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FR2935354B1 - Nacelle pour moteur a double flux - Google Patents

Nacelle pour moteur a double flux

Info

Publication number
FR2935354B1
FR2935354B1 FR0855880A FR0855880A FR2935354B1 FR 2935354 B1 FR2935354 B1 FR 2935354B1 FR 0855880 A FR0855880 A FR 0855880A FR 0855880 A FR0855880 A FR 0855880A FR 2935354 B1 FR2935354 B1 FR 2935354B1
Authority
FR
France
Prior art keywords
nacelle
double flow
flow motor
motor
double
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
FR0855880A
Other languages
English (en)
Other versions
FR2935354A1 (fr
Inventor
Olivier Teulou
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 FR0855880A priority Critical patent/FR2935354B1/fr
Priority to US12/551,648 priority patent/US8162257B2/en
Publication of FR2935354A1 publication Critical patent/FR2935354A1/fr
Application granted granted Critical
Publication of FR2935354B1 publication Critical patent/FR2935354B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • B64D29/00—Power-plant nacelles, fairings or cowlings
    • B64D29/06—Attaching of nacelles, fairings or cowlings
    • 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—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • 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
    • F02K1/76—Control or regulation of thrust reversers
    • F02K1/763—Control or regulation of thrust reversers with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
    • 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
    • F05D2260/50—Kinematic linkage, i.e. transmission of position

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Wind Motors (AREA)
FR0855880A 2008-02-09 2008-09-02 Nacelle pour moteur a double flux Active FR2935354B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0855880A FR2935354B1 (fr) 2008-09-02 2008-09-02 Nacelle pour moteur a double flux
US12/551,648 US8162257B2 (en) 2008-02-09 2009-09-01 Nacelle for double flow engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0855880A FR2935354B1 (fr) 2008-09-02 2008-09-02 Nacelle pour moteur a double flux

Publications (2)

Publication Number Publication Date
FR2935354A1 FR2935354A1 (fr) 2010-03-05
FR2935354B1 true FR2935354B1 (fr) 2011-04-01

Family

ID=40568507

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0855880A Active FR2935354B1 (fr) 2008-02-09 2008-09-02 Nacelle pour moteur a double flux

Country Status (2)

Country Link
US (1) US8162257B2 (fr)
FR (1) FR2935354B1 (fr)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2935444B1 (fr) * 2008-09-02 2010-09-10 Airbus France Inverseur de poussee et nacelle pour aeronef muni d'au moins un tel inverseur
FR2959531B1 (fr) * 2010-04-28 2015-12-18 Aircelle Sa Inverseur a portes
FR2962977B1 (fr) * 2010-07-20 2012-08-17 Airbus Operations Sas Nacelle pour aeronef
FR2978126B1 (fr) * 2011-07-22 2013-09-27 Airbus Operations Sas Nacelle pour ensemble propulsif a tuyere a section variable
US9181898B2 (en) * 2011-09-20 2015-11-10 United Technologies Corporation Thrust reverser for a gas turbine engine with moveable doors
ES2401015B1 (es) * 2011-09-29 2014-03-13 Airbus Operations, S.L. Toma de aire con doble compuerta
US9623976B2 (en) * 2012-07-25 2017-04-18 Rohr, Inc. Nacelle for a high bypass ratio engine with multiple flow paths
US9945324B2 (en) * 2014-11-06 2018-04-17 Rohr, Inc. Sleeve linkage for thrust reverser
US10113508B2 (en) * 2014-11-21 2018-10-30 General Electric Company Gas turbine engine and method of assembling the same
US10465538B2 (en) 2014-11-21 2019-11-05 General Electric Company Gas turbine engine with reversible fan
US20170198658A1 (en) * 2016-01-11 2017-07-13 The Boeing Company Thrust reverser
US10267262B2 (en) 2016-05-06 2019-04-23 Mra Systems, Llc Thrust reverser assembly
US10563615B2 (en) 2016-05-09 2020-02-18 Mra Systems, Llc Gas turbine engine with thrust reverser assembly and method of operating
FR3055669B1 (fr) 2016-09-05 2018-09-28 Airbus Operations Systeme d'inverseur de poussee limitant les perturbations aerodynamiques en configuration inactive
FR3067406B1 (fr) 2017-06-13 2019-07-12 Airbus Operations Systeme d'inverseur de poussee presentant des perturbations aerodynamiques limitees
FR3068081B1 (fr) 2017-06-21 2020-10-16 Airbus Operations Sas Systeme d'inverseur de poussee presentant des perturbations aerodynamiques limitees
US10794328B2 (en) * 2018-07-06 2020-10-06 Rohr, Inc. Thrust reverser with blocker door folding linkage
FR3087422B1 (fr) * 2018-10-23 2021-10-01 Airbus Operations Sas Ensemble turbomachine d’aeronef comportant un capot articule
US11155343B2 (en) * 2018-12-17 2021-10-26 The Boeing Company Brake systems for aircraft and related methods
FR3107932B1 (fr) * 2020-03-09 2022-08-12 Safran Aircraft Engines Sortie d’air de nacelle pour turboréacteur d’aéronef à double flux comprenant un dispositif de guidage pour favoriser une phase d’inversion de poussée
US11754018B2 (en) * 2021-12-17 2023-09-12 Rohr, Inc. Aircraft propulsion system exhaust nozzle with ejector passage(s)

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2146109A1 (fr) * 1971-07-19 1973-03-02 Bruner Georges
US3829020A (en) * 1973-06-13 1974-08-13 Boeing Co Translating sleeve variable area nozzle and thrust reverser
FR2618391B1 (fr) * 1987-07-22 1991-12-06 Aeroplast Sarl Ensemble de direction et de freinage pour vehicules propulses par jets de fluide
US5987880A (en) * 1997-07-08 1999-11-23 Mcdonnell Douglas Corporation Supersonic engine, multi-port thrust reversing system
FR2812035B1 (fr) * 2000-07-24 2003-08-29 Hurel Dubois Avions Perfectionnements aux inverseurs de poussee pour moteurs a reaction, du type a grilles
WO2004046533A2 (fr) * 2002-10-11 2004-06-03 The Nordam Group, Inc. Inverseur de poussee a volet double pliant
FR2887225B1 (fr) 2005-06-21 2008-09-19 Airbus France Sas Nacelle d'aeronef, et aeronef muni d'au moins une telle nacelle
US7559507B2 (en) * 2005-06-27 2009-07-14 The Boeing Company Thrust reversers including locking assemblies for inhibiting deflection
EP2074320B1 (fr) * 2006-10-12 2013-06-26 United Technologies Corporation Inverseur de poussée pour buse à jet pinceau à section variable

Also Published As

Publication number Publication date
US8162257B2 (en) 2012-04-24
FR2935354A1 (fr) 2010-03-05
US20100072324A1 (en) 2010-03-25

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Effective date: 20110916

CD Change of name or company name

Owner name: AIRBUS HOLDING, FR

Effective date: 20110916

CJ Change in legal form

Effective date: 20110916

TP Transmission of property

Owner name: AIRBUS HOLDING, FR

Effective date: 20110913

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