GB433474A - Improvements relating to aeroplanes - Google Patents

Improvements relating to aeroplanes

Info

Publication number
GB433474A
GB433474A GB564434A GB564434A GB433474A GB 433474 A GB433474 A GB 433474A GB 564434 A GB564434 A GB 564434A GB 564434 A GB564434 A GB 564434A GB 433474 A GB433474 A GB 433474A
Authority
GB
United Kingdom
Prior art keywords
fuselage
plane
wings
leading edge
aeroplane
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
GB564434A
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 GB564434A priority Critical patent/GB433474A/en
Publication of GB433474A publication Critical patent/GB433474A/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
    • B64C3/54—Varying in area

Landscapes

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

Abstract

433,474. Aeroplanes. HILMY, S., 50, Church Street, Heliopolis, Cairo, Egypt. Feb. 20, 1934, No. 5644. [Class 4] An aeroplane comprises a longitudinal lifting surface of narrow chord mounted above the fuselage in a position in which it is inclined upwardly from its rear end, means being provided for varying the size of the opening between the forward end of the lifting surface and the fuselage. Fig. 1 shows an aeroplane having a fuselage 1 and a main narrow chord plane 3 which is cut away at the near and as shown to permit air flow over a rudder 8. Plane 3 may be provided with one or more slots 14. Plane 3 is pivotally and slidably mounted at 10 and may be moved to and from a nested position on the upper surface of fuselage 1 by bell-cranks 4 operated by fluid pressure servomotor or other means. In the nested position the leading edge of plane 3 rests behind a fairing 11. In a modified form reciprocating supporting struts 4 may be used. The plane 3 may be of the same width as fuselage 1, may overlap the forward edge of the fuselage or may be extended laterally to obviate necessity for lateral stabilizing wings 7. Wings 7 may be differentially adjustable to act as ailerons. In another form, Fig. 3, plane 3 may be fixed, and the gap between its leading edge and the fuselage bridged by an adjustable flap 12. The features of the two constructions shown may be combined. Lateral wings 7 may be adapted to carry engines and loads.
GB564434A 1934-02-20 1934-02-20 Improvements relating to aeroplanes Expired GB433474A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB564434A GB433474A (en) 1934-02-20 1934-02-20 Improvements relating to aeroplanes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB564434A GB433474A (en) 1934-02-20 1934-02-20 Improvements relating to aeroplanes

Publications (1)

Publication Number Publication Date
GB433474A true GB433474A (en) 1935-08-15

Family

ID=9799943

Family Applications (1)

Application Number Title Priority Date Filing Date
GB564434A Expired GB433474A (en) 1934-02-20 1934-02-20 Improvements relating to aeroplanes

Country Status (1)

Country Link
GB (1) GB433474A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2267265A (en) * 1992-05-22 1993-12-01 George Arthur Henwood Longitudinal wings flying machine.

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2267265A (en) * 1992-05-22 1993-12-01 George Arthur Henwood Longitudinal wings flying machine.

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