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Fastener for aircraft cowlings, doors, fittings, and the like, applicable to aircraft, sheet-metal and appropriate industries

机译:飞机整流罩,门,配件等的紧固件,适用于飞机,钣金及相关行业

摘要

548,658. Fastenings. MILLER, H. A. April 10, 1941, No. 4761. Addition to 541,278. [Class 44] Two panels &c. S, T are fastened together by a stud B with a T-head which is passed through the panels and washers, and then through a wire spring member F supported on T, after which the stud is turned through 90 degrees to engage lateral extensions of the spring, as described in the parent Specification. The spring F may be mounted in a floating manner by coiling it around ferrules N' on rivets N' carried by T, and an ejector spring P may be mounted on the stud to move it out when the fastening is undone, as in Fig. 17. The spring F may have various forms.
机译:548,658。紧固件。 MILLER,H.A.,1941年4月10日,编号4761。增加541,278。 [Class 44]两个面板&c。 S,T由带有T形头的双头螺栓B固定在一起,该T形头穿过面板和垫圈,然后穿过支撑在T上的钢丝弹簧F,然后将双头螺栓旋转90度,以接合其横向延伸。弹簧,如父规范中所述。弹簧F可以通过将其绕在由T承载的铆钉N'上的套圈N'上盘绕而以浮动方式安装,并且弹出弹簧P可以被安装在双头螺栓上以在松开紧固时将其移出,如图2所示。 17.弹簧F可以具有各种形式。

著录项

  • 公开/公告号GB548658A

    专利类型

  • 公开/公告日1942-10-19

    原文格式PDF

  • 申请/专利权人 HENRY ARTHUR MILLER;

    申请/专利号GB19410004761

  • 发明设计人

    申请日1941-04-10

  • 分类号B21D11/06;F16B5/10;

  • 国家 GB

  • 入库时间 2022-08-24 04:00:51

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