WO2001053151A3 - Avion supersonique a turbosoufflantes escamotables par translation horizontale et procedes de mise en oeuvre - Google Patents

Avion supersonique a turbosoufflantes escamotables par translation horizontale et procedes de mise en oeuvre Download PDF

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Publication number
WO2001053151A3
WO2001053151A3 PCT/FR2001/000091 FR0100091W WO0153151A3 WO 2001053151 A3 WO2001053151 A3 WO 2001053151A3 FR 0100091 W FR0100091 W FR 0100091W WO 0153151 A3 WO0153151 A3 WO 0153151A3
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WO
WIPO (PCT)
Prior art keywords
turbo
supersonic
retractable
methods
same
Prior art date
Application number
PCT/FR2001/000091
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English (en)
Other versions
WO2001053151A2 (fr
Inventor
Gerard Fournier
Original Assignee
Gerard Fournier
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 Gerard Fournier filed Critical Gerard Fournier
Priority to EP01903927A priority Critical patent/EP1409343A2/fr
Publication of WO2001053151A2 publication Critical patent/WO2001053151A2/fr
Publication of WO2001053151A3 publication Critical patent/WO2001053151A3/fr

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/20—Aircraft characterised by the type or position of power plants of jet type within, or attached to, fuselages
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C30/00—Supersonic type aircraft
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

L'invention concerne un nouveau concept d'avion supersonique dont la consommation en carburant et le niveau de bruit au décollage sont très inférieurs à ceux des avions existants ou en projet. Ce concept est caractérisé par deux turbosoufflantes (11-12) qui, en vol supersonique, sont escamotées dans un fuselage aplati (1) placé sous les ailes (4), par déplacement horizontal d'un chariot. Les turboréacteurs (21-22) de vol supersonique, uniquement optimisés pour la croisière supersonique, sont très simplifiés de sorte que le poids total de la motorisation reste très réduit.
PCT/FR2001/000091 2000-01-19 2001-01-11 Avion supersonique a turbosoufflantes escamotables par translation horizontale et procedes de mise en oeuvre WO2001053151A2 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP01903927A EP1409343A2 (fr) 2000-01-19 2001-01-11 Avion supersonique a turbosoufflantes escamotables par translation horizontale et procedes de mise en oeuvre

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0000624A FR2803822B1 (fr) 2000-01-19 2000-01-19 Avion supersonique a turbosoufflantes escamotables par translation horizontale et procedes de mise en oeuvre
FR00/00624 2000-01-19

Publications (2)

Publication Number Publication Date
WO2001053151A2 WO2001053151A2 (fr) 2001-07-26
WO2001053151A3 true WO2001053151A3 (fr) 2002-02-14

Family

ID=8846043

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/FR2001/000091 WO2001053151A2 (fr) 2000-01-19 2001-01-11 Avion supersonique a turbosoufflantes escamotables par translation horizontale et procedes de mise en oeuvre

Country Status (3)

Country Link
EP (1) EP1409343A2 (fr)
FR (1) FR2803822B1 (fr)
WO (1) WO2001053151A2 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007015373A1 (de) * 2007-03-28 2008-10-02 Eads Deutschland Gmbh Luftfahrzeug
FR2921043B1 (fr) * 2007-09-18 2010-04-02 Gfic Methode pour faire decoller et atterrir, a faible niveau de bruit, un avion de transport, ainsi que pour ameliorer son rendement, et avion permettant la mise en oeuvre de cette methode
GB201817279D0 (en) 2018-10-24 2018-12-05 Rolls Royce Plc Supersonic jet aircraft

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB851916A (en) * 1957-10-21 1960-10-19 Power Jets Res & Dev Ltd Aircraft
FR1513933A (fr) * 1966-03-11 1968-02-16 Rolls Royce Avion à décollage vertical
DE1481682A1 (de) * 1966-03-31 1969-10-30 Ver Flugtechnische Werke Flugzeug mit Hubvorrichtungen
US4674712A (en) * 1985-01-22 1987-06-23 The Boeing Company Double-lobe fuselage composite airplane
WO1997048600A1 (fr) * 1996-06-21 1997-12-24 The Boeing Company Avion supersonique a impulseur subsonique et son procede de fonctionnement
FR2784960A1 (fr) * 1998-10-26 2000-04-28 Gerard Fernand Fournier Avion supersonique a faible consommation de carburant et procedes, pour le faire fonctionner a la dite faible consommation ainsi qu'a faible bruit au decollage

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB894822A (en) * 1958-09-01 1962-04-26 Bristol Siddeley Engines Ltd Improvements in aircraft

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB851916A (en) * 1957-10-21 1960-10-19 Power Jets Res & Dev Ltd Aircraft
FR1513933A (fr) * 1966-03-11 1968-02-16 Rolls Royce Avion à décollage vertical
DE1481682A1 (de) * 1966-03-31 1969-10-30 Ver Flugtechnische Werke Flugzeug mit Hubvorrichtungen
US4674712A (en) * 1985-01-22 1987-06-23 The Boeing Company Double-lobe fuselage composite airplane
WO1997048600A1 (fr) * 1996-06-21 1997-12-24 The Boeing Company Avion supersonique a impulseur subsonique et son procede de fonctionnement
FR2784960A1 (fr) * 1998-10-26 2000-04-28 Gerard Fernand Fournier Avion supersonique a faible consommation de carburant et procedes, pour le faire fonctionner a la dite faible consommation ainsi qu'a faible bruit au decollage

Also Published As

Publication number Publication date
FR2803822A1 (fr) 2001-07-20
WO2001053151A2 (fr) 2001-07-26
FR2803822B1 (fr) 2002-03-01
EP1409343A2 (fr) 2004-04-21

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