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Improvements in or relating to hydraulic jacks and power actuated systems including such jacks

机译:液压千斤顶和包括此类千斤顶的电动系统的改进或相关

摘要

690,219. Hydraulic machines ; Huid-pressure servomotor-control systems. NATIONAL RESEARCH DEVELOPMENT CORPORATION. Aug. 23,1950 [July 9, 1949], No. 18216/49. Classes 69 (ii) and 135 [Also in Group XXX] In a hydraulic servomotor-control system of the kind described in Specification 632,513 suitable for the operation of aircraft control surfaces, a hydraulic vane motor 53 is secured to the threaded shaft 48 which co-operates with the threaded piston 10 to either assist or restrain rotation of the threaded shaft. As shown in Fig. 1, the screw-threaded shaft 48 is made irreversible and the vane motor 53 housed in an extension of the cylinder 11 and connected by ducts 60, 57 to the valve casing. On movement of the pilot valve 17, e.g. to the left on rotation of the shaft 47 either electrically or manually, the main valve 28 moves to the left to connect the pressure duct 13 through the duct 60 simultaneously to the left-hand end of the cylinder I and the vane motor 53 and the exhaust duct 14 through the duct 57 to the vane motor. Thus rotation of the vane motor permits the axial movement of the piston 10 under the pressure applied to its left face. Rotation of the shaft 48 through bevel gears 50, 51, 52 recentres the valve 17 with respect to the valve 28. Under normal operation, a spring-loaded stop 63 is held out of engagement with the splined shaft 42 by liquid pressure. In the event of failure of the liquid pressure the stop 63 engages in a recess 64 on the shaft 42 whence rotation of the shaft 47 moves the valve 17 into engagement with one of the end stops 65, 66 to move the valve 28 to connect the vane motor and the left-hand end of the cylinder 11 with the exhaust duct 14 and lock the shaft 42 to the bevel gear 52, so that the shaft 48 may be rotated and hence the piston 10 axially moved through the gears 52, 51, 50. As shown in Fig. 2, the screw-threaded shaft 48 is made reversible, i.e., rotation of the shaft moves the piston 10 and movement of the piston rotates the shaft. In this case, the duct 60 supplies pressure liquid to the cylinder 11 only, the vane motor being connected to a port 70 in the valve casing by a duct 78 whilst the duct 57 branches into two ducts 73, 74 housing oppositely disposed non-return valves controlling ports 71, 72 in the valve casing. In the neutral position of the valves 17, 28, the port 70 is masked by a land 69 on the valve 28, the vane motor 53 then being hydraulically locked. On movement of the valve 17 to move the valve 28, pressure liquid circulates through the vane motor 53 in the corresponding direction but at a rate which retards the movement of the piston due to the restriction of the ports 70, 71, 72.
机译:690,219。液压机;液压伺服电机控制系统。国家研究开发公司。 1950年8月23日[1949年7月9日],编号18216/49。类69(ii)和135 [也属于XXX组]在适用于飞机操纵面操作的规范632513中描述的那种液压伺服电动机控制系统中,液压叶片电动机53固定在螺纹轴48上,该轴-与带螺纹的活塞10一起操作以辅助或限制带螺纹的轴的旋转。如图1所示,螺纹轴48是不可逆的,并且叶片电动机53容纳在气缸11的延伸部中,并通过管道60、57连接至阀壳体。在先导阀17移动时,例如在电动或手动旋转轴47时,主阀28向左移动,以通过管道60将压力管道13同时连接到气缸I的左端和叶片电动机53,以及排气管道14通过管道57到达叶片电动机。因此,叶片马达的旋转允许活塞10在施加到其左侧面上的压力下轴向运动。轴48通过锥齿轮50、51、52的旋转使阀17相对于阀28重新定位。在正常操作下,弹簧加载的止动件63通过液压而与花键轴42不接合。在液压故障的情况下,止动件63接合在轴42上的凹口64中,当轴47的旋转使阀17与端部止动件65、66之一接合时,阀28移动以连接阀28。叶片马达和带有排气管14的气缸11的左端,并将轴42锁定在锥齿​​轮52上,这样轴48可以旋转,因此活塞10通过齿轮52、51,如图50所示,使螺纹轴48可逆,即,轴的旋转使活塞10运动,而活塞的旋转使轴旋转。在这种情况下,管道60仅向气缸11供应压力液体,叶片电动机通过管道78连接至阀壳体中的端口70,而管道57分支成两个管道73、74,该管道容纳相对设置的止回阀阀壳体中的阀控制端口71、72。在阀17、28的中间位置,端口70被阀28上的凸台69遮盖,然后叶片马达53被液压锁定。在阀17运动以使阀28运动时,压力液体在相应的方向上通过叶片电动机53循环,但是由于端口70、71、72的限制,该压力以阻止活塞运动的速率循环。

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