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.
ORGANE D'OBTURATION AMOVIBLE POUR UNE PARTIE FEMELLE LOGEE DANS UNE OUVERTURE EXTERIEURE D'UNE NACELLE DE MOTEUR D'AERONEF
REMOVABLE CLOSURE BODY FOR A FEMALE PART HOUSED IN AN EXTERIOR OPENING OF AN AIRCRAFT ENGINE NACELLE
ABNEHMBARE SCHLIESSELEMENT FÜR EINEN WEIBLICHEN TEIL DER IN EINER AUSSEREN ÖFFNUNG EINER FLUGZEUGTRIEBWERKSGONDEL UNTERGEBRACHT IST
2024-01-31
Patent
Electronic Resource
French
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS |
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