GB614887A - Improvements in or relating to a hydraulic brake system - Google Patents

Improvements in or relating to a hydraulic brake system

Info

Publication number
GB614887A
GB614887A GB2382146A GB2382146A GB614887A GB 614887 A GB614887 A GB 614887A GB 2382146 A GB2382146 A GB 2382146A GB 2382146 A GB2382146 A GB 2382146A GB 614887 A GB614887 A GB 614887A
Authority
GB
United Kingdom
Prior art keywords
pipes
valves
brake
pump
brake system
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
GB2382146A
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.)
Glenn L Martin Co
Original Assignee
Glenn L Martin Co
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 Glenn L Martin Co filed Critical Glenn L Martin Co
Priority to GB2382146A priority Critical patent/GB614887A/en
Publication of GB614887A publication Critical patent/GB614887A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Braking Systems And Boosters (AREA)

Abstract

614,887. Hydraulic brakes. STEVENS, A. H. (Martin Co., G. L.). Aug. 12, 1946, No. 23821. [Class 103 (i)] In a hydraulic brake system in which pressure liquid is supplied to each brake by a pump through a driver's pressure-control valve, an accumulator being interposed between the pump and valve, the latter is connected to a manuallyoperable flow-control valve arranged to direct the liquid through either of two separate pipes by which it is connected to the brake, one pipe being used for normal supply and the other for emergency supply if the first pipe breaks or is shot away. The aircraft brake system shown comprises a reservoir R, pump P, accumulator A and pressure-control valves 5, 51 operable by the rudder pedals. The valves are connected by pipes 11, 11<SP>1</SP> to fourway flow-control valves 15, 15<SP>1</SP> connected by pipes 19, 23 and 19<SP>1</SP>, 23<SP>1</SP> and shuttle valves 21, 211 to the brake cylinders. With the valves in the position shown, liquid is supplied through the pipes 19, 19<SP>1</SP> and the shuttle valves are vented through pipes 23, 23<SP>1</SP> and pipes 25, 25<SP>1</SP> connected to a reservoir pipe 27. If the pipes 23, 23<SP>1</SP> are used as supply lines, the shuttle valves are vented through the pipes 19, 191.
GB2382146A 1946-08-12 1946-08-12 Improvements in or relating to a hydraulic brake system Expired GB614887A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2382146A GB614887A (en) 1946-08-12 1946-08-12 Improvements in or relating to a hydraulic brake system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2382146A GB614887A (en) 1946-08-12 1946-08-12 Improvements in or relating to a hydraulic brake system

Publications (1)

Publication Number Publication Date
GB614887A true GB614887A (en) 1948-12-23

Family

ID=10201853

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2382146A Expired GB614887A (en) 1946-08-12 1946-08-12 Improvements in or relating to a hydraulic brake system

Country Status (1)

Country Link
GB (1) GB614887A (en)

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