GB522296A - Improvements in or relating to aerodynes - Google Patents

Improvements in or relating to aerodynes

Info

Publication number
GB522296A
GB522296A GB15725/39A GB1572539A GB522296A GB 522296 A GB522296 A GB 522296A GB 15725/39 A GB15725/39 A GB 15725/39A GB 1572539 A GB1572539 A GB 1572539A GB 522296 A GB522296 A GB 522296A
Authority
GB
United Kingdom
Prior art keywords
centre
gravity
plane
stabilizing
pressure
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
GB15725/39A
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.)
JACQUES MARIE PAUL JOSEPH HUBE
Original Assignee
JACQUES MARIE PAUL JOSEPH HUBE
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 JACQUES MARIE PAUL JOSEPH HUBE filed Critical JACQUES MARIE PAUL JOSEPH HUBE
Publication of GB522296A publication Critical patent/GB522296A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds

Landscapes

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

Abstract

522,296. Aeroplanes. GUIGUES DE MORETON DE CHABRILLAN, J. M. P. J. H. R. R., and DECROIX, P. M. E. May 26, 1939, Nos. 15725 and 15726. Convention dates, Dec. 8, 1938, and Feb. 16, 1939. [Class 4] An aircraft comprises a main lifting system, having its centre of pressure behind the centre of gravity of the craft, and a stabilizing aerofoil of adjustable lift arranged forward of and well above the centre of gravity so that both its lift and drag have a movement about the transverse axis through the centre of gravity. An aeroplane is shown having a main wing 3, with its centre of pressure 4 behind the centre of gravity 8, and a stabilizing plane 10 pivoted about its centre of pressure 12. A part only of the plane 10 may be tiltable. The plane 10 may have a slot forming slat 30, Fig. 7, instead of or in addition to the plane being pivoted, the slat being interconnected by a sliding rod 27 to a hinged trailing flap 24 and operated through a flexible connection by a lever 32. The slot forming means may be operated in conjunction with slot forming means on the main planes. A fin 5 and rudder 6 is provided but there is no stabilizing tail.
GB15725/39A 1938-12-08 1939-05-26 Improvements in or relating to aerodynes Expired GB522296A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR522296X 1938-12-08

Publications (1)

Publication Number Publication Date
GB522296A true GB522296A (en) 1940-06-13

Family

ID=8917809

Family Applications (1)

Application Number Title Priority Date Filing Date
GB15725/39A Expired GB522296A (en) 1938-12-08 1939-05-26 Improvements in or relating to aerodynes

Country Status (1)

Country Link
GB (1) GB522296A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2538224A (en) * 1945-11-13 1951-01-16 Daniel R Zuck Wing with interconnected flap and nose slat
US4896846A (en) * 1985-04-09 1990-01-30 Dynamic Engineering, Inc. Superagile tactical fighter aircraft and method of flying it in supernormal flight
USRE35387E (en) * 1985-04-09 1996-12-03 Dynamic Engineering, Inc. Superfragile tactical fighter aircraft and method of flying it in supernormal flight

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2538224A (en) * 1945-11-13 1951-01-16 Daniel R Zuck Wing with interconnected flap and nose slat
US4896846A (en) * 1985-04-09 1990-01-30 Dynamic Engineering, Inc. Superagile tactical fighter aircraft and method of flying it in supernormal flight
USRE35387E (en) * 1985-04-09 1996-12-03 Dynamic Engineering, Inc. Superfragile tactical fighter aircraft and method of flying it in supernormal flight

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