GB138381A - Improvements in elevator and the like control elements of aircraft - Google Patents

Improvements in elevator and the like control elements of aircraft

Info

Publication number
GB138381A
GB138381A GB16003/18A GB1600318A GB138381A GB 138381 A GB138381 A GB 138381A GB 16003/18 A GB16003/18 A GB 16003/18A GB 1600318 A GB1600318 A GB 1600318A GB 138381 A GB138381 A GB 138381A
Authority
GB
United Kingdom
Prior art keywords
elevator
aircraft
control elements
edge
ailerons
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
GB16003/18A
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 GB16003/18A priority Critical patent/GB138381A/en
Publication of GB138381A publication Critical patent/GB138381A/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
    • B64C13/30—Transmitting means without power amplification or where power amplification is irrelevant mechanical using cable, chain, or rod mechanisms

Landscapes

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

Abstract

138,381. Page, F. H. Oct. 2. 1918. Steering and balancing; planes, construction of.-The elevators, rudders, or ailerons 5, 6 of an aeroplane are pivoted about axes 7, 8 situated at a greater distance from the trailing edge of the adjacent fixed surface than the thickness of that edge, and are so shaped or tapered that their front edges do not project beyond the fixed plane in any position. Where twin control surfaces are used, they are provided with single king- posts 11, 12, projecting towards one another, for the attachment of control cables 13.
GB16003/18A 1918-10-02 1918-10-02 Improvements in elevator and the like control elements of aircraft Expired GB138381A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB16003/18A GB138381A (en) 1918-10-02 1918-10-02 Improvements in elevator and the like control elements of aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB16003/18A GB138381A (en) 1918-10-02 1918-10-02 Improvements in elevator and the like control elements of aircraft

Publications (1)

Publication Number Publication Date
GB138381A true GB138381A (en) 1920-02-02

Family

ID=10069435

Family Applications (1)

Application Number Title Priority Date Filing Date
GB16003/18A Expired GB138381A (en) 1918-10-02 1918-10-02 Improvements in elevator and the like control elements of aircraft

Country Status (1)

Country Link
GB (1) GB138381A (en)

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