 may be configured to provide two phase excitation current to the main starter-generator rotor windings 408. These two phase windings are shifted by 90 electrical degrees in time and in space. It may be appreciated that relatively negative phase sequence excitation, as used herein, is excitation that is supplied in a direction opposite that which the exciter rotor 124 is rotating, and relatively positive sequence excitation, as used herein, is excitation that is supplied in a direction the same as which the exciter rotor 124 is rotating. It may be also appreciated that the exciter can be operating at three different modes, namely sub synchronous (negative phase sequence), super synchronous (positive phase sequence) and synchronous (DC current).

0027The excitation frequency and phase sequence that the exciter controller 140 may supply to the exciter stator windings 406 may depend upon the desired torque and rotational speed needed to turn the prime mover 160 in order to augment the main starter-generator stator 134. Alternatively, the exciter controller 140 may supply to the exciter stator windings 406 an excitation frequency and phase sequence to control the starting of the main engine (not shown) and avoid high in-rush current being generated in the main stator windings 404 and power supply units (not shown). In other words, the exciter controller 140 may control the phasing and frequency of the current in the exciter stator 122 to produce the appropriate prime mover 160 starting torque to meet the main engine start torque profile. This may eliminate the requirement for controlled power electronics to be supplied to the main starter-generator stator 134.

0028Referring now to <figref idref="f0005">Figure 5</figref>, the present invention may also include a method 500 for starting an aircraft engine. Such a method 500 may include, for example, a step 510 of creating a rotor winding scheme using two phase windings that are in quadrature with each other and are controlled in a manner that allows the air gap flux to rotate at a speed that is synchronous with the stator power frequency. The method may also include a step 520 for controlling the rotor flux speed by an exciter stator that induces a current in the rotor windings of appropriate amplitude, phasing and frequency. Furthermore, the methods of the present invention may also include a step 530 for controlling, with an electronic controller, for example, the phasing and frequency of the current in an exciter stator having a plurality of windings wrapped therearound, to produce the appropriate rotor starting current and starting torque to meet the main engine start torque profile requirements. It may be appreciated that a starter-generator with the configuration configuration described in this invention can also start a main engine or other type of loads by directly connecting its main stator windings 404 to a readily available CF power supply without exciting the exciter stator 122.

0029It should be understood, of course, that the foregoing relates to exemplary embodiments of the invention and that modifications may be made without departing from the scope of the invention as set forth in the following claims.