GB317083A - - Google Patents

Info

Publication number
GB317083A
GB317083A GB24142/29A GB2414229A GB317083A GB 317083 A GB317083 A GB 317083A GB 24142/29 A GB24142/29 A GB 24142/29A GB 2414229 A GB2414229 A GB 2414229A GB 317083 A GB317083 A GB 317083A
Authority
GB
United Kingdom
Prior art keywords
fluid
cylinders
pressure
roller
chamber
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
GB24142/29A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB317083A publication Critical patent/GB317083A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/42Arrangement or adaptation of brakes
    • B64C25/44Actuating mechanisms
    • B64C25/445Brake regulators for preventing somersaulting
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/42Arrangement or adaptation of brakes
    • B64C25/44Actuating mechanisms
    • B64C25/46Brake regulators for preventing skidding or aircraft somersaulting
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/42Arrangement or adaptation of brakes
    • B64C25/44Actuating mechanisms
    • B64C25/48Actuating mechanisms differentially operated for steering purposes

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Braking Arrangements (AREA)
  • Steering Control In Accordance With Driving Conditions (AREA)
  • Regulating Braking Force (AREA)

Abstract

317,083. Messier, G. L. R. J. Aug. 10, 1928, [Convention date]. Fluid-pressure; force-transmitting mechanism. -For regulating a fluid-pressure-actuated brake, particularly for aeroplane wheels, a number of parallel cylinders contain pistons which act upon one face of a common transmitting element, the other face pressing against a rod or roller to actuate the brake, and fluid is admitted only to the required number of cylinders. The brake pressure on the two sides of the machine may be varied by having separate groups of cylinders for actuating the two brakes, or a single group may be used and the pressure of the transmitting element variably distributed. The fluid pressure may be derived from a skid actuated pump. Fig. 6 shows a series of cylinders a<1>, a<2>, for example four, having plungers acting on a common element d sliding on a guide e', fluid pressure being admitted to the required number of cylinders and the remainder left open to exhaust. The element d acts through a roller q upon a floating lever r connected at its ends to the pistons of two hydraulic transmissions connected to the brakes on the two sides of the machine. The position of the roller q is varied by a connection to a, lever t which controls the rudder. Alternatively the element d may act through a hydraulic transmission or directly through a rod connected to the roller q through a swinging rod, and the lever r may apply the brakes through mechanical transmission. Fig. 3 shows a valve for admitting fluid to the four cylinders a<1>, a<2>, &c. Two pistons i<1>, i<2> on a common stem divide a cylinder h into three chambers h', h<2>, h<3>, the chamber h<2> being in communication with the pressure fluid through a pipe j, and the chamber h<3> being connected to exhaust through a pipe l. A passage i<*> in the valve stem connects the chambers h<1>, h<3>. By moving the valve stem, the required number of ports k<1> - - k<4>, connected to the cylinders, are put into communication with the chamber h<3>, the remainder being left open to exhaust through the passage i<*>. A spring plunger m engages notches n in the valve stem to retain it in any of its five positions. The pipe l may lead to a chamber having an airspace under low pressure so as to return any exhausted fluid to the pump actuated by the tail skid.
GB24142/29A 1928-08-10 1929-08-07 Expired GB317083A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR317083T 1928-08-10

Publications (1)

Publication Number Publication Date
GB317083A true GB317083A (en) 1930-09-25

Family

ID=31897927

Family Applications (2)

Application Number Title Priority Date Filing Date
GB24142/29A Expired GB317083A (en) 1928-08-10 1929-08-07
GB385?6/30A Expired GB341007A (en) 1928-08-10 1929-08-07 Means for controlling brakes upon an aeroplane

Family Applications After (1)

Application Number Title Priority Date Filing Date
GB385?6/30A Expired GB341007A (en) 1928-08-10 1929-08-07 Means for controlling brakes upon an aeroplane

Country Status (3)

Country Link
DE (2) DE508858C (en)
FR (1) FR673646A (en)
GB (2) GB317083A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106800087A (en) * 2015-11-26 2017-06-06 中国直升机设计研究所 A kind of manned wheel braking controller for helicopter

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2478020A1 (en) * 1980-03-11 1981-09-18 Aerospatiale METHOD AND DEVICE FOR BRAKING WIDE-RUNWAY AIRCRAFT ON THE GROUND

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106800087A (en) * 2015-11-26 2017-06-06 中国直升机设计研究所 A kind of manned wheel braking controller for helicopter
CN106800087B (en) * 2015-11-26 2019-05-07 中国直升机设计研究所 A kind of manned wheel braking controller for helicopter

Also Published As

Publication number Publication date
DE520668C (en) 1931-03-13
FR673646A (en) 1930-01-17
GB341007A (en) 1931-01-07
DE508858C (en) 1930-10-03

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