GB474460A - Improvements in or relating to the control of aircraft brakes - Google Patents

Improvements in or relating to the control of aircraft brakes

Info

Publication number
GB474460A
GB474460A GB1373836A GB1373836A GB474460A GB 474460 A GB474460 A GB 474460A GB 1373836 A GB1373836 A GB 1373836A GB 1373836 A GB1373836 A GB 1373836A GB 474460 A GB474460 A GB 474460A
Authority
GB
United Kingdom
Prior art keywords
aircraft
lever
brakes
cams
operated
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
GB1373836A
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.)
Honeywell UK Ltd
Original Assignee
Bendix 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 Bendix Ltd filed Critical Bendix Ltd
Priority to GB1373836A priority Critical patent/GB474460A/en
Publication of GB474460A publication Critical patent/GB474460A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/42—Arrangement or adaptation of brakes
    • B64C25/44—Actuating mechanisms
    • B64C25/48—Actuating mechanisms differentially operated for steering purposes

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Of Braking Force In Braking Systems (AREA)

Abstract

474,460. Aircraft wheel brakes. BENDIX. Ltd., and ROBERTS, G. P. May 15, 1936, No. 13738. [Class 4] A control unit for fluid-pressure aircraft brakes comprises two valves on hydraulic cylinders respectively controlling brakes on opposite sides of the aircraft and mounted side by side and actuated by a pair of levers operable simultaneously by a hand lever and a Bowden wire h or differentially by cams n, m on a shaft p operated by the rudder bar. Only one valve a and one lever j are visible in Fig. 1. Each lever j is pivoted to the plunger e operated by the wire h and carries an adjustable stud s adapted to operate the valve and carries a roller l engaging one of the cams n, m. When the rudder bar is turned, one roller runs on the concentric pawl x of a cam but the other roller runs on to a substantially radial part y to relieve the pressure of one brake. The lower ends of the levers are guided by rods k.
GB1373836A 1936-05-15 1936-05-15 Improvements in or relating to the control of aircraft brakes Expired GB474460A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1373836A GB474460A (en) 1936-05-15 1936-05-15 Improvements in or relating to the control of aircraft brakes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1373836A GB474460A (en) 1936-05-15 1936-05-15 Improvements in or relating to the control of aircraft brakes

Publications (1)

Publication Number Publication Date
GB474460A true GB474460A (en) 1937-11-02

Family

ID=10028461

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1373836A Expired GB474460A (en) 1936-05-15 1936-05-15 Improvements in or relating to the control of aircraft brakes

Country Status (1)

Country Link
GB (1) GB474460A (en)

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