FR3016863B1 - Nacelle pour turboreacteur d'avion - Google Patents

Nacelle pour turboreacteur d'avion

Info

Publication number
FR3016863B1
FR3016863B1 FR1450687A FR1450687A FR3016863B1 FR 3016863 B1 FR3016863 B1 FR 3016863B1 FR 1450687 A FR1450687 A FR 1450687A FR 1450687 A FR1450687 A FR 1450687A FR 3016863 B1 FR3016863 B1 FR 3016863B1
Authority
FR
France
Prior art keywords
aircraft
nacelle
turbo
aircraft turbo
turbo aircraft
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
FR1450687A
Other languages
English (en)
Other versions
FR3016863A1 (fr
Inventor
Vulpillieres Eric De
Gaetan Jean Mabboux
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA 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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR1450687A priority Critical patent/FR3016863B1/fr
Priority to PCT/FR2015/050175 priority patent/WO2015114241A1/fr
Priority to US15/114,554 priority patent/US10273016B2/en
Publication of FR3016863A1 publication Critical patent/FR3016863A1/fr
Application granted granted Critical
Publication of FR3016863B1 publication Critical patent/FR3016863B1/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; ARRANGEMENTS 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; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/16—Aircraft characterised by the type or position of power plant of jet type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • 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
    • F02K1/60—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers
    • 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
    • F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
    • 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
    • F02K1/78—Other construction of jet pipes
    • F02K1/80—Couplings or connections
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
    • 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
    • F05D2240/14—Casings or housings protecting or supporting assemblies within
    • 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
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/24—Three-dimensional ellipsoidal
    • F05D2250/241—Three-dimensional ellipsoidal spherical
    • 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
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/26—Three-dimensional paraboloid
    • 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
    • F05D2250/00—Geometry
    • F05D2250/60—Structure; Surface texture
    • F05D2250/61—Structure; Surface texture corrugated
    • 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
    • F05D2250/00—Geometry
    • F05D2250/70—Shape
    • F05D2250/71—Shape curved
    • F05D2250/711—Shape curved convex
FR1450687A 2014-01-29 2014-01-29 Nacelle pour turboreacteur d'avion Active FR3016863B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1450687A FR3016863B1 (fr) 2014-01-29 2014-01-29 Nacelle pour turboreacteur d'avion
PCT/FR2015/050175 WO2015114241A1 (fr) 2014-01-29 2015-01-26 Nacelle pour turboréacteur d'avion
US15/114,554 US10273016B2 (en) 2014-01-29 2015-01-26 Nacelle for an airplane turbojet

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1450687A FR3016863B1 (fr) 2014-01-29 2014-01-29 Nacelle pour turboreacteur d'avion

Publications (2)

Publication Number Publication Date
FR3016863A1 FR3016863A1 (fr) 2015-07-31
FR3016863B1 true FR3016863B1 (fr) 2017-05-26

Family

ID=50424598

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1450687A Active FR3016863B1 (fr) 2014-01-29 2014-01-29 Nacelle pour turboreacteur d'avion

Country Status (3)

Country Link
US (1) US10273016B2 (fr)
FR (1) FR3016863B1 (fr)
WO (1) WO2015114241A1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10927792B2 (en) * 2018-06-22 2021-02-23 The Boeing Company Jet noise suppressor
US11187187B2 (en) * 2018-08-06 2021-11-30 Rohr, Inc. Thrust reverser

Family Cites Families (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4298089A (en) * 1976-12-23 1981-11-03 The Boeing Company Vortex generators for internal mixing in a turbofan engine
US4194692A (en) * 1977-08-05 1980-03-25 Rohr Industries, Inc. Flight thrust reverser and vertical thrust control divergent nozzle systems
US4238092A (en) * 1978-08-17 1980-12-09 Rohr Industries, Inc. Accessory for a turbine engine
US4447028A (en) * 1979-01-02 1984-05-08 The Boeing Company Upper surface blown powered lift system for aircraft
FR2486153B1 (fr) * 1980-07-04 1985-10-04 Hurel Dubois Avions Inverseur de poussee pour moteur a reaction, destine notamment a equiper un aeronef
US4407120A (en) * 1980-08-25 1983-10-04 Rohr Industries, Inc. Thrust reverser geared linkage
FR2622928A1 (fr) * 1987-11-05 1989-05-12 Hispano Suiza Sa Inverseur de poussee de turboreacteur a portes,a section variable d'ejection
US5529263A (en) * 1992-10-21 1996-06-25 The Boeing Company Supersonic airplane with subsonic boost engine means and method of operating the same
FR2704907B1 (fr) * 1993-05-06 1995-06-09 Hispano Suiza Sa Systeme auto-bloquant de commande des portes d'inverseur de poussee d'un turboreacteur.
US5598990A (en) * 1994-12-15 1997-02-04 University Of Kansas Center For Research Inc. Supersonic vortex generator
FR2741114B1 (fr) 1995-11-15 1997-12-05 Hispano Suiza Sa Inverseur de poussee de turboreacteur a obstacles aval tendant a l'equilibrage
GB9613166D0 (en) * 1996-06-24 1996-08-28 Short Brothers Plc Aircraft propulsive power unit
GB0321139D0 (en) * 2003-09-10 2003-10-08 Short Brothers Plc A device
FR2901243B1 (fr) * 2006-05-16 2008-06-27 Airbus France Sas Dispositif d'accrochage d'un moteur d'aeronef
US8151551B2 (en) * 2006-10-12 2012-04-10 United Technologies Corporation Variable area fan nozzle thrust reverser
US7870722B2 (en) * 2006-12-06 2011-01-18 The Boeing Company Systems and methods for passively directing aircraft engine nozzle flows
WO2008150202A1 (fr) * 2007-06-08 2008-12-11 Volvo Aero Corporation Structure de transfert de charges au niveau d'une turbine à gaz, et turbine et aéronef comportant une telle structure
WO2009029401A2 (fr) * 2007-08-08 2009-03-05 Rohr, Inc. Buse de ventilateur à surface variable avec écoulement de dérivation
FR2933070B1 (fr) * 2008-06-25 2010-08-20 Snecma Systeme propulsif d'aeronef
FR2950860B1 (fr) * 2009-10-01 2011-12-09 Airbus Operations Sas Dispositif d'accrochage d'un moteur a un mat d'aeronef
FR2962977B1 (fr) * 2010-07-20 2012-08-17 Airbus Operations Sas Nacelle pour aeronef
FR2970520B1 (fr) * 2011-01-14 2015-03-27 Aircelle Sa Porte pour inverseur de poussee d’une nacelle d’un aeronef
US9429071B2 (en) * 2011-06-23 2016-08-30 Continuum Dynamics, Inc. Supersonic engine inlet diffuser with deployable vortex generators
US9617009B2 (en) * 2013-02-22 2017-04-11 United Technologies Corporation ATR full ring sliding nacelle
US9631578B2 (en) * 2013-02-22 2017-04-25 United Technologies Corporation Pivot thrust reverser surrounding inner surface of bypass duct
US9771894B2 (en) * 2013-10-07 2017-09-26 Rohr, Inc. Radially connected cascade grids
PL417165A1 (pl) * 2016-05-12 2017-11-20 Mra Systems, Inc. Zespół odwracacza ciągu

Also Published As

Publication number Publication date
WO2015114241A1 (fr) 2015-08-06
US10273016B2 (en) 2019-04-30
FR3016863A1 (fr) 2015-07-31
US20160340052A1 (en) 2016-11-24

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