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Improvements relating to door-operating and like mechanism

机译:与门操作及类似机构有关的改进

摘要

593,175. Door-operating mechanism. GENERAL MOTORS CORPORATION. June 12, 1945, No. 14848. Convention date, July 19, 1944. [Classes 44 and 65 (i)] [Also in Group XXXVII] Door-operating mechanism comprises a latch-held spring forming part of a telescopic link, and a motor-operated screw and nut device, the nut of which is adapted to move in one direction to release the spring and effect a quick movement of the door and to move in the return direction and effect a slow reverse movement of the door. A tubular member 60 while telescoping within a casing 81 stresses a coil spring 78 which is held in the stressed condition by a spring- loaded pivoted latch 71 engaging the outer race of a ball bearing 50 mounted on a screw shaft 25. A recess 64 in the link pivotally engages a lug mounted on a bomb-bay door of an aircraft. A nut 52 having a bevelled portion 73 which in the closed position of the door as shown, abuts the latch, is adapted to slide within the link, the nut and shaft co-operating by means of travelling balls 53 which are contained within a channel defined by coincident helical grooves. An electric motor 20, pivotally connected to the fuselage of the aircraft by an apertured lug 21, is adapted to rotate the shaft through a magnetic clutch which drives a spindle 23, on an eccentric portion 40 of which is rotatably mounted a hypocylic gear member 43 having two sets of teeth which mesh respectively with internal teeth on gears 28 and 32. The former is secured to the screw-shaft and the latter is held stationary by the meshing of external teeth with a worm 35. The gear 28 has a flange 100 formed with a worm tooth which meshes with a gear 101 coupled by a train of reduction gearing to a switch control cam. To open the door a selector switch is moved to the " down " position, closing circuits for operating the motor to move the nut downwards, thereby tripping the latch and releasing the spring which projects the link out of the casing, a collar 61 on the link then resting on an upper flange 152 of the nut. The cam operates switches arranged to stop the motor after the latch is tripped. When the door is fully open a signal lamp becomes illuminated. The selector switch when moved to the " up " position closes further circuits which energize a reversing field winding in the motor. The nut then ascends carrying with it the link until the latch becomes re-engaged. The cam is arranged to reverse the direction of rotation of the motor at this point, causing the nut to descend until it abuts the latch, when the motor is stopped by the cam. A second signal lamp then becomes illuminated to indicate that the door is fully closed.
机译:593,175。门操作机构。通用汽车公司。 1945年6月12日,第14848号。会议日期,1944年7月19日。[44和65(i)级] [也在XXXVII组中]门操纵机构包括一个闩锁式弹簧,该弹簧构成伸缩连杆的一部分,以及一种电动螺丝和螺母装置,其螺母适于沿一个方向运动以释放弹簧并实现门的快速运动,并沿返回方向运动并实现门的慢速反向运动。当管状构件60在壳体81内伸缩时,螺旋弹簧78受到应力,该螺旋弹簧78由弹簧加载的枢转闩锁71保持在受力状态,该闩锁71接合安装在螺杆25上的球轴承50的外圈。连杆可枢转地接合安装在飞机炸弹舱门上的凸耳。螺母52具有斜面部分73,该斜面部分73在如图所示的门的关闭位置中与闩锁邻接,该螺母52适于在连杆内滑动,螺母和轴通过包含在通道内的行进球53协同工作。由重合的螺旋形凹槽定义。电动机20通过有孔的凸耳21可枢转地连接到飞机的机身,该电动机20适于通过电磁离合器旋转轴,该电磁离合器驱动心轴23,在心轴23的偏心部分40上可旋转地安装有次圆柱齿轮构件43。具有两组分别与齿轮28和32上的内齿啮合的齿。前者固定在螺杆上,而后者则通过外齿与蜗杆35的啮合而保持静止。齿轮28具有法兰100由蜗轮齿构成的蜗杆与蜗轮101啮合,该齿轮通过减速齿轮系与开关控制凸轮相连。为了打开门,将一个选择器开关移至“向下”位置,关闭电路以使电动机运转,以使螺母向下移动,从而使闩锁跳闸,并释放弹簧,该弹簧将连杆从壳体中伸出,在壳体上的卡圈61上。然后将连杆固定在螺母的上凸缘152上。凸轮操作开关,以使闩锁跳闸后停止电动机。门完全打开后,信号灯会亮起。当移动到“向上”位置的选择器开关闭合进一步电路中激励的换向字段中的电机绕组。然后,螺母随连杆一起上升,直到闩锁重新啮合。凸轮设置成在这一点上使电动机的旋转方向反向,从而在电动机被凸轮停止时使螺母下降直到其紧靠闩锁。然后第二个信号灯点亮,指示门已完全关闭。

著录项

  • 公开/公告号GB593175A

    专利类型

  • 公开/公告日1947-10-09

    原文格式PDF

  • 申请/专利权人 GENERAL MOTORS CORPORATION;

    申请/专利号GB19450014848

  • 发明设计人

    申请日1945-06-12

  • 分类号E05F15/10;

  • 国家 GB

  • 入库时间 2022-08-24 02:50:48

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