Systems and methods are provided for an aircraft propulsor (108) with a fan cowl with one or more tangential restraints. The tangential restraints may be configured to contact one or more tangential receiving portions of a fixed portion of the aircraft propulsor (108). The fan cowl may receive a load that may include a bending load. The tangential restraints may be configured to convert the bending load to membrane tension and thus decrease deflection of the fan cowl.
NACELLE FAN COWL TANGENTIAL RESTRAINT
TANGENTIALSTÜTZE EINER TRIEBWERKSGONDELFANHAUBE
SUPPORT TANGENTIEL DE CAPOT DE SOUFFLANTE D'UNE NACELLE
2019-11-20
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |