GB236177A - Improvements in aeroplanes in connection with their transverse and steering equilibrium - Google Patents

Improvements in aeroplanes in connection with their transverse and steering equilibrium

Info

Publication number
GB236177A
GB236177A GB13467/25A GB1346725A GB236177A GB 236177 A GB236177 A GB 236177A GB 13467/25 A GB13467/25 A GB 13467/25A GB 1346725 A GB1346725 A GB 1346725A GB 236177 A GB236177 A GB 236177A
Authority
GB
United Kingdom
Prior art keywords
steering
fins
aeroplanes
equilibrium
transverse
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
GB13467/25A
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.)
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
Publication of GB236177A publication Critical patent/GB236177A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C5/00Stabilising surfaces
    • B64C5/08Stabilising surfaces mounted on, or supported by, wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Steering-Linkage Mechanisms And Four-Wheel Steering (AREA)

Abstract

236,177. Tammeo, A., Caminada, E., Foppiano, P., and Scotti, C. June 30, 1924, [Convention date]. Planes, arrangement and construction of. - Two fins 1, 2 parallel to the longitudinal axis of an aeroplane, are arranged above and extend rearwardly of the main planes so that the centres of pressure of the fins are above the rolling axis and behind the steering axis of the machine. The fins counteract yawing, rolling, and side slip.
GB13467/25A 1924-06-30 1925-05-22 Improvements in aeroplanes in connection with their transverse and steering equilibrium Expired GB236177A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT236177X 1924-06-30

Publications (1)

Publication Number Publication Date
GB236177A true GB236177A (en) 1926-04-08

Family

ID=11208605

Family Applications (1)

Application Number Title Priority Date Filing Date
GB13467/25A Expired GB236177A (en) 1924-06-30 1925-05-22 Improvements in aeroplanes in connection with their transverse and steering equilibrium

Country Status (1)

Country Link
GB (1) GB236177A (en)

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