GB255619A - Improvements in or connected with control gear for aircraft - Google Patents

Improvements in or connected with control gear for aircraft

Info

Publication number
GB255619A
GB255619A GB17018/25A GB1701825A GB255619A GB 255619 A GB255619 A GB 255619A GB 17018/25 A GB17018/25 A GB 17018/25A GB 1701825 A GB1701825 A GB 1701825A GB 255619 A GB255619 A GB 255619A
Authority
GB
United Kingdom
Prior art keywords
rudder bar
aircraft
adjusted
sliding block
control 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
GB17018/25A
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.)
ALFRED ERNEST MILLS
Blackburn Aeroplane and Motor Co Ltd
Original Assignee
ALFRED ERNEST MILLS
Blackburn Aeroplane and Motor Co 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 ALFRED ERNEST MILLS, Blackburn Aeroplane and Motor Co Ltd filed Critical ALFRED ERNEST MILLS
Priority to GB17018/25A priority Critical patent/GB255619A/en
Publication of GB255619A publication Critical patent/GB255619A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Consolidation Of Soil By Introduction Of Solidifying Substances Into Soil (AREA)

Abstract

255,619. Blackburn Aeroplane & Motor Co., Ltd., and Mills, A. E. July 2, 1925. Steering.-To enable the distance of the rudder bar from the pilot's seat to be adjusted without affecting the tension of the control cables, the pivot C of the rudder bar A is mounted on a sliding block and the control cables F are led over pulleys E, G, carried by the rudder bar, to anchoring points H on the machine. The sliding block moves over guides D and is adjusted in position by a screwed shaft J.
GB17018/25A 1925-07-02 1925-07-02 Improvements in or connected with control gear for aircraft Expired GB255619A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB17018/25A GB255619A (en) 1925-07-02 1925-07-02 Improvements in or connected with control gear for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB17018/25A GB255619A (en) 1925-07-02 1925-07-02 Improvements in or connected with control gear for aircraft

Publications (1)

Publication Number Publication Date
GB255619A true GB255619A (en) 1926-07-29

Family

ID=10087734

Family Applications (1)

Application Number Title Priority Date Filing Date
GB17018/25A Expired GB255619A (en) 1925-07-02 1925-07-02 Improvements in or connected with control gear for aircraft

Country Status (1)

Country Link
GB (1) GB255619A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2610006A (en) * 1950-11-18 1952-09-09 United Aircraft Corp Rudder pedal installation
US4192476A (en) * 1978-07-14 1980-03-11 Northrop Corporation Rudder pedal adjustment system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2610006A (en) * 1950-11-18 1952-09-09 United Aircraft Corp Rudder pedal installation
US4192476A (en) * 1978-07-14 1980-03-11 Northrop Corporation Rudder pedal adjustment system

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