Aircraft engine assembly and method of generating electric energy for an aircraft power system
US-2016348589-A1 · Dec 1, 2016 · US
US10787967B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10787967-B2 |
| Application number | US-201414457798-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 12, 2014 |
| Priority date | Aug 12, 2014 |
| Publication date | Sep 29, 2020 |
| Grant date | Sep 29, 2020 |
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A starter-generator module for a gas turbine engine includes an inner stator portion with an armature defining a rotation axis and an outer rotor portion disposed about the rotation axis. The outer rotor portion includes a permanent magnet and a gear teeth member. The permanent magnet is disposed about the rotation axis and the gear teeth member is defined on the outer rotor portion such that the gear teeth member transmits rotational energy to an accessory gearbox in a start mode and receives rotational energy from the accessory gearbox in a generate mode.
Opening claim text (preview).
What is claimed is: 1. A starter-generator module for a gas turbine engine, comprising: an inner stator portion with an armature defining a rotation axis, where the armature includes a radially inner yoke portion connected to a plurality of radially outer teeth; an outer rotor portion with a permanent magnet disposed about the rotation axis; a gear teeth member defined on the outer rotor portion, wherein the gear teeth member is configured to transmit rotational energy to an accessory gearbox in a start mode and to receive rotational energy from the accessory gearbox in a generate mode; phase windings wrapped about at least two of the plurality of radially outer armature teeth; and a control coil disposed circumferentially between the phase windings; wherein the inner stator portion extends through the gear teeth member, wherein the outer rotor portion is rotationally supported from the inner stator portion with a set of axially spaced apart bearings, wherein the gear teeth member is axially between the axially spaced apart bearings. 2. A starter-generator module as recited in claim 1 , wherein the gear teeth member includes gear teeth facing radially outward from the rotation axis. 3. A starter-generator module as recited in claim 1 , wherein the permanent magnet includes an annular array of permanent magnet elements with circumferentially alternating poles. 4. A starter-generator module as recited in claim 1 , wherein the rotor portion is at least one of a windingless rotor portion and a currentless rotor portion. 5. A starter-generator module as recited in claim 1 , further including a starter-generator static housing disposed radially outward of the gear teeth member, wherein teeth of the gear teeth member are oriented radially outward with respect to the rotation axis. 6. A starter-generator module as recited in claim 1 wherein the phase windings extend in parallel with the rotation axis. 7. A starter-generator module as recited in claim 1 , wherein the control coil is disposed radially outward from the phase windings. 8. A starter-generator module as recited in claim 1 , wherein the control coil extends in parallel with the rotation axis and along a portion of the length of the phase windings. 9. A starter-generator module as recited in claim 1 , further including phase leads and control coil leads extending through the radially inner yoke portion, wherein the phase leads are electrically connected to the phase windings the control lead is electrically connected to the control coil. 10. A starter-generator module as recited in claim 1 , wherein the starter-generator module includes only a single electrical machine. 11. The starter-generator module as recited in claim 1 , wherein the starter-generator module includes no exciter. 12. The starter-generator module as recited in claim 1 , wherein the starter-generator includes no sub-exciter.
Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user ({F02C3/107 - F02C3/13 and} F02C7/32 take precedence; couplings for transmitting rotation F16D; gearing in general F16H) · CPC title
with gears · CPC title
Machine of the outer rotor type · CPC title
structurally associated with turbines or similar engines · CPC title
radially supporting the rotary shaft at both ends of the rotor (H02K7/086, H02K7/09 take precedence) · CPC title
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