DE602005010507D1 - Triebwerkanlage für Überschallflugzeuge - Google Patents

Triebwerkanlage für Überschallflugzeuge

Info

Publication number
DE602005010507D1
DE602005010507D1 DE200560010507 DE602005010507T DE602005010507D1 DE 602005010507 D1 DE602005010507 D1 DE 602005010507D1 DE 200560010507 DE200560010507 DE 200560010507 DE 602005010507 T DE602005010507 T DE 602005010507T DE 602005010507 D1 DE602005010507 D1 DE 602005010507D1
Authority
DE
Germany
Prior art keywords
supersonic aircraft
nacelle
power plant
plane
respect
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.)
Active
Application number
DE200560010507
Other languages
English (en)
Inventor
Guillaume Lebas
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.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
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 Operations SAS filed Critical Airbus Operations SAS
Publication of DE602005010507D1 publication Critical patent/DE602005010507D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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)
DE200560010507 2004-05-24 2005-05-10 Triebwerkanlage für Überschallflugzeuge Active DE602005010507D1 (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
DE602005010507D1 true DE602005010507D1 (de) 2008-12-04

Family

ID=34942259

Family Applications (1)

Application Number Title Priority Date Filing Date
DE200560010507 Active DE602005010507D1 (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
FR2870513B1 (fr) 2006-08-11
US7631836B2 (en) 2009-12-15
EP1607328B1 (de) 2008-10-22
EP1607328A1 (de) 2005-12-21
FR2870513A1 (fr) 2005-11-25
CA2507168A1 (fr) 2005-11-24
ATE411939T1 (de) 2008-11-15
US20050258307A1 (en) 2005-11-24
CA2507168C (fr) 2011-12-13

Similar Documents

Publication Publication Date Title
DE602005010507D1 (de) Triebwerkanlage für Überschallflugzeuge
WO2006057653A3 (en) Integrated air inlet system for multi-propulsion aircraft engines
WO2006054290A3 (en) Use of air internal energy and devices
ATE344876T1 (de) Schallgedämpfte triebwerksgondel eines flugzeugs
ATE473164T1 (de) Gondel für zweistromtriebwerk
EP1728990A3 (de) Hilfstriebwerk beliefert mit Luft von der Gasturbine
EP2011962A3 (de) Rotationsmotor für Zusammensetzungszyklus
EP2236772A3 (de) Gasturbinentriebwerk mit Vorrichtung zur aktiven Steuerung des Schaufelspitzenspiels und zugehöriges Betriebsverfahren
WO2009120778A3 (en) Subsonic and stationary ramjet engines
EP1965053A3 (de) Kombinationsmotoren für Flugzeuge
EP2239428A3 (de) Abgaskammer für ein Turbinentriebwerk
ATE525556T1 (de) Anordnungen zur rückgewinnung ungenutzter energie von abgas einer verbrennungskraftmaschine und entsprechende verfahren
EP1990517A3 (de) Energieerzeugungssystem für Flugzeuge
ATE350774T1 (de) Brennstoffzellen-luftversorgung
EP1548230A3 (de) Schaufel mit gestalteten Stegen an der Abströmkante
US20110139940A1 (en) Wave attenuation panel inserted between the motor and air inlet of an aircraft nacelle
ATE441023T1 (de) Brennkraftmaschine mit sekundärlufteinblassystem
EP1816071A3 (de) Hilfsgasturbine für ein Flugzeug und entsprechendes Betriebsverfahren
FR2873095B1 (fr) Avion multimoteur a puits de descente
RU2008100463A (ru) Турбовинтовентиляторный двигатель
ATE430876T1 (de) Multidiffusor für eine hubkolbenbrennkraftmaschine, sowie hubkolbenbrennkraftmaschine
EA201490069A1 (ru) Системы и способы для двигателя с двухсекционным турбонагнетателем
DE602005023724D1 (de) Grenzschichtsauganordnung
ATE377701T1 (de) Gasturbinenanlage
DE602004012281D1 (de) Aufgeladener motor mit mindestens zwei turboladerstufen

Legal Events

Date Code Title Description
8364 No opposition during term of opposition
R082 Change of representative

Ref document number: 1607328

Country of ref document: EP

Representative=s name: MEISSNER & MEISSNER, 14199 BERLIN, DE