GB425645A - Improvements in or relating to aircraft - Google Patents

Improvements in or relating to aircraft

Info

Publication number
GB425645A
GB425645A GB4928/34A GB492834A GB425645A GB 425645 A GB425645 A GB 425645A GB 4928/34 A GB4928/34 A GB 4928/34A GB 492834 A GB492834 A GB 492834A GB 425645 A GB425645 A GB 425645A
Authority
GB
United Kingdom
Prior art keywords
fins
aircraft
langley
convergence
angle
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
GB4928/34A
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.)
Fairey Aviation Co Ltd
Original Assignee
Fairey Aviation Co 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 Fairey Aviation Co Ltd filed Critical Fairey Aviation Co Ltd
Priority to GB4928/34A priority Critical patent/GB425645A/en
Publication of GB425645A publication Critical patent/GB425645A/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

Abstract

425,645. Aircraft. FAIREY AVIATION CO., Ltd., Cranford Lane, Hayes, Middlesex, and LOBELLE, M. J. O., Ludlow, Langley Road, Langley, Buckinghamshire. Feb. 14, 1934, No. 4928. [Class 4] In an aircraft fuselage provided with fins running longitudinally in substantially the direction of the airflow along the aft end thereof in proximity tc the tail unit, the fins being arranged symmetrically in pairs and converging the angle of convergence of the fins may be varied by turning the fins about longitudinal axes. The fins may be of rectangular or semicircular shape and of thin and symmetrical crosssection, or they may have an asymmetrical aerofoil or other aerodynamic section. The angle of convergence of the fins 17 is adjusted through shafts 21, levers 20, 18 and a link 19.
GB4928/34A 1934-02-14 1934-02-14 Improvements in or relating to aircraft Expired GB425645A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB4928/34A GB425645A (en) 1934-02-14 1934-02-14 Improvements in or relating to aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4928/34A GB425645A (en) 1934-02-14 1934-02-14 Improvements in or relating to aircraft

Publications (1)

Publication Number Publication Date
GB425645A true GB425645A (en) 1935-03-19

Family

ID=9786496

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4928/34A Expired GB425645A (en) 1934-02-14 1934-02-14 Improvements in or relating to aircraft

Country Status (1)

Country Link
GB (1) GB425645A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2573562A (en) * 1946-07-16 1951-10-30 Maurice A Garbell Inc Fluid-dynamic stabilizer and damper
US2630985A (en) * 1950-12-07 1953-03-10 United Aircraft Corp Helicopter stabilizer
US2999657A (en) * 1958-02-17 1961-09-12 Chance Vought Corp Stabilizing means for aircraft
US3384326A (en) * 1965-08-24 1968-05-21 Francis G. Neubeck Aerodynamic strake
US5096143A (en) * 1989-09-04 1992-03-17 William Nash Tail unit with rotatable tailplane

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2573562A (en) * 1946-07-16 1951-10-30 Maurice A Garbell Inc Fluid-dynamic stabilizer and damper
US2630985A (en) * 1950-12-07 1953-03-10 United Aircraft Corp Helicopter stabilizer
US2999657A (en) * 1958-02-17 1961-09-12 Chance Vought Corp Stabilizing means for aircraft
US3384326A (en) * 1965-08-24 1968-05-21 Francis G. Neubeck Aerodynamic strake
US5096143A (en) * 1989-09-04 1992-03-17 William Nash Tail unit with rotatable tailplane

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