GB285190A - Improvements in or relating to control mechanisms peculiar to aircraft - Google Patents

Improvements in or relating to control mechanisms peculiar to aircraft

Info

Publication number
GB285190A
GB285190A GB30265/26A GB3026526A GB285190A GB 285190 A GB285190 A GB 285190A GB 30265/26 A GB30265/26 A GB 30265/26A GB 3026526 A GB3026526 A GB 3026526A GB 285190 A GB285190 A GB 285190A
Authority
GB
United Kingdom
Prior art keywords
lever
aircraft
relating
control mechanisms
control mechanism
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
GB30265/26A
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
Priority to GB30265/26A priority Critical patent/GB285190A/en
Publication of GB285190A publication Critical patent/GB285190A/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
    • B64C13/24—Transmitting means
    • B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
    • B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
    • B64C13/32—Transmitting means without power amplification or where power amplification is irrelevant mechanical using cam mechanisms

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Abstract

285,190. Parnall, G. G., and Bolas, H. Nov. 30, 1926. Steering and balancing.-Control mechanism for operating devices situated on a removable or foldable part of aircraft is divided into sections which co-operate when the aircraft is assembled and are automatically disconnected when the part is removed or folded. As shown, the control rod 19 or wire mounted on a fuselage terminates in a lever 14 adapted to cooperate with a lever 6 m:ounted on a wing 10, the lever 6 having aileron control rods 5 or wires. The lever 6 is adjustable on an eccentric bush 8<a> and apertured plate 12<a> and is provided with cams 11 which may be designed to give differential movement. The control mechanism is adaptable to disconnectable tail units.
GB30265/26A 1926-11-30 1926-11-30 Improvements in or relating to control mechanisms peculiar to aircraft Expired GB285190A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB30265/26A GB285190A (en) 1926-11-30 1926-11-30 Improvements in or relating to control mechanisms peculiar to aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB30265/26A GB285190A (en) 1926-11-30 1926-11-30 Improvements in or relating to control mechanisms peculiar to aircraft

Publications (1)

Publication Number Publication Date
GB285190A true GB285190A (en) 1928-02-16

Family

ID=10304902

Family Applications (1)

Application Number Title Priority Date Filing Date
GB30265/26A Expired GB285190A (en) 1926-11-30 1926-11-30 Improvements in or relating to control mechanisms peculiar to aircraft

Country Status (1)

Country Link
GB (1) GB285190A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2542693A1 (en) * 1983-03-15 1984-09-21 Agusta Aeronaut Costr WAREHOUSE SYSTEM FOR CONNECTING TWO MOVING PARTS, IN PARTICULAR FOR AN AIRCRAFT
FR2728226A1 (en) * 1994-12-20 1996-06-21 Eurocopter France Coupling for control of helicopter yaw push rod, esp. for helicopters whose rear boom is foldable as in case of helicopter carrying ships

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2542693A1 (en) * 1983-03-15 1984-09-21 Agusta Aeronaut Costr WAREHOUSE SYSTEM FOR CONNECTING TWO MOVING PARTS, IN PARTICULAR FOR AN AIRCRAFT
GB2137943A (en) * 1983-03-15 1984-10-17 Agusta Aeronaut Costr Drive Gear Chain particularly between Disconnectable Parts of an Aircraft
FR2728226A1 (en) * 1994-12-20 1996-06-21 Eurocopter France Coupling for control of helicopter yaw push rod, esp. for helicopters whose rear boom is foldable as in case of helicopter carrying ships

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