The present disclosure relates to a gear set, especially for a rotary-wing aircraft, with two intermeshing gear wheels, each mounted on a respective shaft. In particular, in a normal section, the gear wheels of the gear set have different pressure angles on a drive side from the pressure angles on a freewheel side at the beginning of an engagement.
Gearwheel set, in particular for a gyroplane
2018-11-06
Patent
Electronic Resource
English
Engineering Index Backfile | 1938
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|Engineering Index Backfile | 1938
|Engineering Index Backfile | 1937