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Improved means for assisting the landing of aircraft on the deck of an aircraft carrier

机译:协助飞机降落在航空母舰甲板上的改进手段

摘要

605,030. Aircraft arrester gear. FAIREY AVIATION CO., Ltd., and CHAPLIN, H. E. Dec. 12, 1945, No. 33663. [Class 4] Means for assisting the landing of an aircraft on the deck of a carrier comprises a strut f capable of being projected downwardly from the nose a of the aircraft, to engage a crash barrier wire, and a hook-like member u to prevent the wire from riding over the nose of the aircraft. The strut carries a deckengaging roller at its forward end, and pairs of rollers g, h, disposed respectively at the rear end and forward thereof, for engagement with channel shaped guides b, c along which the strut is projected and retracted. The portions b of the guides are horizontal, while portions c are inclined forwardly and downwardly, the rollers h moving along the latter to bring the strut into its operative position, the rollers g then engaging pockets d at the junction of the guide portions. Operating mechanism for the strut consists of toggle links m, n connected by a spring q to a bell-crank lever r, s and link t, the latter of which is connected to the undercarriage operating mechanism, whereby the strut is projected when the undercarriage is lowered. The hook-like member u is moved into its operative position by the projection of the strut, and is formed with a lug z which is engaged by the roller j during retraction of the strut to return the hook to the inoperative position. A spring link x is connected to the hook member in such a way that it passes through dead-centre positions when the hook moves into the operative, and returns to the inoperative position. The strut may be retracted manually with the undercarriage in the extended position, the spring q permitting the necessary lost-motion between the toggle links m, n, and the bell-crank r, s.
机译:605030。飞机避雷器齿轮。 FAIREY AVIATION CO。,Ltd.和CHAPLIN,HE,1945年12月12日,编号33663。[第4类]辅助飞机降落在航母甲板上的装置包括可从以下位置向下突出的支柱f飞机的机头a与防撞金属丝接合,钩状部件u用来防止金属丝越过飞机的机头。支杆在其前端处带有拉紧辊,以及分别设置在其后端和前部的成对的辊对g,h,以与支杆沿其伸出和缩回的槽形导向件b,c接合。导向器的部分b是水平的,而部分c是向前和向下倾斜的,辊子h沿着后者移动以将支杆带入其工作位置,然后辊子g在导向器部分的接合处接合凹穴d。撑杆的操纵机构包括肘节连杆m,n,该连杆通过弹簧q连接到曲柄杆r,s和连杆t,连杆t连接到起落架操纵机构,从而当起落架起步时,撑杆伸出被降低。钩状构件u通过支柱的突出而移动到其工作位置,并且形成有凸耳z,该凸耳z在支柱缩回期间由滚子j接合,以将钩返回到不工作位置。弹簧连杆x以这样的方式连接到钩构件:当钩移入工作位置时,弹簧连杆x穿过死点位置,并返回到不工作位置。可以在底盘处于伸出位置的情况下手动缩回支杆,弹簧q允许肘节连杆m,n和曲柄r,s之间必要的空行程。

著录项

  • 公开/公告号GB605030A

    专利类型

  • 公开/公告日1948-07-14

    原文格式PDF

  • 申请/专利号GB3366345A

  • 发明设计人

    申请日1945-12-12

  • 分类号B64C25/68;

  • 国家 GB

  • 入库时间 2022-08-24 02:38:36

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