A blade pitch actuation mechanism comprising a rotating race member in which is formed a race configured to receive a trunnion pin attached to a blade, whereby the race defines a cam profile such that rotation of the race member causes the trunnion pin received in the race to rotate as it slides over the cam profile.
BLADE PITCH ACTUATION MECHANISM
2021-09-16
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |