A torque limiting device (24) comprises an input shaft (56), an output shaft (50) and a machined torsion spring (80) having a first end (82) and a second end (84). The first end (82) and the second end (84) of the torsion spring (80) are coupled to the both the input shaft (56) and the output shaft (50), whereby torque is transmitted between the input shaft (56) and output shaft (50) via the torsion spring (80). The couplings between the torsion spring (80) and the input shaft (56) and the output shaft (50) permit limited relative rotation between the input shaft (56) and the output shaft 50). The device further comprises a jamming mechanism (78) operable in response to relative rotation between the input shaft (56) and output shaft (50) to stop rotation of both the input shaft (56) and the output shaft (50).
УСТРОЙСТВО ДЛЯ ОГРАНИЧЕНИЯ КРУТЯЩЕГО МОМЕНТА
17.09.2018
Patent
Elektronische Ressource
Russisch
IPC: | B64C AEROPLANES , Flugzeuge |
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