An assistance device is provided to maneuver of a cover of a nacelle of a turbojet engine. The assistance device includes a joint collinear with an existing joint or hinge for a fitting of the cover, and the joint of the device is rigidly secured to an angled part of which one end bears on the fitting of the cover and of which one point is hinged to a compression spring in order to apply assistance momentum to the fitting of the cover when the cover is raised.
ASSISTANCE DEVICE FOR OPERATING A COWL AND A NACELLE FOR TURBOJET ENGINE EQUIPPED THEREWITH
2016-04-14
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / E05D Scharniere oder andere Aufhängevorrichtungen für Türen, Fenster oder Flügel , HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS, OR WINGS / E05F DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION , Vorrichtungen zum Bewegen der Flügel in die Offen- oder Schließstellung / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES |
TURBOJET NACELLE EQUIPPED WITH NACELLE COMPONENT COOLING ASSY
European Patent Office | 2015
|NACELLE FOR AN AIRCRAFT TURBOJET ENGINE WITH HYBRID AIR INLET AND FAN COWL
European Patent Office | 2019
|Nacelle for an aircraft turbojet engine with hybrid air inlet and fan cowl
European Patent Office | 2020
|