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MECANISME BISTABLE POUR PORTE D'AERONEF
Aircraft door designed to assume a first configuration and a second configuration, having a bistable mechanism biasing the aircraft door towards either the first or second configuration, the bistable mechanism including: a first yoke having a base attached to the first member and a first pivot rotatably mounted on the bas; a second yoke having: a base attached to the first member; a lever a first end of which is mounted so as to pivot on the base; a second pivot mounted so as to rotate on the second end of the lever; a coupling device for coupling the lever to the second member of the door; an arch which can be elastically deformed by bending and a first end of which is attached to the first pivot and a second end attached to the second pivot.
MECANISME BISTABLE POUR PORTE D'AERONEF
Aircraft door designed to assume a first configuration and a second configuration, having a bistable mechanism biasing the aircraft door towards either the first or second configuration, the bistable mechanism including: a first yoke having a base attached to the first member and a first pivot rotatably mounted on the bas; a second yoke having: a base attached to the first member; a lever a first end of which is mounted so as to pivot on the base; a second pivot mounted so as to rotate on the second end of the lever; a coupling device for coupling the lever to the second member of the door; an arch which can be elastically deformed by bending and a first end of which is attached to the first pivot and a second end attached to the second pivot.
MECANISME BISTABLE POUR PORTE D'AERONEF
BISTABLE MECHANISM FOR AN AIRCRAFT DOOR
BISTABILER MECHANISMUS FÜR EINE FLUGZEUGTÜR
DEVILLEZ SÉBASTIEN (author)
2025-01-01
Patent
Electronic Resource
French