GB454556A - Improvements relating to aircraft - Google Patents

Improvements relating to aircraft

Info

Publication number
GB454556A
GB454556A GB954435A GB954435A GB454556A GB 454556 A GB454556 A GB 454556A GB 954435 A GB954435 A GB 954435A GB 954435 A GB954435 A GB 954435A GB 454556 A GB454556 A GB 454556A
Authority
GB
United Kingdom
Prior art keywords
wing
sub
wings
adjustable
fully extended
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
GB954435A
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.)
ROSE MACDONALD
Original Assignee
ROSE MACDONALD
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 ROSE MACDONALD filed Critical ROSE MACDONALD
Priority to GB954435A priority Critical patent/GB454556A/en
Publication of GB454556A publication Critical patent/GB454556A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/38Adjustment of complete wings or parts thereof
    • B64C3/54Varying in area

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Eye Examination Apparatus (AREA)

Abstract

454,556. Controlling aircraft. MACDONALD, R., 81, South Audley Street, Mayfair, London. March 27, 1935, No. 9544. [Class 4] An aeroplane has wings of variable effective area comprising fixed parts 2, Fig. 2, and movable parts 5 which are pivoted near the wing tips at 9 so as to be capable of being drawn rearwardly, the inner edges of the movable parts 5 being guided in tracks 7 secured to the sides of the body and arranged to permit tilting of the planes 5 when fully extended. The auxiliary wings 5 are provided with flaps 4. In another form, Fig. 2, a subwing 14 is provided with adjustable flaps 13, 15 of which flap 13 serves to assist the outward movement of the sub wing and is adjustable in the fully extended position, Fig. 2(c) to open or close a slot between the main and sub-wings. Fig. 3 shows a subwing partially housed within the main wing and either arranged or not to form a slot when fully extended. Fig. 4 shows a guide track 23 for a sub-wing 22 which is pivotally mounted on the fuselage at 24 and adjustable in a guide 25. In a modification, a sub-wing is guided in a fixed channel by a ball-ended pin and may be adjusted in incidence without movement of the channel. The auxiliary wing 5 may be mounted above the main plane. The aerofoils may have a stressed skin covering consisting of a layer of wire gauze sandwiched between sheets of metal foil and means may be provided for passing an electric current through the covering for removing ice.
GB954435A 1935-03-27 1935-03-27 Improvements relating to aircraft Expired GB454556A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB954435A GB454556A (en) 1935-03-27 1935-03-27 Improvements relating to aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB954435A GB454556A (en) 1935-03-27 1935-03-27 Improvements relating to aircraft

Publications (1)

Publication Number Publication Date
GB454556A true GB454556A (en) 1936-09-28

Family

ID=9874035

Family Applications (1)

Application Number Title Priority Date Filing Date
GB954435A Expired GB454556A (en) 1935-03-27 1935-03-27 Improvements relating to aircraft

Country Status (1)

Country Link
GB (1) GB454556A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2555862A (en) * 1947-05-23 1951-06-05 Onera (Off Nat Aerospatiale) High-lift appliance for largely sweptback wings
US2596436A (en) * 1947-03-11 1952-05-13 Robert Roger Aime Folding wing for aircraft
US2614774A (en) * 1948-12-31 1952-10-21 United Aircraft Corp Flap mechanism
US2670910A (en) * 1949-09-16 1954-03-02 Blackburn & Gen Aircraft Ltd Aircraft
GB2388094A (en) * 1986-08-12 2003-11-05 Aerospatiale Missile with variable flying surface
CN107284651A (en) * 2016-04-05 2017-10-24 及兰平 Folding wing
WO2019141361A1 (en) 2018-01-18 2019-07-25 Fleck Future Concepts Gmbh Space-efficiently stowable, automatably deployable, condensable airplane wing
WO2019150289A1 (en) * 2018-02-02 2019-08-08 Mark Fraser A sail

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2596436A (en) * 1947-03-11 1952-05-13 Robert Roger Aime Folding wing for aircraft
US2555862A (en) * 1947-05-23 1951-06-05 Onera (Off Nat Aerospatiale) High-lift appliance for largely sweptback wings
US2614774A (en) * 1948-12-31 1952-10-21 United Aircraft Corp Flap mechanism
US2670910A (en) * 1949-09-16 1954-03-02 Blackburn & Gen Aircraft Ltd Aircraft
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
CN107284651A (en) * 2016-04-05 2017-10-24 及兰平 Folding wing
WO2019141361A1 (en) 2018-01-18 2019-07-25 Fleck Future Concepts Gmbh Space-efficiently stowable, automatably deployable, condensable airplane wing
WO2019150289A1 (en) * 2018-02-02 2019-08-08 Mark Fraser A sail

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