Aircraft engine assembly and method of generating electric energy for an aircraft power system
US-2016348589-A1 · Dec 1, 2016 · US
US11519336B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11519336-B2 |
| Application number | US-202017016711-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 10, 2020 |
| Priority date | Aug 12, 2014 |
| Publication date | Dec 6, 2022 |
| Grant date | Dec 6, 2022 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
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. An accessory gearbox assembly, comprising: an accessory gearbox including a drive gear configured to transmit and receive rotational energy from a gas turbine engine; and a starter-generator module connected to the accessory gearbox, including: an inner stator with an armature defining a rotation axis; an outer rotor with a permanent magnet disposed about the rotation axis; and wherein the outer rotor is operatively connected to transmit rotational energy to the accessory gearbox through the drive gear in a start mode and receive rotational energy from the accessory gearbox through the drive gear in a generate mode, where the armature includes a radially inner yoke portion connected to a plurality of radially outer teeth, further including phase windings wrapped about at least two of the plurality of radially outer teeth, wherein the phase windings extend in parallel with the rotation axis, further including a control coil disposed circumferentially between the phase windings. 2. The accessory gearbox assembly as recited in claim 1 , wherein the drive gear is a first drive gear and wherein the accessory gearbox further includes a second drive gear operatively associated with the first drive gear and engaged with the outer rotor and a gear train of the accessory gearbox. 3. The accessory gearbox assembly as recited in claim 1 , wherein the permanent magnet includes an annular array of permanent magnet elements with circumferentially alternating poles. 4. The accessory gearbox assembly as recited in claim 1 , wherein a rotor portion is at least one of a windingless rotor portion and a currentless rotor portion. 5. The accessory gearbox assembly as recited in claim 1 , wherein the control coil is disposed radially outward from the phase coils. 6. The accessory gearbox assembly 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. 7. The accessory gearbox assembly as recited in claim 1 , wherein the starter-generator module includes only a single electrical machine. 8. The accessory gearbox assembly as recited in claim 1 , wherein the accessory gear box includes a gear teeth member defined on the outer rotor, wherein the gear teeth member is configured to transmit rotational energy to the accessory gearbox in a start mode and to receive rotational energy from the accessory gearbox in a generate mode. 9. The accessory gearbox assembly as recited in claim 8 , wherein the gear teeth member includes gear teeth facing radially outward from the rotation axis. 10. The accessory gearbox assembly as recited in claim 8 , 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. 11. The accessory gearbox assembly as recited in claim 10 , further including phase leads and control coil leads extending through a 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.
Arrangement, mounting, or driving, of auxiliaries · CPC title
Mechanical drives · CPC title
Machine of the outer rotor type · CPC title
radially supporting the rotary shaft at both ends of the rotor (H02K7/086, H02K7/09 take precedence) · CPC title
structurally associated with turbines or similar engines · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.