A removable closure member is configured to close a female portion received in an external opening formed in the external surface of a nacelle for an aircraft engine. The female portion includes at least one air inlet opening. The closure member includes a base that forms the external contour of the member and that extends beyond the external opening of the nacelle so as to move into abutment against the external surface of the nacelle. The closure member further includes at least one resiliently deformable position retention member that projects from the base and is configured to be inserted into the air inlet opening.
REMOVABLE CLOSURE MEMBER FOR A FEMALE PORTION RECEIVED IN AN EXTERNAL OPENING OF AN AIRCRAFT ENGINE NACELLE
2023-06-08
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Removable closure member for concave portion received in external opening of aircraft nacelle
European Patent Office | 2022
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