A removable closure member (50) configured to close a concave portion (40) received in an external opening (16b) formed in an external surface (16) of a nacelle (10) for an aircraft engine, the concave portion (40) including at least one air inlet opening (48). The closure member (50) comprises a base (51) forming an outer contour of the member and extending beyond an outer opening (16b) of the nacelle (10) so as to be moved against an outer surface (16) of the nacelle, and at least one elastically deformable position retaining member (56) for retaining the position of the nacelle (10). The at least one elastically deformable position retaining member protrudes from the base (51) and is configured to be inserted into the air inlet opening (48).

    一种可移除的封闭构件(50),该可移除的封闭构件被配置成封闭凹形部分(40),该凹形部分被接收在飞行器发动机用的短舱(10)的外部表面(16)中形成的外部开口(16b)中,该凹形部分(40)包括至少一个空气入口开口(48)。该封闭构件(50)包括基部(51)和至少一个可弹性变形的位置保持构件(56),该基部形成该构件的外部轮廓并且延伸超过该短舱(10)的外部开口(16b),以便移动成抵靠该短舱的外部表面(16),该至少一个可弹性变形的位置保持构件从该基部(51)突出并且被配置成插置到该空气入口开口(48)中。


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    Title :

    Removable closure member for concave portion received in external opening of aircraft nacelle


    Additional title:

    接收在飞行器发动机短舱的外部开口中的凹形部分用的可移除的封闭构件


    Contributors:

    Publication date :

    2022-11-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    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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