FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft propeller electrical drives. Aircraft electrical drive (1), particularly, for helicopter (20) with at least one rotor (23) driven by dynamoelectric dual-type machine (2). Rotor (6) is arranged in air gap (12) and contains permanent magnets (13) at support (14). Note here that stators (4, 5) of said dynamoelectric machine (2) and/or rotor (6) includes cooling means. Planetary gear (3) is located in axial direction of dynamoelectric machine (2), between said rotor and said machine. Said dynamoelectric machine (2) and said planetary gear (3) are located in common housing and included common support (7) arranged there between. Support (14) of rotor (6) represents a composite design and is shaped to a bell. At least one stator (4, 5) includes oil cooling circuit. Note here that said oil circuit lubes both stator (4, 5) and said planetary gear (3).
EFFECT: higher efficiency.
6 cl, 2 dwg
| Title |
Year |
Author |
Number |
| HELICOPTER ANTI-TORQUE ROTOR |
2011 |
- Khamann Jens
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- Shtojber Ditmar
|
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|
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2020 |
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|
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|
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|
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2020 |
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|
RU2739753C1 |
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2019 |
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- Turchi, Thomas
|
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2009 |
|
RU2510559C2 |
| ELECTROMAGNETIC DEVICE WITH REVERSIBLE GENERATOR AND MOTOR OPERATION |
2009 |
|
RU2516373C2 |
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2020 |
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|
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