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Improvements in or relating to valve assemblies particularly for pumps

机译:阀组件的改进或相关的改进,特别是用于泵的阀组件

摘要

605,862. Relief valves. THOMPSON PRODUCTS, Inc. March 31, 1944, No. 6017. Convention date, March 26, 1943. [Class 135] A combined relief and byepass valve assembly for pumps especially fuel pumps for aircraft, comprises an open-ended sleeve 50 formed intermediate its ends with a wall 50c having an external valve face 50d and an internal valve seat 50e for the byepass valve 55. In Fig. 2, the assembly is shown in a positive displacement type of pump having an eccentric rotor 20 with slidable vanes 21 operating in a sleeve 19 arranged between inlet and discharge chambers 17, 18 in a pump casing 11. The valve assembly is arranged in a casing 12 between the pump casing 11 and a spring casing 13, the three casings being secured together by bolts 14. A diaphragm 16 of synthetic rubber or fabric impregnated with synthetic rubber is clamped between the casings 12 and 13. The chambers 17, 18 connect respectively with passages 29, 31 which in turn open through respective ports 30, 32 into counter-bores 24, 26 in the valve casing 12. A seat 25 for relief valve face 50d is formed between the bores 24, 26. The valve sleeve 50 is guided at its upper end by a flange 50a working in the bore 24 and at its lower end by cylindrical faces 50g on legs 50f working in a further bore 27. Ports 51 are formed in the sleeve 50 below the flange 50a to permit access of fluid to the interior of the sleeve 50. The byepass valve 55 like the relief valve 50 may be made of metal or of plastic material and has on its upper face a resilient washer 58 of fabric impregnated with synthetic rubber held in place by a dished metal spring washer 59 itself retained by a cotter-pin 60 passing through a boss 55b on the byepass valve. The byepass valve is loaded by a light spring 57 abutting a shoulder 28a on the valve casing. The relief valve 50 is loaded by a coil spring 41 having an upper retainer 39 adjustable on a screw 36 and a lower retainer 42. The latter has a boss 42a pressing into a complementary depression 43a in a washer 43 and thence through the diaphragm 16 into a similar depression in an inverted cup member 53 resting on shoulders 50h on the relief valve. The spring retainer 39 is prevented from rotating by a key 40. The screw 36 has a flange 36b which after adjustment of the screw is clamped against the underside of the casing 13 by a nut 38 threaded on a wider part 36c of the spindle. The upper side of the diaphragm 16 is subject to the pressure of the ambient air or to the pressure in the engine intake manifold through an aperture in a boss 13b. A washer 33 determines the effective area of the diaphragm.
机译:605862。安全阀。汤普森产品公司(Thompson Products,Inc。),1944年3月31日,编号6017。会议日期,1943年3月26日。[135类]组合式安全阀和旁通阀组件,用于飞机的泵,尤其是飞机的燃油泵,包括一个中间开口的套筒50其端部带有壁50c,该壁50c具有外部阀面50d和用于旁通阀55的内部阀座50e。在图2中,该组件以正排量型泵示出,该泵具有偏心转子20,该偏心转子20具有可操作的叶片21。阀组件布置在位于泵壳体11中的进气腔室17和排气腔室18之间的套筒19中。阀组件布置在泵壳体11和弹簧壳体13之间的壳体12中,这三个壳体通过螺栓14固定在一起。壳体12和13之间夹有由合成橡胶或浸渍有合成橡胶的织物制成的隔膜16。腔室17、18分别与通道29、31连接,通道29、31又通过各自的端口30、32通向内孔24、26。 VA活套12。在孔24、26之间形成用于安全阀面50d的座25。阀套50的上端通过在孔24中工作的凸缘50a引导,而其下端则通过在孔24中的圆柱面50g引导。支腿50f在另一个孔27中工作。在法兰50a下方的套筒50中形成端口51,以允许流体进入套筒50的内部。旁通阀55如安全阀50可以由金属制成或由金属制成。弹性材料制成的弹性垫圈58的上表面浸有合成橡胶,该垫圈由碟形金属弹簧垫圈59固定在适当的位置,碟形弹簧垫圈本身由开口销60保持,该销穿过旁通阀上的凸台55b。旁通阀由轻弹簧57加载,该轻弹簧57邻接阀壳体上的肩部28a。安全阀50由螺旋弹簧41加载,该螺旋弹簧41具有可在螺钉36上调节的上部保持器39和下部保持器42。下部保持器42具有凸台42a,该凸台42a压入垫圈43中的互补凹部43a,并由此穿过隔膜16进入。倒置的杯状部件53中的类似凹部位于减压阀的肩部50h上。弹簧保持器39通过键40防止旋转。螺钉36具有凸缘36b,在螺钉调整之后,该凸缘36b通过拧在主轴的较宽部分36c上的螺母38而被夹紧在壳体13的下侧。隔膜16的上侧通过凸台13b中的孔承受环境空气的压力或发动机进气歧管中的压力。垫圈33确定隔膜的有效面积。

著录项

  • 公开/公告号GB605862A

    专利类型

  • 公开/公告日1948-08-03

    原文格式PDF

  • 申请/专利权人 THOMPSON PRODUCTS INCORPORATED;

    申请/专利号GB601744A

  • 发明设计人

    申请日1944-03-31

  • 分类号F04C14/26;

  • 国家 GB

  • 入库时间 2022-08-24 02:38:26

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