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POST FOUNDATION

机译:成立后

摘要

One embodiment is an earth penetrating apparatus with foldable, lockable wings. The apparatus includes a frame consisting of a tube (1), fixed steering fins (2) and fastening plates (7). Wings consisting of a reinforcement (9) and a blade (12) are attached to the fastening plates (7) with a bolt (10) and nut (1 1) to create a hinge joint, making the wings foldable. A locking- and wedge-piece (14) attached to a rod (15) is placed inside the frame tube (1 ), and an end cap (17) is fitted to the upper end of the frame tube (1). The rod (15) and end cap (17) are locked together by a nut (18) and a key- wedge (19), creating a wing locking mechanism. The wing locking mechanism is released by removing the nut (18) and replacing the end cap (17) with a hit cap (20). When deployed in a horizontal position the wings provide a large area that resists sinkage.
机译:一个实施例是一种具有可折叠的,可锁定的翼的探地设备。该设备包括框架,该框架由管子(1),固定的转向鳍片(2)和固定板(7)组成。由加强件(9)和叶片(12)组成的机翼通过螺栓(10)和螺母(11)固定在固定板(7)上,形成铰链连接,使机翼可折叠。安装在杆(15)上的锁定楔块(14)被放置在框架管(1)的内部,并且端盖(17)被安装在框架管(1)的上端。杆(15)和端盖(17)通过螺母(18)和楔形楔块(19)锁定在一起,从而形成机翼锁定机构。通过卸下螺母(18)并用防撞帽(20)替换端盖(17)来释放机翼锁定机构。当以水平位置展开时,机翼可提供较大的面积以防沉没。

著录项

  • 公开/公告号WO2017137652A1

    专利类型

  • 公开/公告日2017-08-17

    原文格式PDF

  • 申请/专利权人 KOIVUOJA MIKKO;

    申请/专利号WO2016FI00030

  • 发明设计人 KOIVUOJA MIKKO;

    申请日2016-12-27

  • 分类号E04H12/22;E02D5/54;E02D5/80;

  • 国家 WO

  • 入库时间 2022-08-21 13:30:09

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