FR3040076B1 - Ensemble moteur pour aeronef comprenant une structure primaire de mat d'accrochage equipee d'une extension de caisson comprenant deux parties en forme globale d'arceau - Google Patents
Ensemble moteur pour aeronef comprenant une structure primaire de mat d'accrochage equipee d'une extension de caisson comprenant deux parties en forme globale d'arceauInfo
- Publication number
- FR3040076B1 FR3040076B1 FR1557719A FR1557719A FR3040076B1 FR 3040076 B1 FR3040076 B1 FR 3040076B1 FR 1557719 A FR1557719 A FR 1557719A FR 1557719 A FR1557719 A FR 1557719A FR 3040076 B1 FR3040076 B1 FR 3040076B1
- Authority
- FR
- France
- Prior art keywords
- arceau
- global
- parts
- shape
- primary structure
- 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
Links
- 230000008878 coupling Effects 0.000 title 1
- 238000010168 coupling process Methods 0.000 title 1
- 238000005859 coupling reaction Methods 0.000 title 1
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
- B64D27/40—Arrangements for mounting power plants in 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
- 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
- B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
-
- 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
- B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type
- B64D27/12—Aircraft characterised by the type or position of power plants of gas-turbine type within, or attached to, wings
-
- 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
- B64D27/40—Arrangements for mounting power plants in aircraft
- B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
-
- 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
- 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
- F05D2240/90—Mounting on supporting structures or systems
-
- 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
-
- 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)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1557719A FR3040076B1 (fr) | 2015-08-13 | 2015-08-13 | Ensemble moteur pour aeronef comprenant une structure primaire de mat d'accrochage equipee d'une extension de caisson comprenant deux parties en forme globale d'arceau |
CA2937764A CA2937764A1 (fr) | 2015-08-13 | 2016-08-01 | Ensemble moteur d'aeronef comportant une premiere structure d'un pylone de montage equipe d'une rallonge de boite comportant deux parties de forme generale courbee |
US15/231,898 US10017267B2 (en) | 2015-08-13 | 2016-08-09 | Engine assembly for an aircraft comprising a primary structure of a mounting pylon equipped with a box extension comprising two parts in the overall shape of an arch |
CN201610665530.7A CN106428578B (zh) | 2015-08-13 | 2016-08-12 | 用于飞行器的发动机组件和包括此发动机组件的飞行器 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1557719A FR3040076B1 (fr) | 2015-08-13 | 2015-08-13 | Ensemble moteur pour aeronef comprenant une structure primaire de mat d'accrochage equipee d'une extension de caisson comprenant deux parties en forme globale d'arceau |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3040076A1 FR3040076A1 (fr) | 2017-02-17 |
FR3040076B1 true FR3040076B1 (fr) | 2017-08-11 |
Family
ID=54260994
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1557719A Active FR3040076B1 (fr) | 2015-08-13 | 2015-08-13 | Ensemble moteur pour aeronef comprenant une structure primaire de mat d'accrochage equipee d'une extension de caisson comprenant deux parties en forme globale d'arceau |
Country Status (4)
Country | Link |
---|---|
US (1) | US10017267B2 (fr) |
CN (1) | CN106428578B (fr) |
CA (1) | CA2937764A1 (fr) |
FR (1) | FR3040076B1 (fr) |
Families Citing this family (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2981046B1 (fr) * | 2011-10-06 | 2013-10-25 | Aircelle Sa | Ensemble propulsif d'aeronef |
FR3055669B1 (fr) | 2016-09-05 | 2018-09-28 | Airbus Operations | Systeme d'inverseur de poussee limitant les perturbations aerodynamiques en configuration inactive |
US10414509B2 (en) * | 2017-02-23 | 2019-09-17 | United Technologies Corporation | Propulsor mounting for advanced body aircraft |
FR3065441B1 (fr) * | 2017-04-19 | 2019-07-05 | Airbus Operations | Ensemble pour aeronef comprenant une structure primaire de mat d'accrochage fixee a un caisson de voilure a l'aide d'une liaison boulonnee |
US10723471B2 (en) * | 2017-06-14 | 2020-07-28 | General Electric Company | Method and system for mounting an aircraft engine |
FR3069848B1 (fr) * | 2017-08-02 | 2019-08-30 | Airbus | Structure primaire allegee pour mat d'accrochage de moteur d'aeronef |
FR3071820B1 (fr) * | 2017-10-03 | 2020-12-04 | Airbus Operations Sas | Ensemble moteur d'aeronef |
GB201804962D0 (en) | 2018-03-28 | 2018-05-09 | Rolls Royce Plc | A geared turbofan engine mount arrangement |
FR3084339A1 (fr) * | 2018-07-30 | 2020-01-31 | Airbus Operations | Ensemble pour un aeronef, l'ensemble comportant un mat et une attache moteur avant |
US11008884B2 (en) * | 2018-08-10 | 2021-05-18 | Rolls-Royce North American Technologies, Inc. | Gensets and methods of producing gensets from an engine and generator for hybrid electric propulsion |
