A hold open rod (36) has a control sleeve (46), an outer cylinder (42), lock balls (51), a lock sleeve (44), a piston (38), a piston head (40), a release spring (50), and a lock spring (48). The control sleeve (46) has first and second cavity sections (142, 144), an inner radial surface (150), a CS channel (148), and a pin (146). The outer cylinder (42) has an OC inner cavity (92), OC inner and outer radial surfaces (94, 96), an OC axial end wall (102), lock ball apertures (106), and a pin guide slot (108). The lock balls (51) are configured to pass through the lock ball apertures (106). The piston (38) has first and second sections (58, 60). The piston head (40) has an outer radial surface (78), a channel (80), and a piston bore (84). The piston bore (84) is configured to receive the first section (58) of the piston (38). The release spring (50) biases the control sleeve (46) toward a first axial end (54). The lock spring (48) biases the lock sleeve (44) toward a second axial end (56).
LOCK MECHANISM FOR TELESCOPIC HOLD OPEN ROD
VERRIEGELUNGSMECHANISMUS FÜR TELESKOPISCHE OFFENHALTESTANGE
MÉCANISME DE VERROUILLAGE POUR TIGE DE MAINTIEN EN POSITION OUVERTE TÉLESCOPIQUE
08.01.2025
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |