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    REMOVABLE BLIND FASTENER FOR NARROW APERTURES
    6.
    发明公开
    REMOVABLE BLIND FASTENER FOR NARROW APERTURES 有权
    ABNEHMBARER BLINDBEFESTIGERFÜRSCHMALEÖFFNUNGEN

    公开(公告)号：EP3011192A1

    公开(公告)日：2016-04-27

    申请号：EP14737330.2

    申请日：2014-06-18

    申请人： Kwikbolt Limited

    发明人： NIKLEWICZ, Jan ,  CARRAN, Dean

    IPC分类号： F16B19/10

    CPC分类号： F16B5/0258 ,  F16B13/063 ,  F16B19/1072 ,  F16B19/109 ,  F16B21/00

    摘要： The present invention provides a removable blind fastener (2) having a first tubular element (4) comprising an arm portion (22), a second tubular element (6) comprising an arm portion (28), and an elongate screw member (8). The elements (4 and 6) are arranged in telescoping relationship one with the other and which fastener (2), when in use as a temporary fastener, is caused to secure the component parts (10 and 12) of an airframe by causing telescoping movement of the elements (4 and 6) towards each other when the screw member (8) is turned in one direction and is caused to release the component parts (10 and 12) of the airframe by causing telescoping movement of the elements (4 and 6) away from each other when the screw member (8) is turned in an opposite direction. The arm portions (22, 28) of the elements (4 and 6) are located in mutual juxtaposition for telescoping movement upon rotation of the screw member (8) as aforesaid with end portions (30a and 32a) of elongate arms (30 and 32) of the arm portions (22 and 28) being brought into engagement with a tapered portion (44) of the screw (8) whereby the arms (30 and 32) are caused to splay outwardly to bring the end portions (30a and 32a) into engagement with an underside (126) of the component (12) and moving the component (12) into secure temporary relationship with the component (10) of the airframe.

    摘要翻译： 本发明提供了一种具有包括臂部分（22）的第一管状元件（4）和包括臂部分（28）的第二管状元件（6）和细长螺钉构件（8）的可拆卸盲链扣件（2） 。 元件（4和6）与另一个以伸缩关系布置，并且当用作临时紧固件时，通过引起伸缩运动使紧固件（2）固定在机身的部件（10和12）上 当螺钉构件（8）沿一个方向转动并且通过使元件（4和6）的伸缩运动而被释放时，元件（4和6）彼此朝向彼此 ）当螺杆构件（8）沿相反方向转动时彼此远离。 元件（4和6）的臂部分（22,28）位于相互并列的位置，用于当如上所述旋转螺杆构件（8）时伸缩运动，伸长臂（30和32）的端部（30a和32a） 的臂部（22和28）与螺钉（8）的锥形部分（44）接合，从而使臂（30和32）向外张开以使端部（30a和32a） 与部件（12）的下侧（126）接合并将部件（12）移动到与机身的部件（10）的安全的临时关系中。

    WET-FIT FASTENER
    9.
    发明公开
    WET-FIT FASTENER 审中-公开

    公开(公告)号：EP3491256A1

    公开(公告)日：2019-06-05

    申请号：EP17758277.2

    申请日：2017-07-24

    申请人： Kwikbolt Limited

    发明人： NIKLEWICZ, Jan ,  CARRAN, Dean

    IPC分类号： F16B13/08 ,  F16B19/10

    摘要： A dowelling fastener 200 has a head end and an insertion end and a cylindrical dowelling portion 201. The fastener is provided with a plunger 201 at the insertion end for clearing material from a hole as the fastener 200 is inserted into the hole. The plunger 204 may be rigid and has a circular cross section with a diameter substantially the same as the dowelling portion 201 of the fastener, the plunger thereby being a close fit with the hole.

    REMOVABLE BLIND FASTENER FOR NARROW APERTURES
    10.
    发明授权
    REMOVABLE BLIND FASTENER FOR NARROW APERTURES 有权

    公开(公告)号：EP3011192B1

    公开(公告)日：2018-07-25

    申请号：EP14737330.2

    申请日：2014-06-18

    申请人： Kwikbolt Limited

    发明人： NIKLEWICZ, Jan ,  CARRAN, Dean

    IPC分类号： F16B19/10

    CPC分类号： F16B5/0258 ,  F16B13/063 ,  F16B19/1072 ,  F16B19/109 ,  F16B21/00

    摘要： The present invention provides a removable blind fastener (2) having a first tubular element (4) comprising an arm portion (22), a second tubular element (6) comprising an arm portion (28), and an elongate screw member (8). The elements (4 and 6) are arranged in telescoping relationship one with the other and which fastener (2), when in use as a temporary fastener, is caused to secure the component parts (10 and 12) of an airframe by causing telescoping movement of the elements (4 and 6) towards each other when the screw member (8) is turned in one direction and is caused to release the component parts (10 and 12) of the airframe by causing telescoping movement of the elements (4 and 6) away from each other when the screw member (8) is turned in an opposite direction. The arm portions (22, 28) of the elements (4 and 6) are located in mutual juxtaposition for telescoping movement upon rotation of the screw member (8) as aforesaid with end portions (30a and 32a) of elongate arms (30 and 32) of the arm portions (22 and 28) being brought into engagement with a tapered portion (44) of the screw member (8) whereby the arms (30 and 32) are caused to splay outwardly to bring the end portions (30a and 32a) into engagement with an underside (126) of the component (12) and moving the component (12) into secure temporary relationship with the component (10) of the airframe.