GB695026A - Improvements in or relating to high speed aircraft - Google Patents

Improvements in or relating to high speed aircraft

Info

Publication number
GB695026A
GB695026A GB1570450A GB1570450A GB695026A GB 695026 A GB695026 A GB 695026A GB 1570450 A GB1570450 A GB 1570450A GB 1570450 A GB1570450 A GB 1570450A GB 695026 A GB695026 A GB 695026A
Authority
GB
United Kingdom
Prior art keywords
aircraft
fuselage
wings
relating
portions
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
GB1570450A
Inventor
Frederick Francis Crocombe
Thomas George Guppy
Charles Willis Prower
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.)
Blackburn and General Aircraft Ltd
Original Assignee
Blackburn and General Aircraft 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 Blackburn and General Aircraft Ltd filed Critical Blackburn and General Aircraft Ltd
Priority to GB1570450A priority Critical patent/GB695026A/en
Publication of GB695026A publication Critical patent/GB695026A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/40—Varying angle of sweep

Abstract

695,026. Aircraft wings. BLACKBURN & GENERAL AIRCRAFT. Ltd. Aug. 31, 1951. [June 23, 1950] No. 15704/50. Class 4. In an aircraft having wings E which may be swung from a spread to a swept back position, the leading edge roots J are separately hinged at the point K so that on entering the fuselage these parts do not foul one another. The portions J may be displaced by a link N pivotted about the point O on the fuselage. Alternatively, an abutment S is provided on the fuselage so that as the wings swing into the spread position the portions J are opened against the action of the spring R. A curved guide T, co-operating with a slot in the wing E, may be provided. Specifications 665,171, [Group XXV], and 695,025 are referred to.
GB1570450A 1950-06-23 1950-06-23 Improvements in or relating to high speed aircraft Expired GB695026A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1570450A GB695026A (en) 1950-06-23 1950-06-23 Improvements in or relating to high speed aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1570450A GB695026A (en) 1950-06-23 1950-06-23 Improvements in or relating to high speed aircraft

Publications (1)

Publication Number Publication Date
GB695026A true GB695026A (en) 1953-08-05

Family

ID=10063977

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1570450A Expired GB695026A (en) 1950-06-23 1950-06-23 Improvements in or relating to high speed aircraft

Country Status (1)

Country Link
GB (1) GB695026A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2836381A (en) * 1955-08-16 1958-05-27 Jess Rink P Airplane with variable sweepback airfoils
DE1186748B (en) * 1962-09-21 1965-02-04 Heinkel Ag Ernst Airplane with wings that can be swiveled around vertical axes

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2836381A (en) * 1955-08-16 1958-05-27 Jess Rink P Airplane with variable sweepback airfoils
DE1186748B (en) * 1962-09-21 1965-02-04 Heinkel Ag Ernst Airplane with wings that can be swiveled around vertical axes

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