FIELD: aviation.
SUBSTANCE: device (3) for aircraft (1) emergency power supply device comprises at least one air intake duct (5), a turbine (25) and at least one energy generating device (31) for the aircraft. The air intake duct (5) is designed in such a way that it ensures reception of the relative wind V during the aircraft flight. The turbine (25) is located in the mentioned duct (5) so that it can be driven by the relative wind V and is connected to the mentioned generating device (31).
EFFECT: invention reduces the weight of the aircraft.
9 cl, 1 dwg
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|
RU2646695C2 |
| AIRCRAFT | 2018 |
|
RU2706760C1 |
