A latch pin actuator (600) comprises a primary lock (702) having a curvature (712) configured to allow a latch pin (602) into a housing (604) when the primary lock (702) is in an unlocked position, and wherein the primary lock (702) is configured to prevent the latch pin (602) from entering a housing (604) in a locked position, by facing the curvature (712) in a different direction in the locked position, a spring (706) and a piston (710). The primary lock (702) is attached to a primary lock cam (608) and has a notch (716) as a fracture evident geometry. The spring (706) is biased to lock the primary lock (702). The piston (710) is configured to unlock the primary lock (702).
FOLDING WING SYSTEM
KLAPPFLÜGELSYSTEM
SYSTÈME D'AILE PLIABLE
2020-08-19
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |