GB146628A - Improvements in or relating to elevator-controlling mechanism in aircraft - Google Patents

Improvements in or relating to elevator-controlling mechanism in aircraft

Info

Publication number
GB146628A
GB146628A GB9300/19A GB930019A GB146628A GB 146628 A GB146628 A GB 146628A GB 9300/19 A GB9300/19 A GB 9300/19A GB 930019 A GB930019 A GB 930019A GB 146628 A GB146628 A GB 146628A
Authority
GB
United Kingdom
Prior art keywords
elevator
aircraft
relating
controlling mechanism
enclosed
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
GB9300/19A
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.)
HUBERT SCOTT PAINE
SUPERMARINE AVIAT WORKS Ltd
Original Assignee
HUBERT SCOTT PAINE
SUPERMARINE AVIAT WORKS 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 HUBERT SCOTT PAINE, SUPERMARINE AVIAT WORKS Ltd filed Critical HUBERT SCOTT PAINE
Priority to GB9300/19A priority Critical patent/GB146628A/en
Publication of GB146628A publication Critical patent/GB146628A/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)
  • Flexible Shafts (AREA)

Abstract

146,628. Paine, H. Scott-, and Supermarine Aviation Works, Ltd. April 11, 1919. Steering and regulating altitude.-The elevator C, which is mounted at a distance from the hull or enclosed body, has a pivotally mounted main spar C<1> and is controlled through a single rigid member D actuated by the usual flexible cables through a lever E<1> within the body. The part D may be enclosed in a vertical fin, or in a streamline casing.
GB9300/19A 1919-04-11 1919-04-11 Improvements in or relating to elevator-controlling mechanism in aircraft Expired GB146628A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9300/19A GB146628A (en) 1919-04-11 1919-04-11 Improvements in or relating to elevator-controlling mechanism in aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9300/19A GB146628A (en) 1919-04-11 1919-04-11 Improvements in or relating to elevator-controlling mechanism in aircraft

Publications (1)

Publication Number Publication Date
GB146628A true GB146628A (en) 1920-07-12

Family

ID=9869298

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9300/19A Expired GB146628A (en) 1919-04-11 1919-04-11 Improvements in or relating to elevator-controlling mechanism in aircraft

Country Status (1)

Country Link
GB (1) GB146628A (en)

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