GB783087A - Aircraft - Google Patents

Aircraft

Info

Publication number
GB783087A
GB783087A GB1569/53A GB156953A GB783087A GB 783087 A GB783087 A GB 783087A GB 1569/53 A GB1569/53 A GB 1569/53A GB 156953 A GB156953 A GB 156953A GB 783087 A GB783087 A GB 783087A
Authority
GB
United Kingdom
Prior art keywords
wing
jan
aircraft
delta
leading edge
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
GB1569/53A
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 GB1569/53A priority Critical patent/GB783087A/en
Publication of GB783087A publication Critical patent/GB783087A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tires In General (AREA)
  • Toys (AREA)

Abstract

783,087. Aircraft. ECKINGTON, F. J. Jan. 20, 1954 [Jan. 20, 1953], No. 1569/53. Class 4. A delta-shape wing is provided with lateral wing extensions 6, provided with control surfaces 6A. The maximum thickness of both main and stub wings occurs at point 7 and the wings in section may increase in thickness from leading edge to trailing edge. The broken lines indicate a tail extension 6B and wing extensions 6C. A variety of wing plan-form shapes are shown in the drawings and a fin slidable along the aircraft body may be provided. The leading edges of the delta wing may carry hinged flaps which may be moved outwardly to vary the leading edge camber. Specification 652,248 is referred to.
GB1569/53A 1953-01-20 1953-01-20 Aircraft Expired GB783087A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1569/53A GB783087A (en) 1953-01-20 1953-01-20 Aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1569/53A GB783087A (en) 1953-01-20 1953-01-20 Aircraft

Publications (1)

Publication Number Publication Date
GB783087A true GB783087A (en) 1957-09-18

Family

ID=9724257

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1569/53A Expired GB783087A (en) 1953-01-20 1953-01-20 Aircraft

Country Status (1)

Country Link
GB (1) GB783087A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1296020B (en) * 1962-12-07 1969-05-22 Saab Ab Airplane with swept main wing and swept secondary wing
FR2401061A1 (en) * 1977-08-26 1979-03-23 Benson William Aircraft configured for aerodynamic lift from stationary - has wings forming double-delta aerofoil profile with engine intake for drawn over wing surface

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1296020B (en) * 1962-12-07 1969-05-22 Saab Ab Airplane with swept main wing and swept secondary wing
FR2401061A1 (en) * 1977-08-26 1979-03-23 Benson William Aircraft configured for aerodynamic lift from stationary - has wings forming double-delta aerofoil profile with engine intake for drawn over wing surface

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