FR2803822B1 - 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

Info

Publication number
FR2803822B1
FR2803822B1 FR0000624A FR0000624A FR2803822B1 FR 2803822 B1 FR2803822 B1 FR 2803822B1 FR 0000624 A FR0000624 A FR 0000624A FR 0000624 A FR0000624 A FR 0000624A FR 2803822 B1 FR2803822 B1 FR 2803822B1
Authority
FR
France
Prior art keywords
turbosoufflantes
implementation
methods
horizontal translation
supersonic aircraft
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 - Fee Related
Application number
FR0000624A
Other languages
English (en)
Other versions
FR2803822A1 (fr
Inventor
Gerard Fernand Fournier
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 FR0000624A priority Critical patent/FR2803822B1/fr
Priority to PCT/FR2001/000091 priority patent/WO2001053151A2/fr
Priority to EP01903927A priority patent/EP1409343A2/fr
Publication of FR2803822A1 publication Critical patent/FR2803822A1/fr
Application granted granted Critical
Publication of FR2803822B1 publication Critical patent/FR2803822B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/16Aircraft characterised by the type or position of power plants of jet type
    • B64D27/20Aircraft characterised by the type or position of power plants of jet type within, or attached to, fuselages
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C30/00Supersonic type aircraft
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR0000624A 2000-01-19 2000-01-19 Avion supersonique a turbosoufflantes escamotables par translation horizontale et procedes de mise en oeuvre Expired - Fee Related FR2803822B1 (fr)

Priority Applications (3)

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
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
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 (1)

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

Publications (2)

Publication Number Publication Date
FR2803822A1 FR2803822A1 (fr) 2001-07-20
FR2803822B1 true FR2803822B1 (fr) 2002-03-01

Family

ID=8846043

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0000624A Expired - Fee Related FR2803822B1 (fr) 2000-01-19 2000-01-19 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

Family Cites Families (7)

* 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
GB894822A (en) * 1958-09-01 1962-04-26 Bristol Siddeley Engines Ltd Improvements in aircraft
GB1075128A (en) * 1966-03-11 1967-07-12 Rolls Royce Vertical take-off aircraft
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
FR2784960B1 (fr) 1998-10-26 2000-12-01 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
EP1409343A2 (fr) 2004-04-21
FR2803822A1 (fr) 2001-07-20
WO2001053151A3 (fr) 2002-02-14
WO2001053151A2 (fr) 2001-07-26

Similar Documents

Publication Publication Date Title
ID17661A (id) Metode untuk memperluas pipa
AU9663401A (en) Method and apparatus for expansion sealing concentric tubular structures
NO20011548L (no) Fremgangsmåte for kronostratigrafisk tolkning av et seismisk tverrsnitt eller en blokk
GB2329918B (en) Downhole pipe expansion apparatus and method
DK0676600T3 (da) Køleapparatur med ekspansionsturbine
NO994796L (no) Anordning og fremgangsmåte for utvinning av hydrater
EP1189020A4 (fr) Bloc principal de controle et procede de production dudit bloc
DE69620229D1 (de) System zum ausrichten einer windturbine
DE69723998D1 (de) Verfahren zum plasma-löten
FI940978A0 (fi) Hierarkkinen synkronointimenetelmä
SG82042A1 (en) Method of repairing turbine airfoils
FR2803822B1 (fr) Avion supersonique a turbosoufflantes escamotables par translation horizontale et procedes de mise en oeuvre
DK0913708T3 (da) Elektromagnetisk signalopsamlingsapparat og fremgangsmåde til brug af samme
FI935572A (fi) Menetelmä ja laitteisto energian tuottamiseksi ulkoilman ja veden lämpötilaerosta
DE69832848D1 (de) SPS-Synchronisationsverfahren
FI940980A0 (fi) Hierarkkinen synkronointimenetelmä
FI19992112A (fi) Synkronointimenetelmä ja -järjestely
FI20002798A0 (fi) Menetelmä ja laitteisto putkien valmistamiseksi
DE69501731T2 (de) Leichtbau-wärmedämmplatten
FI963910A (fi) Hierarkinen synkronointimenetelmä
FI963909A (fi) Hierarkkinen synkronointimenetelmä
IL114123A0 (en) Gas turbine system with heat recovery cycle and method for using the same
AU2001271546A1 (en) Segmented support structure and method and fixture for making the same
DE29623052U1 (de) Vorrichtung zum Einbringen einer Dehnungsfuge zwischen zwei Bauelementen
DE69400687T2 (de) Vorrichtung und Verfahren zum Befestigen einer Elektronenkanone an Glasstäben

Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20110930