The invention relates to a method for locking a mobile element (101) of an aircraft, such as a hold door or a landing gear, the mobile element being moved between a deployed position and a closed or retracted position by means of an actuator (200) having a sliding stem (3) coupled to the mobile element, the stem being mounted so as to be able to slide in a body (1) of the actuator between an extended position corresponding to the deployed position of the mobile element and a withdrawn position corresponding to the closed or retracted position of the mobile element. The method of the invention comprises the step of positively blocking the sliding stem of the actuator in the withdrawn position.
PROCEDE DE MANŒUVRE DE TRAPPES DE SOUTES D'AERONEF, ET ACTIONNEUR FAISANT APPLICATION
02.02.2018
Patent
Elektronische Ressource
Französisch
IPC: | B64C AEROPLANES , Flugzeuge |
PROCÉDÉ DE MANOEUVRE DE TRAPPES DE SOUTES D'AÉRONEF, ET ACTIONNEUR FAISANT APPLICATION
Europäisches Patentamt | 2016
|ATTERRISSEUR D'AÉRONEF À ACTIONNEUR DE MANOEUVRE ROTATIF
Europäisches Patentamt | 2019
|ATTERRISSEUR D’AERONEF A ACTIONNEUR DE MANŒUVRE ROTATIF
Europäisches Patentamt | 2018
|DISPOSITIF D'ATTELAGE D'UN ACTIONNEUR DE MANOEUVRE D'UN ATTERRISSEUR D'AERONEF
Europäisches Patentamt | 2016
|Europäisches Patentamt | 2023
|