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DUAL-FLOW TURBOJET ENGINE FOR AN AIRCRAFT WITH AN OPENING PROVIDED WITH A HINGE WITH GOOSENECK FITTING
DUAL-FLOW TURBOJET ENGINE FOR AN AIRCRAFT WITH AN OPENING PROVIDED WITH A HINGE WITH GOOSENECK FITTING
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机译:双流涡轮喷气发动机,带开口的带有鹅颈管接头的带开口的飞机
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摘要
A bypass turbojet engine comprising a fixed structure, a central core and a cowl comprising a fixed part and a mobile cowl mounted with the ability to rotate on the fixed structure between a closed position and an open position via hinges with gooseneck fitting. At least one hinge with gooseneck fitting comprises a gooseneck fitting having one end mounted in articulated manner on the mobile cowl and one end mounted in an articulated manner on the fixed structure, the bypass turbojet engine comprises anti-vibration means which are configured to exert pressure against the gooseneck fitting when the mobile cowl is in the closed position.
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