TRANSMISSION SYSTEM FOR AVIATION POWER
A transmission system for an aircraft powerplant includes a transmission shaft (1), where an input end of the transmission shaft is sleeved with a driven gear (2), one end of the driven gear is axially limited, and the other end of the transmission shaft is configured to connect a rotating member; a...
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Format: | Patent |
Sprache: | eng ; fre ; ger |
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Zusammenfassung: | A transmission system for an aircraft powerplant includes a transmission shaft (1), where an input end of the transmission shaft is sleeved with a driven gear (2), one end of the driven gear is axially limited, and the other end of the transmission shaft is configured to connect a rotating member; an end of the driven gear is in transmission connection with a stop hub (5), the stop hub is in transmission connection with an overload clutch (6), the overload clutch is in transmission connection with the transmission shaft, an end of the overload clutch away from the stop hub abuts against one end of a disc spring member (7), the other end of the disc spring member is axially limited, and a force value of the overload clutch is a fixed value; and an end face of the driven gear facing the stop hub is provided with a protruding claw A, an end of the stop hub is provided with a protruding claw B matching the protruding claw A, and the stop hub and the driven gear are in transmission through the matching between the protruding claws. The transmission system for an aircraft powerplant can further protect the transmission shaft, avoid the risk of fracture of the transmission shaft, and also protect other parts of the transmission system. |
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