GB564925A - Improvements in and relating to aircraft - Google Patents

Improvements in and relating to aircraft

Info

Publication number
GB564925A
GB564925A GB483343A GB483343A GB564925A GB 564925 A GB564925 A GB 564925A GB 483343 A GB483343 A GB 483343A GB 483343 A GB483343 A GB 483343A GB 564925 A GB564925 A GB 564925A
Authority
GB
United Kingdom
Prior art keywords
wings
aircraft
flaps
transverse
stub
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
GB483343A
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.)
ALFRED ERIC BUDD
Original Assignee
ALFRED ERIC BUDD
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 ALFRED ERIC BUDD filed Critical ALFRED ERIC BUDD
Priority to GB483343A priority Critical patent/GB564925A/en
Publication of GB564925A publication Critical patent/GB564925A/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

Landscapes

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

Abstract

564,925. Controlling aircraft. BUDD, A. E. March 25, 1943, No. 4833. [Class 4] An aeroplane has the outer portions 3 of its wings movable from a position transverse to the machine to a position adjacent to the fuselage during flight. The portions 3 are pivoted about vertical axes within slots formed in the stub wings 2. When flying with the wings turned back, the aircraft is controlled by flaps 10 hinged to both upper and lower surfaces of the stub wings 2. The wings are locked in both their transverse and longitudinal positions. The flaps may also be used to increase the resistance at landing with the wings extended. The usual ailerons 12 are also provided.
GB483343A 1943-03-25 1943-03-25 Improvements in and relating to aircraft Expired GB564925A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB483343A GB564925A (en) 1943-03-25 1943-03-25 Improvements in and relating to aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB483343A GB564925A (en) 1943-03-25 1943-03-25 Improvements in and relating to aircraft

Publications (1)

Publication Number Publication Date
GB564925A true GB564925A (en) 1944-10-19

Family

ID=9784649

Family Applications (1)

Application Number Title Priority Date Filing Date
GB483343A Expired GB564925A (en) 1943-03-25 1943-03-25 Improvements in and relating to aircraft

Country Status (1)

Country Link
GB (1) GB564925A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2699300A (en) * 1950-04-20 1955-01-11 Bell Aircraft Corp Aircraft with adjustable swept-back wings
GB2388094A (en) * 1986-08-12 2003-11-05 Aerospatiale Missile with variable flying surface

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2699300A (en) * 1950-04-20 1955-01-11 Bell Aircraft Corp Aircraft with adjustable swept-back wings
GB2388094A (en) * 1986-08-12 2003-11-05 Aerospatiale Missile with variable flying surface
GB2388094B (en) * 1986-08-12 2004-04-07 Aerospatiale Missile with variable flying surface

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