GB146631A - Improvements in or relating to the tail planes of aircraft - Google Patents

Improvements in or relating to the tail planes of aircraft

Info

Publication number
GB146631A
GB146631A GB9304/19A GB930419A GB146631A GB 146631 A GB146631 A GB 146631A GB 9304/19 A GB9304/19 A GB 9304/19A GB 930419 A GB930419 A GB 930419A GB 146631 A GB146631 A GB 146631A
Authority
GB
United Kingdom
Prior art keywords
struts
spar
secured
aircraft
relating
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
GB9304/19A
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 GB9304/19A priority Critical patent/GB146631A/en
Publication of GB146631A publication Critical patent/GB146631A/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)
  • Insulated Conductors (AREA)

Abstract

146,631. Paine, H. Scott-, and Supermarine Aviation Works, Ltd. April 11, 1919. Planes, disposition of, and connecting to machine.-The tail-plane is secured away from the body A by struts D<2> attached at one end to opposite sides of the body and at the other end to the front spar B at points spaced apart, while two additional struts D<1> are secured together at one end and to the spar B, and at the other end to the body close to the struts D<2>. A vertical strut D may also be used. The rear spar B<1> is secured by a vertical strut C and inclined struts C<1>, the points of attachment to the spars of the front and rear struts being preferably in alinement. The struts may be adjustable, and the struts D<1> should preferably be in compression initially. Bracing- wires F are also used.
GB9304/19A 1919-04-11 1919-04-11 Improvements in or relating to the tail planes of aircraft Expired GB146631A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9304/19A GB146631A (en) 1919-04-11 1919-04-11 Improvements in or relating to the tail planes of aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9304/19A GB146631A (en) 1919-04-11 1919-04-11 Improvements in or relating to the tail planes of aircraft

Publications (1)

Publication Number Publication Date
GB146631A true GB146631A (en) 1920-07-12

Family

ID=9869387

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9304/19A Expired GB146631A (en) 1919-04-11 1919-04-11 Improvements in or relating to the tail planes of aircraft

Country Status (1)

Country Link
GB (1) GB146631A (en)

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