ATE411939T1 - Triebwerkanlage für überschallflugzeuge - Google Patents

Triebwerkanlage für überschallflugzeuge

Info

Publication number
ATE411939T1
ATE411939T1 AT05290996T AT05290996T ATE411939T1 AT E411939 T1 ATE411939 T1 AT E411939T1 AT 05290996 T AT05290996 T AT 05290996T AT 05290996 T AT05290996 T AT 05290996T AT E411939 T1 ATE411939 T1 AT E411939T1
Authority
AT
Austria
Prior art keywords
nacelle
supersonic aircraft
plane
engine system
respect
Prior art date
Application number
AT05290996T
Other languages
English (en)
Inventor
Guillaume Lebas
Original Assignee
Airbus France
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 Airbus France filed Critical Airbus France
Application granted granted Critical
Publication of ATE411939T1 publication Critical patent/ATE411939T1/de

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C30/00—Supersonic type aircraft
    • 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
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/0536—Highspeed fluid intake means [e.g., jet engine intake]

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • General Electrical Machinery Utilizing Piezoelectricity, Electrostriction Or Magnetostriction (AREA)
  • Apparatuses For Generation Of Mechanical Vibrations (AREA)
  • Degasification And Air Bubble Elimination (AREA)
AT05290996T 2004-05-24 2005-05-10 Triebwerkanlage für überschallflugzeuge ATE411939T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0405557A FR2870513B1 (fr) 2004-05-24 2004-05-24 Nacelle de reacteur pour avion supersonique

Publications (1)

Publication Number Publication Date
ATE411939T1 true ATE411939T1 (de) 2008-11-15

Family

ID=34942259

Family Applications (1)

Application Number Title Priority Date Filing Date
AT05290996T ATE411939T1 (de) 2004-05-24 2005-05-10 Triebwerkanlage für überschallflugzeuge

Country Status (6)

Country Link
US (1) US7631836B2 (de)
EP (1) EP1607328B1 (de)
AT (1) ATE411939T1 (de)
CA (1) CA2507168C (de)
DE (1) DE602005010507D1 (de)
FR (1) FR2870513B1 (de)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070181743A1 (en) * 2006-02-08 2007-08-09 Lockheed Martin Corporation Method for streamline traced external compression inlet
US7871455B1 (en) * 2009-06-19 2011-01-18 Vintage Capital Group, Llc Jet engine protection system
US9447731B1 (en) * 2012-08-15 2016-09-20 The Boeing Company Supersonic elliptical ramp inlet
US9291101B2 (en) * 2013-02-28 2016-03-22 United Technologies Corporation Gas turbine engine inlet wall design
US9896219B2 (en) * 2015-02-20 2018-02-20 The Boeing Company Flow inlet
US10618638B2 (en) 2015-09-22 2020-04-14 Nctar, Llc Shockwave mitigation system for supersonic aircraft
CN112324572B (zh) * 2020-11-02 2021-11-19 厦门大学 基于弯曲激波理论的全三维内转进气道反设计方法

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1313327A (fr) * 1961-11-17 1962-12-28 Nord Aviation Instrument de bord pour le contrôle d'une entrée d'air de forme variable pour un moteur supersonique
US3347496A (en) * 1966-05-03 1967-10-17 Ryan Aeronautical Co Engine air inlet system for supersonic v/stol aircraft
GB1458033A (en) * 1973-05-31 1976-12-08 British Aircraft Corp Ltd Air intakes for jet propulsion engines
FR2635075B1 (fr) * 1988-08-04 1994-09-23 Onera (Off Nat Aerospatiale) Entree d'air supersonique bidimensionnelle et asymetrique pour l'air de combustion d'un moteur d'aeronef
US5934607A (en) * 1997-01-21 1999-08-10 Lockheed Martin Corporation Shock suppression supersonic aircraft
US6793175B1 (en) * 1999-08-25 2004-09-21 The Boeing Company Supersonic external-compression diffuser and method for designing same
US6575406B2 (en) * 2001-01-19 2003-06-10 The Boeing Company Integrated and/or modular high-speed aircraft

Also Published As

Publication number Publication date
CA2507168C (fr) 2011-12-13
US7631836B2 (en) 2009-12-15
EP1607328B1 (de) 2008-10-22
US20050258307A1 (en) 2005-11-24
FR2870513B1 (fr) 2006-08-11
FR2870513A1 (fr) 2005-11-25
DE602005010507D1 (de) 2008-12-04
CA2507168A1 (fr) 2005-11-24
EP1607328A1 (de) 2005-12-21

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Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties