FR2955154B1 - Inverseur de poussee pour aeronef a turboreacteurs a double flux semi-enterres - Google Patents

Inverseur de poussee pour aeronef a turboreacteurs a double flux semi-enterres

Info

Publication number
FR2955154B1
FR2955154B1 FR1050093A FR1050093A FR2955154B1 FR 2955154 B1 FR2955154 B1 FR 2955154B1 FR 1050093 A FR1050093 A FR 1050093A FR 1050093 A FR1050093 A FR 1050093A FR 2955154 B1 FR2955154 B1 FR 2955154B1
Authority
FR
France
Prior art keywords
burial
double flow
thrust inverter
flow semi
turbo
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
FR1050093A
Other languages
English (en)
Other versions
FR2955154A1 (fr
Inventor
Jacques Herve Marche
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
Priority to FR1050093A priority Critical patent/FR2955154B1/fr
Priority to US13/520,917 priority patent/US9062626B2/en
Priority to PCT/FR2010/052918 priority patent/WO2011083256A1/fr
Publication of FR2955154A1 publication Critical patent/FR2955154A1/fr
Application granted granted Critical
Publication of FR2955154B1 publication Critical patent/FR2955154B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/56—Reversing jet main flow
    • F02K1/62—Reversing jet main flow by blocking the rearward discharge by means of flaps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/90—Braking
    • 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
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1050093A 2010-01-08 2010-01-08 Inverseur de poussee pour aeronef a turboreacteurs a double flux semi-enterres Expired - Fee Related FR2955154B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1050093A FR2955154B1 (fr) 2010-01-08 2010-01-08 Inverseur de poussee pour aeronef a turboreacteurs a double flux semi-enterres
US13/520,917 US9062626B2 (en) 2010-01-08 2010-12-27 Thrust reverser for an aircraft having semi-recessed turbofan engines
PCT/FR2010/052918 WO2011083256A1 (fr) 2010-01-08 2010-12-27 Inverseur de poussée pour aéronef à turboréacteurs à double flux semi-enterrés

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1050093A FR2955154B1 (fr) 2010-01-08 2010-01-08 Inverseur de poussee pour aeronef a turboreacteurs a double flux semi-enterres

Publications (2)

Publication Number Publication Date
FR2955154A1 FR2955154A1 (fr) 2011-07-15
FR2955154B1 true FR2955154B1 (fr) 2012-01-06

Family

ID=42350361

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1050093A Expired - Fee Related FR2955154B1 (fr) 2010-01-08 2010-01-08 Inverseur de poussee pour aeronef a turboreacteurs a double flux semi-enterres

Country Status (3)

Country Link
US (1) US9062626B2 (fr)
FR (1) FR2955154B1 (fr)
WO (1) WO2011083256A1 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10161358B2 (en) * 2013-03-14 2018-12-25 United Technologies Corporation Twin target thrust reverser module
PL235797B1 (pl) 2018-02-21 2020-10-19 Gen Electric Zespół dyszy dzwonowej do silników turbogazowych oraz sposób odwracania ciągu silnika turbowentylatorowego
US11286879B2 (en) * 2018-07-02 2022-03-29 Rohr, Inc. Target door reverser wit h non-parallel hinge lines
GB2599686A (en) * 2020-10-09 2022-04-13 Rolls Royce Plc An improved turbofan gas turbine engine

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3658279A (en) * 1970-04-21 1972-04-25 Lockheed Aircraft Corp Integrated propulsion system
US4030687A (en) * 1976-02-23 1977-06-21 The Boeing Company Articulated nozzle for upper surface blown aircraft
GB1534583A (en) * 1976-06-08 1978-12-06 Short Bros Ltd Reversal of thrust in gas turbine engines
FR2698913B1 (fr) 1992-12-04 1995-02-03 Hurel Dubois Avions Ensemble d'inversion de poussée à portes équipé d'un dispositif de contrôle de jet.
FR2741114B1 (fr) 1995-11-15 1997-12-05 Hispano Suiza Sa Inverseur de poussee de turboreacteur a obstacles aval tendant a l'equilibrage
FR2757901B1 (fr) 1996-12-26 1999-01-29 Hispano Suiza Sa Inverseur de poussee de turboreacteur a double flux a coquilles aval
FR2812035B1 (fr) 2000-07-24 2003-08-29 Hurel Dubois Avions Perfectionnements aux inverseurs de poussee pour moteurs a reaction, du type a grilles
FR2914956A1 (fr) 2007-04-12 2008-10-17 Aircelle Sa Nacelle pour turboreacteur equipee d'un systeme d'inversion de poussee a porte

Also Published As

Publication number Publication date
US20130097998A1 (en) 2013-04-25
FR2955154A1 (fr) 2011-07-15
US9062626B2 (en) 2015-06-23
WO2011083256A1 (fr) 2011-07-14

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