GB762722A - Improvements in or relating to locking devices, more particularly for the hydraulic actuators of aircraft landing gear - Google Patents

Improvements in or relating to locking devices, more particularly for the hydraulic actuators of aircraft landing gear

Info

Publication number
GB762722A
GB762722A GB29777/54A GB2977754A GB762722A GB 762722 A GB762722 A GB 762722A GB 29777/54 A GB29777/54 A GB 29777/54A GB 2977754 A GB2977754 A GB 2977754A GB 762722 A GB762722 A GB 762722A
Authority
GB
United Kingdom
Prior art keywords
piston
fingers
sleeve
locking
cylinder
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
GB29777/54A
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.)
Bendix Aviation Corp
Original Assignee
Bendix Aviation Corp
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 Bendix Aviation Corp filed Critical Bendix Aviation Corp
Publication of GB762722A publication Critical patent/GB762722A/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)
  • Actuator (AREA)

Abstract

762,722. Hydraulic actuators. BENDIX AVIATION CORPORATION. Oct. 15, 1954 [Nov. 18, 1953], No. 29777/54. Class 69 (2). A hydraulic actuator for raising and lowering the undercarriage of aircraft comprises a piston and cylinder and means for locking the piston at one end of the cylinder. A valve unit is also carried within the cylinder and is actuated to allow pressure liquid to effect movement of the piston only after the locking means is released. The piston in a tube piston 38 slidable within a cylinder 30'and is provided at one end with fingers 102 adapted to spring over an inwardly projecting sleeve 55, when the piston is moved to contract by pressure exerting a force on surface 56, to engage the end 104 of the fingers beyond the end of the sleeve. In this position the fingers are locked by the end of a locking sleeve 68 slidably mounted on inner sections 62, 64 projecting within the cylinder and held in the locking position by a spring 70. Upon pressure fluid entering port 86, it is fed into a chamber 76 by passing over the square edges of a valve 90, Figs. 2 and 3. The pressure exerted bears on the edge 69 of the sleeve 68 and forces it to move against the spring and to release its end from locking engagement with the fingers 102. A projection 103 on the inside of the sleeve 68 engages the valve 90 when the end of the sleeve disengages the fingers and lifts the valve from its seating permitting pressure fluid to pass through holes 94 in section 64 and to flow through a central tube 96. The tube 96 carries a wall 100 at its end which serves as the stationary end wall of an expansion chamber 98 of which the inside of the piston forms the remaining walls. The piston therefore extends to raise the undercarriage. A micro-switch 118 is provided to give an indication whether the locking elements are in their locked or unlocked position, and is operated by a feeler 124 which engages both the fingers and end of tube 68 to ensure their correct positioning. The feeler is pivoted on an arm 120 which holds the contacts of the switch open when the piston is correctly locked in its retracted position.
GB29777/54A 1953-11-18 1954-10-15 Improvements in or relating to locking devices, more particularly for the hydraulic actuators of aircraft landing gear Expired GB762722A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US762722XA 1953-11-18 1953-11-18

Publications (1)

Publication Number Publication Date
GB762722A true GB762722A (en) 1956-12-05

Family

ID=22130941

Family Applications (1)

Application Number Title Priority Date Filing Date
GB29777/54A Expired GB762722A (en) 1953-11-18 1954-10-15 Improvements in or relating to locking devices, more particularly for the hydraulic actuators of aircraft landing gear

Country Status (1)

Country Link
GB (1) GB762722A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2286227A (en) * 1994-01-18 1995-08-09 Dowty Aerospace Gloucester Actuator
US9688390B2 (en) 2012-09-17 2017-06-27 Safran Landing Systems Uk Ltd Landing gear assembly
CN110356545A (en) * 2019-08-21 2019-10-22 成都弗格森液压机电有限公司 A kind of unmanned plane undercarriage control retaining mechanism

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2286227A (en) * 1994-01-18 1995-08-09 Dowty Aerospace Gloucester Actuator
GB2286227B (en) * 1994-01-18 1997-05-28 Dowty Aerospace Gloucester Actuator
US9688390B2 (en) 2012-09-17 2017-06-27 Safran Landing Systems Uk Ltd Landing gear assembly
CN110356545A (en) * 2019-08-21 2019-10-22 成都弗格森液压机电有限公司 A kind of unmanned plane undercarriage control retaining mechanism

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