GB700070A - Improvements in or relating to control members for operating the steering gear of aircraft - Google Patents

Improvements in or relating to control members for operating the steering gear of aircraft

Info

Publication number
GB700070A
GB700070A GB1303252A GB1303252A GB700070A GB 700070 A GB700070 A GB 700070A GB 1303252 A GB1303252 A GB 1303252A GB 1303252 A GB1303252 A GB 1303252A GB 700070 A GB700070 A GB 700070A
Authority
GB
United Kingdom
Prior art keywords
arm
shaft
aircraft
rotation
axis
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
GB1303252A
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.)
STEPHEN CECIL WOODWARD
Blackburn and General Aircraft Ltd
Original Assignee
STEPHEN CECIL WOODWARD
Blackburn and General Aircraft 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 STEPHEN CECIL WOODWARD, Blackburn and General Aircraft Ltd filed Critical STEPHEN CECIL WOODWARD
Priority to GB1303252A priority Critical patent/GB700070A/en
Publication of GB700070A publication Critical patent/GB700070A/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 
    • B64C25/50—Steerable undercarriages; Shimmy-damping

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Control Devices (AREA)

Abstract

700,070. Aircraft controls. BLACKBURN & GENERAL AIRCRAFT, Ltd., and WOODWARD, S. C. May 22, 1952, No. 13032/52. Class 4 An operating control for the steering gear of an aircraft steerable nose wheel or landing wheels comprises an arm 11 which is retractable into a shaft 4, the rotation of which shaft effects the steering, in an arrangement such that on extension of such arm it extends at an angle to the axis of the shaft, and a rotation of the arm about said axis rotates the shaft. The shaft 4 is provided with a hollow block 8 in which the arm slides, which hollow block has a slot 9 to take the pin 14 fastened to the arm and a slot 10 with which the arm engages to transmit rotation. The end 13 of the arm 11 is suitably bevelled so that on pulling out the arm, it automatically inclines to the shaft. A sprung cable 15 is attached to the arm to ensure complete retraction when the arm is moved to the direction of the shaft axis. A disc 17 fast to the shaft provides an indicator and stops.
GB1303252A 1952-05-22 1952-05-22 Improvements in or relating to control members for operating the steering gear of aircraft Expired GB700070A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1303252A GB700070A (en) 1952-05-22 1952-05-22 Improvements in or relating to control members for operating the steering gear of aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1303252A GB700070A (en) 1952-05-22 1952-05-22 Improvements in or relating to control members for operating the steering gear of aircraft

Publications (1)

Publication Number Publication Date
GB700070A true GB700070A (en) 1953-11-25

Family

ID=10015558

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1303252A Expired GB700070A (en) 1952-05-22 1952-05-22 Improvements in or relating to control members for operating the steering gear of aircraft

Country Status (1)

Country Link
GB (1) GB700070A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4982918A (en) * 1988-01-29 1991-01-08 British Aerospace Public Limited Company Force sensitive aircraft throttle with feedback

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4982918A (en) * 1988-01-29 1991-01-08 British Aerospace Public Limited Company Force sensitive aircraft throttle with feedback

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