ATE418492T1 - Turbojet für flugzeug, mit solch einem turbojet ausgestattetes flugzeug und verfahren zur befestigung solch eines turbojets an einem flugzeug - Google Patents

Turbojet für flugzeug, mit solch einem turbojet ausgestattetes flugzeug und verfahren zur befestigung solch eines turbojets an einem flugzeug

Info

Publication number
ATE418492T1
ATE418492T1 AT06808280T AT06808280T ATE418492T1 AT E418492 T1 ATE418492 T1 AT E418492T1 AT 06808280 T AT06808280 T AT 06808280T AT 06808280 T AT06808280 T AT 06808280T AT E418492 T1 ATE418492 T1 AT E418492T1
Authority
AT
Austria
Prior art keywords
aircraft
turbojet
jet engine
attaching
stabilizer
Prior art date
Application number
AT06808280T
Other languages
English (en)
Inventor
Bernard Guering
Olivier Teulou
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 ATE418492T1 publication Critical patent/ATE418492T1/de

Links

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
    • 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
    • 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)
  • Vehicle Body Suspensions (AREA)
AT06808280T 2005-09-23 2006-09-05 Turbojet für flugzeug, mit solch einem turbojet ausgestattetes flugzeug und verfahren zur befestigung solch eines turbojets an einem flugzeug ATE418492T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0552830A FR2891242B1 (fr) 2005-09-23 2005-09-23 Turboreacteur pour aeronef, aeronef muni d'un tel turboreacteur, et procede de montage d'un tel turboreacteur sur un aeronef

Publications (1)

Publication Number Publication Date
ATE418492T1 true ATE418492T1 (de) 2009-01-15

Family

ID=36570817

Family Applications (1)

Application Number Title Priority Date Filing Date
AT06808280T ATE418492T1 (de) 2005-09-23 2006-09-05 Turbojet für flugzeug, mit solch einem turbojet ausgestattetes flugzeug und verfahren zur befestigung solch eines turbojets an einem flugzeug

Country Status (11)

Country Link
US (1) US8167239B2 (de)
EP (1) EP1954563B1 (de)
JP (1) JP5087545B2 (de)
CN (1) CN100526159C (de)
AT (1) ATE418492T1 (de)
BR (1) BRPI0616104A2 (de)
CA (1) CA2622151C (de)
DE (1) DE602006004477D1 (de)
FR (1) FR2891242B1 (de)
RU (1) RU2398714C2 (de)
WO (1) WO2007034094A1 (de)

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WO2014066503A1 (en) 2012-10-23 2014-05-01 General Electric Company Unducted thrust producing system
FR2997681B1 (fr) * 2012-11-08 2015-05-15 Snecma Avion propulse par un turboreacteur a soufflantes contrarotatives
WO2014074145A1 (en) 2012-11-12 2014-05-15 United Technologies Corporation Angled core gas turbine engine mounting
US9567062B2 (en) 2012-11-12 2017-02-14 United Technologies Corporation Box wing with angled gas turbine engine cores
US9884674B2 (en) 2012-11-15 2018-02-06 United Technologies Corporation Stabilizer with structural box and sacrificial surfaces
FR3020347B1 (fr) * 2014-04-28 2016-05-20 Airbus Operations Sas Procede d'assemblage d'une partie arriere d'aeronef
RU2620246C2 (ru) * 2015-10-23 2017-05-23 Акционерное общество "Информационные спутниковые системы" имени академика М.Ф. Решетнёва" Замок натяжной регулируемый
US11111029B2 (en) * 2017-07-28 2021-09-07 The Boeing Company System and method for operating a boundary layer ingestion fan
US10759545B2 (en) 2018-06-19 2020-09-01 Raytheon Technologies Corporation Hybrid electric aircraft system with distributed propulsion
US10906657B2 (en) * 2018-06-19 2021-02-02 Raytheon Technologies Corporation Aircraft system with distributed propulsion
US12571360B2 (en) 2021-04-14 2026-03-10 General Electric Deutschland Holding Gmbh Three-stream gas turbine engine with embedded electric machine
US11492918B1 (en) 2021-09-03 2022-11-08 General Electric Company Gas turbine engine with third stream
US12071896B2 (en) 2022-03-29 2024-08-27 General Electric Company Air-to-air heat exchanger potential in gas turbine engines
US11834995B2 (en) 2022-03-29 2023-12-05 General Electric Company Air-to-air heat exchanger potential in gas turbine engines
US12065989B2 (en) 2022-04-11 2024-08-20 General Electric Company Gas turbine engine with third stream
US11834954B2 (en) 2022-04-11 2023-12-05 General Electric Company Gas turbine engine with third stream
US11834992B2 (en) 2022-04-27 2023-12-05 General Electric Company Heat exchanger capacity for one or more heat exchangers associated with an accessory gearbox of a turbofan engine
US12060829B2 (en) 2022-04-27 2024-08-13 General Electric Company Heat exchanger capacity for one or more heat exchangers associated with an accessory gearbox of a turbofan engine
US11680530B1 (en) 2022-04-27 2023-06-20 General Electric Company Heat exchanger capacity for one or more heat exchangers associated with a power gearbox of a turbofan engine
US12366204B2 (en) 2022-04-27 2025-07-22 General Electric Company Heat exchanger capacity for one or more heat exchangers associated with a power gearbox of a turbofan engine
US12560132B2 (en) 2022-08-02 2026-02-24 General Electric Company Gas turbine engine with third stream
US12486817B2 (en) 2022-08-02 2025-12-02 General Electric Company Gas turbine engine with third stream
US12031504B2 (en) 2022-08-02 2024-07-09 General Electric Company Gas turbine engine with third stream
US12577926B2 (en) 2022-08-02 2026-03-17 General Electric Company Gas turbine engine
US12565866B2 (en) 2022-08-02 2026-03-03 General Electric Company Gas turbine engine with third stream
US12421917B2 (en) 2022-08-02 2025-09-23 General Electric Company Gas turbine engine with third stream
US12577925B2 (en) 2022-08-02 2026-03-17 General Electric Company Gas turbine engine with third stream
US12571358B2 (en) 2022-08-02 2026-03-10 General Electric Company Gas turbine engine with third stream
US12410763B2 (en) 2022-08-02 2025-09-09 General Electric Company Gas turbine engine with third stream
US12618384B2 (en) 2022-08-02 2026-05-05 General Electric Company Gas turbine engine having a bypass passage, a fan duct, and a core duct
US12516647B2 (en) 2022-08-02 2026-01-06 General Electric Company Gas turbine engine with third stream

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Also Published As

Publication number Publication date
CN101267984A (zh) 2008-09-17
JP2009508748A (ja) 2009-03-05
BRPI0616104A2 (pt) 2011-06-07
FR2891242B1 (fr) 2007-10-26
US8167239B2 (en) 2012-05-01
RU2398714C2 (ru) 2010-09-10
DE602006004477D1 (de) 2009-02-05
EP1954563A1 (de) 2008-08-13
CN100526159C (zh) 2009-08-12
US20090078819A1 (en) 2009-03-26
EP1954563B1 (de) 2008-12-24
WO2007034094A1 (fr) 2007-03-29
CA2622151C (fr) 2013-06-11
RU2008115894A (ru) 2009-10-27
JP5087545B2 (ja) 2012-12-05
FR2891242A1 (fr) 2007-03-30
CA2622151A1 (fr) 2007-03-29

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Legal Events

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