FR3089954B1 (fr) * | 2018-12-12 | 2021-01-08 | Airbus Operations Sas | Ensemble de motorisation pour un aeronef comprenant un support de charge |
GB201900609D0 (en) * | 2019-01-16 | 2019-03-06 | Rolls Royce Plc | Mounting apparatus for gas turbine engine |
CN112776993A (zh) * | 2019-11-05 | 2021-05-11 | 中国航发商用航空发动机有限责任公司 | 一种飞机及其吊挂结构 |
EP3950507B1 (fr) * | 2020-08-04 | 2023-11-08 | Airbus SAS | Procédé d'assemblage d'un mât d'aéronef et mât d'aéronef obtenu à partir de ce procédé |
FR3114129B1 (fr) * | 2020-09-14 | 2022-08-05 | Safran Aircraft Engines | Ensemble comportant une turbomachine d’aeronef et son pylone d’accrochage |
FR3122644B1 (fr) * | 2021-05-04 | 2023-06-16 | Airbus Operations Sas | Assemblage d’une structure primaire d’un mât d’aéronef et d’une attache-moteur arrière comprenant au moins un élément de fixation latéral et aéronef comprenant au moins un tel assemblage |
FR3123377B1 (fr) * | 2021-05-27 | 2023-05-19 | Safran Aircraft Engines | Ensemble de supportage d’une boite d’accessoires d’une turbomachine d'aéronef |
GB202117777D0 (en) * | 2021-12-09 | 2022-01-26 | Rolls Royce Plc | Support structure for attaching a gas turbine engine to an aircraft pylon |
Family Cites Families (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5351930A (en) * | 1992-08-11 | 1994-10-04 | Lord Corporation | Mounting for engines and the like |
FR2738034B1 (fr) * | 1995-08-23 | 1997-09-19 | Snecma | Dispositif de suspension d'un turbopropulseur |
GB9602130D0 (en) | 1996-02-02 | 1996-04-03 | Rolls Royce Plc | Improved method of combining ducted fan gas turbine engine modules and aircraft structure |
US6607165B1 (en) * | 2002-06-28 | 2003-08-19 | General Electric Company | Aircraft engine mount with single thrust link |
FR2873985B1 (fr) * | 2004-08-04 | 2006-11-24 | Airbus France Sas | Ensemble moteur pour aeronef |
FR2878229B1 (fr) * | 2004-11-23 | 2008-04-18 | Airbus France Sas | Systeme de fixation d'un mat de moteur a l'aile d'un aeronef |
FR2885877B1 (fr) * | 2005-05-23 | 2008-12-12 | Airbus France Sas | Mat d'accrochage de turboreacteur pour aeronef |
FR2889163B1 (fr) * | 2005-07-29 | 2007-09-07 | Airbus France Sas | Ensemble pour aeronef comprenant un element de voilure ainsi qu'un mat d'accrochage |
FR2891247B1 (fr) * | 2005-09-26 | 2009-04-03 | Airbus France Sas | Ensemble pour aeronef comprenant un element de voilure ainsi qu'un mat d'accrochage |
FR2891245B1 (fr) * | 2005-09-26 | 2007-10-26 | Airbus France Sas | Procede de montage d'un moteur d'aeronef sur une structure rigide d'un mat d'accrochage du moteur |
FR2891254B1 (fr) * | 2005-09-29 | 2007-10-26 | Airbus France Sas | Ensemble moteur pour aeronef |
FR2891526B1 (fr) * | 2005-10-03 | 2007-11-02 | Airbus France Sas | Mat d'accrochage de turboreacteur pour aeronef |
US8256707B2 (en) * | 2007-08-01 | 2012-09-04 | United Technologies Corporation | Engine mounting configuration for a turbofan gas turbine engine |
FR2920409B1 (fr) * | 2007-08-27 | 2009-12-18 | Airbus France | Berceau de support de capot de soufflante monte sur le mat d'accrochage et sur l'entree d'air de la nacelle |
US8205825B2 (en) * | 2008-02-27 | 2012-06-26 | Spirit Aerosystems, Inc. | Engine pylon made from composite material |
FR2941673B1 (fr) * | 2009-02-04 | 2011-01-14 | Aircelle Sa | Ensemble de suspension pour turboreacteur d'aeronef |
FR2964364B1 (fr) * | 2010-09-03 | 2012-09-28 | Airbus Operations Sas | Mat d'accrochage de turboreacteur pour aeronef comprenant des attaches voilure avant alignees |
US20130074517A1 (en) * | 2011-09-23 | 2013-03-28 | United Technologies Corporation | Gas turbine engine mount assembly |
US9212607B2 (en) * | 2012-07-18 | 2015-12-15 | Spirit Aerosystems, Inc. | Intermediate structure for independently de-mountable propulsion components |
JP6114043B2 (ja) * | 2013-01-25 | 2017-04-12 | 三菱航空機株式会社 | 航空機のパイロン、及び、航空機 |
US9248921B2 (en) * | 2013-07-11 | 2016-02-02 | Spirit Aerosystems, Inc. | Method for mounting a pylon to an aircraft |
WO2015047539A1 (fr) * | 2013-09-27 | 2015-04-02 | United Technologies Corporation | Systèmes de montage pour moteurs à turbine à gaz |
FR3014841B1 (fr) | 2013-12-17 | 2017-12-08 | Airbus Operations Sas | Ensemble pour aeronef comprenant un corps d'attache moteur en partie realise d'une seule piece avec une nervure interieure de rigidification d'un caisson de mat d'accrochage |
FR3027875A1 (fr) * | 2014-10-30 | 2016-05-06 | Airbus Operations Sas | Dispositif de fixation d'un moteur d'aeronef, et aeronef correspondant |
-
2015
- 2015-08-13 FR FR1557719A patent/FR3040076B1/fr active Active
-
2016
- 2016-08-01 CA CA2937764A patent/CA2937764A1/fr not_active Abandoned
- 2016-08-09 US US15/231,898 patent/US10017267B2/en active Active
- 2016-08-12 CN CN201610665530.7A patent/CN106428578B/zh active Active
Also Published As
Publication number | Publication date |
---|---|
FR3040076A1 (fr) | 2017-02-17 |
US20170043878A1 (en) | 2017-02-16 |
CN106428578B (zh) | 2021-05-28 |
CN106428578A (zh) | 2017-02-22 |
US10017267B2 (en) | 2018-07-10 |
CA2937764A1 (fr) | 2017-02-13 |
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