Aircraft power generating assembly
View Patent ↗An aircraft power generating assembly having a mechanical gear transmission, and an electric machine integrated in the mechanical transmission; the electric machine having a stator connected directly to a fixed frame of the mechanical transmission, and a rotor surrounding and rotated by a rotary shaft of the mechanical transmission; and the opposite ends of the rotary shaft being connected to respective further rotary input/output shafts.
1. An aircraft power generating assembly comprising an electric machine, and a mechanical gear transmission connected to said electric machine; the mechanical gear transmission comprising a fixed supporting frame, at least one rotary shaft connected to the fixed supporting frame to rotate about a fixed axis, and first and second connector assemblies rotating with and connecting said at least one rotary shaft to respective further rotary input/output shafts; wherein said electric machine is located between said first and second connector assemblies, surrounds said at least one rotary shaft, and is releasably connectable to said at least one rotary shaft by a releasable coupling movable axially along said at least one rotary shaft between connected and released positions.
2. The aircraft power generating assembly as claimed in claim 1 , wherein said electric machine comprises a hollow rotor fitted to said at least one rotary shaft.
3. The aircraft power generating assembly as claimed in claim 2 , wherein said rotor loosely surrounds said at least on rotary shaft; and a bearing assembly is interposed directly between said rotor and said at least one rotary shaft.
4. The aircraft power generating assembly as claimed in claim 2 , wherein the releasable coupling is releasably interposed as a direct drive element between said hollow rotor and said at least one rotary shaft.
5. The aircraft power generating assembly as claimed in claim 1 , wherein said electric machine comprises a hollow rotor surrounding said at least one rotary shaft and fitted to said fixed supporting frame.
6. The aircraft power generating assembly as claimed in claim 2 , wherein said hollow rotor surrounds said at least one rotary shaft, and further includes a separate supporting structure; an additional bearing assembly being interposed between said separate supporting structure and said fixed supporting frame.
7. The aircraft power generating assembly as claimed in claim 6 , further comprising an interface frame interposed between said fixed supporting frame and said additional bearing assembly.
8. The aircraft power generating assembly as claimed in claim 7 , wherein the releasable coupling is interposed between said fixed supporting frame and said interface frame.
9. The aircraft power generating assembly as claimed in claim 7 , wherein the releasable coupling is interposed as a direct drive element between said at least one rotary shaft and said separate supporting structure.
10. The aircraft power generating assembly as claimed in claim 1 , wherein said electric machine comprises a stator connected to said fixed supporting frame.
11. The aircraft power generating assembly as claimed in claim 10 , wherein said fixed supporting frame defines a closed outer casing; and said at least one rotary shaft, said stator, and said rotor are housed in said closed outer casing.
12. The aircraft power generating assembly as claimed in claim 1 , wherein said second connector assembly connects said at least one rotary shaft directly to a shaft of a propulsion system of the aircraft.
13. The aircraft power generating assembly as claimed in claim 1 , wherein said second connector assembly connects said at least one rotary shaft to at least one accessory device of the aircraft.
14. The aircraft power generating assembly as claimed in claim 1 , wherein the electric machine is convertible to operate both as an electric power generator and as a drive motor.
15. An aircraft power generating assembly comprising an electric machine, and a mechanical gear transmission connected to said electric machine; the mechanical gear transmission comprising a fixed supporting frame, at least one rotary shaft connected to the fixed supporting frame to rotate about a fixed axis, and first and second connector assemblies rotating with and connecting said at least one rotary shaft to respective further rotary input/output shafts; wherein said electric machine is located between said first and second connector assemblies, surrounds said at least one rotary shaft, and is releasably connectable to said at least one rotary shaft, said electric machine comprises a hollow rotor fitted to said at least one rotary shaft, and said hollow rotor surrounds said at least one rotary shaft, and further includes a separate supporting structure with an additional bearing assembly being interposed between said separate supporting structure and said fixed supporting frame.
16. The aircraft power generating assembly as claimed in claim 15 , further comprising an interface frame interposed between said fixed supporting frame and said additional bearing assembly.
17. The aircraft power generating assembly as claimed in claim 16 , further comprising a releasable connector interposed between said fixed supporting frame and said interface frame.
18. The aircraft power generating assembly as claimed in claim 17 , further comprising a releasable connector interposed as a direct drive element between said at least one rotary shaft and said separate supporting structure.