GB551527A - Improvements in or relating to distant control gear for hydraulic apparatus - Google Patents

Improvements in or relating to distant control gear for hydraulic apparatus

Info

Publication number
GB551527A
GB551527A GB941641A GB941641A GB551527A GB 551527 A GB551527 A GB 551527A GB 941641 A GB941641 A GB 941641A GB 941641 A GB941641 A GB 941641A GB 551527 A GB551527 A GB 551527A
Authority
GB
United Kingdom
Prior art keywords
valve
pump
piston
spring
contacts
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB941641A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
RUBERY OWEN MESSIER Ltd
Original Assignee
RUBERY OWEN MESSIER Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by RUBERY OWEN MESSIER Ltd filed Critical RUBERY OWEN MESSIER Ltd
Priority to GB941641A priority Critical patent/GB551527A/en
Publication of GB551527A publication Critical patent/GB551527A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/02Undercarriages
    • B64C25/08Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/18Operating mechanisms
    • B64C25/22Operating mechanisms fluid

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fluid-Pressure Circuits (AREA)

Abstract

551,527. Hydraulic control systems MESSIER, Ltd., R. O., and CONWAY, H. G. July 24, 1941, No. 9416. [Class 69 (ii)] An electrically controlled hydraulic control sys'em which is especially applicable for operating jacks or aircraft to control the undercarriages &c. is constructed with a control valve box 12, Fig. 1, for directing the liquid delivered by a pump 14 to the required end of the jack so as to move the carriage up or down. The valve 20 which may be a piston or other valve is actuated by energizing one or other of two electromagnets 25, 26 by actuating a lever 36 with push-buttons 34, 35 for closing contacts 38, 39 or 41, 42, and at the same time other contacts are closed to energize an electromagnet 48 which opens a normally closed valve 46 to permit pneumatic pressure from a pipe 43 to be directed to a clutch which drives the pump 14 from the aircraft engine. The valve 46 is held open by a spring- controlled latch 66 which is released by energization of an electromagnet 65 when the carriage has completed its movement in either direction and pressure builds up and operates a piston 59 causing closing of contacts 62, 63. When the latch 66 is released the magnet 65 is automatically de-energized by the breaking of contacts 72 by the motion of the core 70. For control in emergencies a hand-pump 73 supplied by a reservoir 74 can be used to direct liquid under pressure to a pipe 78 which is directed by a shuttle valve 81 to the jack and thus lowers the undercarriage, the pressure fluid passage from the pump being cut off and a by-pass valve 84 opened to connect the lower end of the jack cylinder to exhaust. In a modification the clutch for driving the pump 14 is controlled by a spring toggle device actuated by electromagnets energized similarly to the magnet 65 by pressure-actuated contacts 62, 63. In a further modification, Fig. 3, the pump 14 is driven continuously but is normally by-passed to exhaust via an outlet 109 of a chamber 100 fitted with a piston valve 103 held by a spring-plunger 107 against the action of a spring 104. The plunger can be withdrawn by energize ion of a magnet 110 and the spring then raises the piston 103 so as to cut off the by-pass. The magnet 110 is de-energized automatically, and the plunger 107 then engages a groove in the piston 103, and holds it raised until the rise in pressure at the end of the movement of the jack overcomes the action of spring 108 on the plunger 107 and the piston valve is forced down to the position shown in Fig. 3, thus again by-pasing the pump. Specifications 492,300 and 544,493, [Group XXXIII], are referred to.
GB941641A 1941-07-24 1941-07-24 Improvements in or relating to distant control gear for hydraulic apparatus Expired GB551527A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB941641A GB551527A (en) 1941-07-24 1941-07-24 Improvements in or relating to distant control gear for hydraulic apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB941641A GB551527A (en) 1941-07-24 1941-07-24 Improvements in or relating to distant control gear for hydraulic apparatus

Publications (1)

Publication Number Publication Date
GB551527A true GB551527A (en) 1943-02-26

Family

ID=9871541

Family Applications (1)

Application Number Title Priority Date Filing Date
GB941641A Expired GB551527A (en) 1941-07-24 1941-07-24 Improvements in or relating to distant control gear for hydraulic apparatus

Country Status (1)

Country Link
GB (1) GB551527A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2475373A (en) * 2009-11-11 2011-05-18 Gm Global Tech Operations Inc Manual hydraulic pump for releasing a blocked clutch

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2475373A (en) * 2009-11-11 2011-05-18 Gm Global Tech Operations Inc Manual hydraulic pump for releasing a blocked clutch

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