GB457709A - Hydraulic controls for retractable undercarriages of aircraft - Google Patents

Hydraulic controls for retractable undercarriages of aircraft

Info

Publication number
GB457709A
GB457709A GB1585235A GB1585235A GB457709A GB 457709 A GB457709 A GB 457709A GB 1585235 A GB1585235 A GB 1585235A GB 1585235 A GB1585235 A GB 1585235A GB 457709 A GB457709 A GB 457709A
Authority
GB
United Kingdom
Prior art keywords
control
valve
port
spring
gear
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
GB1585235A
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.)
RAYMOND NOEL DOREY
Original Assignee
RAYMOND NOEL DOREY
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 RAYMOND NOEL DOREY filed Critical RAYMOND NOEL DOREY
Priority to GB1585235A priority Critical patent/GB457709A/en
Publication of GB457709A publication Critical patent/GB457709A/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

457,709. Aircraft alighting gear. RUBBRA. A. A., Red Roofs, Carlton Road, Derby, and DOREY, R. N., Grasmere, Burton Road, Findern, near Derby. May 31, 1935, No. 15852. [Class 4] Means for raising and lowering the retractable alighting-gear of aircraft include one or more constantly - operating pumps A normally circulating fluid idly, one or more hydraulic rams C adapted to cause movement of the gear, a control D operating a valve B to govern the direction of fluid supply to the rams and means for holding the control and valve means in their displaced position during movement of the gear and returning them to the neutral position when the movement has ceased, thus positively locking the gear in position. When the control D is moved against one or other of spring plungers E it is caught by one or other of two catches pivoted on a pin E<5> carried by a plunger E<6> and integral with levers E<3> pivoted on shafts E<2>. The pin control can be released from the plunger, on actuation of a lever G<1> against the action of a spring G<2>. In the midposition of control D, oil from the pump is returned to a reservoir A<1> through a pipe A<3> and ports H, H<1>. On rotation of valve B port H is closed, pressure builds up under plunger E<6> which is raised against the action of a spring E<7> and raises the pin E<5> to cause one or other of the catches E<1> to engage the control D and hold it deflected ; simultaneously, port H<2> is opened to the fluid supply which passes through the valve to the ram C. When the ram reaches the end of its travel, the spring E<7> forces plunger E<6> downwardly, oil passing through the leakage aperture E<8> to release the control D which is then returned to its mid-position. In a modification, when the control D, Fig. 7, is moved, e.g. to the left, the right-hand plunger J<2> is moved against the action of its spring J<3> and the valve is rotated closing port K thereby causing oil to flow into port M. Oil passes to the ram through port M<1> and back to the reservoir through a port in the valve. When the ram reaches the end of its stroke, the compressed spring J<3> forces its ram to the left, oil leaking through the piston, and returns the control D.
GB1585235A 1935-05-31 1935-05-31 Hydraulic controls for retractable undercarriages of aircraft Expired GB457709A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1585235A GB457709A (en) 1935-05-31 1935-05-31 Hydraulic controls for retractable undercarriages of aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1585235A GB457709A (en) 1935-05-31 1935-05-31 Hydraulic controls for retractable undercarriages of aircraft

Publications (1)

Publication Number Publication Date
GB457709A true GB457709A (en) 1936-11-30

Family

ID=10066682

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1585235A Expired GB457709A (en) 1935-05-31 1935-05-31 Hydraulic controls for retractable undercarriages of aircraft

Country Status (1)

Country Link
GB (1) GB457709A (en)

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