GB462498A - Improvements in or relating to means for controlling aircraft - Google Patents

Improvements in or relating to means for controlling aircraft

Info

Publication number
GB462498A
GB462498A GB9295/36A GB929536A GB462498A GB 462498 A GB462498 A GB 462498A GB 9295/36 A GB9295/36 A GB 9295/36A GB 929536 A GB929536 A GB 929536A GB 462498 A GB462498 A GB 462498A
Authority
GB
United Kingdom
Prior art keywords
wing
chord
aerofoil
controlling 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
GB9295/36A
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 GB9295/36A priority Critical patent/GB462498A/en
Publication of GB462498A publication Critical patent/GB462498A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B64C9/18—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by single flaps

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tires In General (AREA)
  • Control Of Turbines (AREA)
  • General Details Of Gearings (AREA)

Abstract

462,498. Controlling aircraft. FAIREY AVIATION CO., Ltd., and YOUNGMAN, R. T. March 28, 1936, No. 9295. Drawings to Specification. [Class 4] In means for controlling aircraft in which an aerofoil is of less chord and is pivotally mounted about, substantially, its centre of pressure below the main wing, the aerofoil has a chord of about 0À1 to 0À5 of that of the main wing and extends over about one half of the total length of the wing, its undersurface being disposed at approximately 0À05 to 0À3 of the wing chord below the wing, and its trailing edge immediately beneath or up to approximately 0À4 of the wing chord in advance that of the main wing. The aerofoil may be adjusted to an angle of incidence between 30‹ and 50‹ and may be in two or more sections.
GB9295/36A 1936-03-28 1936-03-28 Improvements in or relating to means for controlling aircraft Expired GB462498A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9295/36A GB462498A (en) 1936-03-28 1936-03-28 Improvements in or relating to means for controlling aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9295/36A GB462498A (en) 1936-03-28 1936-03-28 Improvements in or relating to means for controlling aircraft

Publications (1)

Publication Number Publication Date
GB462498A true GB462498A (en) 1937-03-10

Family

ID=9869213

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9295/36A Expired GB462498A (en) 1936-03-28 1936-03-28 Improvements in or relating to means for controlling aircraft

Country Status (1)

Country Link
GB (1) GB462498A (en)

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