The invention provides a helicopter tail output reducing flange. By optimal design in structure, the tail output reducing flange has functions of a tail rotor hub for mounting and fixing a tail blade, functions of the tail rotor hub in the prior art are realized through a flange plate of the tail output reducing flange and optimal design on an outer cover plate, system structure of the tail rotor hub is simplified, overall size of the hub system is reduced, overall weight of the hub system is reduced, and reliability of the system is improved.
Helicopter tail output reducing flange
2015-09-09
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
A SYSTEMATIC APPROACH TO REDUCING HELICOPTER TAIL DRIVE SHAFT MAINTENANCE
British Library Conference Proceedings | 2013
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