GB710841A - Improvements in and relating to aircraft - Google Patents

Improvements in and relating to aircraft

Info

Publication number
GB710841A
GB710841A GB26400/52A GB2640052A GB710841A GB 710841 A GB710841 A GB 710841A GB 26400/52 A GB26400/52 A GB 26400/52A GB 2640052 A GB2640052 A GB 2640052A GB 710841 A GB710841 A GB 710841A
Authority
GB
United Kingdom
Prior art keywords
aircraft
wing aircraft
elevons
wings
delta
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
GB26400/52A
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
Priority to GB26400/52A priority Critical patent/GB710841A/en
Publication of GB710841A publication Critical patent/GB710841A/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)
  • Toys (AREA)

Abstract

710,841. Aircraft control surfaces. BENNETT, D. C. T. Oct. 21, 1952, No. 26400/52. Class 4 The elevators of a swept-back wing aircraft or the elevons of a delta-wing aircraft are positioned so that in the attitude or normal flight they lie wholly below a horizontal plane passing through the lowest point on the trailing edge of the wings. In Fig. 1 (not shown), the tailplane of a sweptback wing aircraft lies wholly below such a plane. In Fig. 4, an underside view of a delta-wing plane is shown wherein the elevons are pivoted on brackets below the wings. Motive power may be supplied by a gas turbine, ducted fan, or rocket.
GB26400/52A 1952-10-21 1952-10-21 Improvements in and relating to aircraft Expired GB710841A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB26400/52A GB710841A (en) 1952-10-21 1952-10-21 Improvements in and relating to aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB26400/52A GB710841A (en) 1952-10-21 1952-10-21 Improvements in and relating to aircraft

Publications (1)

Publication Number Publication Date
GB710841A true GB710841A (en) 1954-06-16

Family

ID=10243044

Family Applications (1)

Application Number Title Priority Date Filing Date
GB26400/52A Expired GB710841A (en) 1952-10-21 1952-10-21 Improvements in and relating to aircraft

Country Status (1)

Country Link
GB (1) GB710841A (en)

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