The present embodiments relate to an aircraft door 104, and, more particularly, to an electromechanical door system 200 for operating an aircraft door 104 that closes an opening in the outer hull 102 of an aircraft 100, as well as to a method of operating an electromechanical door system 200 of an aircraft door 104 that closes an opening in the outer hull 102 of an aircraft 100. The electromechanical door system 200 may be adapted for operating in a normal opening mode, an emergency opening mode, and a closing mode. If desired, the electromechanical door system 200 may include a lifting and lowering lever 210, a lifting and lowering electric motor 215, and a gearbox 218 that transmits a force from the lifting and lowering electric motor 215 to the lifting and lowering lever 210.
AIRCRAFT WITH AN ELECTROMECHANICAL DOOR SYSTEM
FLUGZEUG MIT EINEM ELEKTROMECHANISCHES TÜRSYSTEM
AÉRONEF AVEC UN SYSTÈME DE PORTE ÉLECTROMÉCANIQUE
2023-06-07
Patent
Electronic Resource
English
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