CN1993267B - 用于飞行器的发动机组件 - Google Patents
用于飞行器的发动机组件 Download PDFInfo
- Publication number
- CN1993267B CN1993267B CN2005800262272A CN200580026227A CN1993267B CN 1993267 B CN1993267 B CN 1993267B CN 2005800262272 A CN2005800262272 A CN 2005800262272A CN 200580026227 A CN200580026227 A CN 200580026227A CN 1993267 B CN1993267 B CN 1993267B
- Authority
- CN
- China
- Prior art keywords
- arch
- attaching parts
- turbine engine
- assembly
- 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
Links
- 238000007664 blowing Methods 0.000 claims description 30
- 238000010276 construction Methods 0.000 claims description 26
- 230000002093 peripheral effect Effects 0.000 claims description 18
- 238000012423 maintenance Methods 0.000 claims description 11
- 238000012797 qualification Methods 0.000 claims 2
- 230000000712 assembly Effects 0.000 claims 1
- 238000000429 assembly Methods 0.000 claims 1
- 230000015572 biosynthetic process Effects 0.000 claims 1
- 239000000725 suspension Substances 0.000 claims 1
- 238000005452 bending Methods 0.000 description 11
- 238000013461 design Methods 0.000 description 5
- 238000009434 installation Methods 0.000 description 5
- 238000003466 welding Methods 0.000 description 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 238000002955 isolation Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000002787 reinforcement Effects 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 230000000747 cardiac effect Effects 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
Images
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
- B64D27/40—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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
- Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
- Supercharger (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Retarders (AREA)
Abstract
Description
Claims (17)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0451790A FR2873987B1 (fr) | 2004-08-05 | 2004-08-05 | Ensemble moteur pour aeronef |
FR0451790 | 2004-08-05 | ||
PCT/FR2005/050644 WO2006090031A1 (fr) | 2004-08-05 | 2005-08-03 | Ensemble moteur pour aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
CN1993267A CN1993267A (zh) | 2007-07-04 |
CN1993267B true CN1993267B (zh) | 2011-07-06 |
Family
ID=34948382
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2005800262272A Active CN1993267B (zh) | 2004-08-05 | 2005-08-03 | 用于飞行器的发动机组件 |
Country Status (11)
Country | Link |
---|---|
US (1) | US7740200B2 (zh) |
EP (1) | EP1773661B1 (zh) |
JP (1) | JP4699462B2 (zh) |
CN (1) | CN1993267B (zh) |
AT (1) | ATE428632T1 (zh) |
BR (1) | BRPI0513893A (zh) |
CA (1) | CA2576095C (zh) |
DE (1) | DE602005013965D1 (zh) |
FR (1) | FR2873987B1 (zh) |
RU (1) | RU2383473C2 (zh) |
WO (1) | WO2006090031A1 (zh) |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2903076B1 (fr) * | 2006-06-30 | 2009-05-29 | Aircelle Sa | Nacelle structurante |
GB0622405D0 (en) | 2006-11-10 | 2006-12-20 | Rolls Royce Plc | A turbine engine mounting arrangement |
FR2909974B1 (fr) * | 2006-12-13 | 2009-02-06 | Aircelle Sa | Nacelle pour turboreacteur double flux |
FR2917710A1 (fr) * | 2007-06-22 | 2008-12-26 | Aircelle Sa | Platine de fixation et longeron de manutention d'ensemble propulsif monobloc d'un aeronef |
FR2924094B1 (fr) * | 2007-11-23 | 2010-01-15 | Snecma | Turboreacteur suspendu a un pylone d'aeronef |
US8205825B2 (en) * | 2008-02-27 | 2012-06-26 | Spirit Aerosystems, Inc. | Engine pylon made from composite material |
FR2928181B1 (fr) * | 2008-02-28 | 2010-04-02 | Airbus France | Ensemble moteur pour aeronef comprenant un turboreacteur avec des structures de renfort reliant le carter de soufflante au carter central. |
FR2928180B1 (fr) * | 2008-02-28 | 2010-04-02 | Airbus France | Ensemble moteur pour aeronef comprenant une structure annulaire de transfert d'efforts entourant le carter central d'un turboreacteur. |
FR2928136B1 (fr) * | 2008-02-28 | 2010-04-02 | Airbus France | Ensemble moteur pour aeronef comprenant des attaches moteur deportees vers le bas sur le carter de soufflante. |
FR2931134B1 (fr) * | 2008-05-14 | 2010-06-18 | Airbus France | Mat d'accrochage de moteur d'aeronef comprenant un caisson de section en forme de cercle ou d'ellipse |
FR2933070B1 (fr) * | 2008-06-25 | 2010-08-20 | Snecma | Systeme propulsif d'aeronef |
FR2933073B1 (fr) * | 2008-06-25 | 2010-06-04 | Aircelle Sa | Ensemble d'entree d'air de nacelle de moteur d'avion |
FR2936493A1 (fr) * | 2008-10-01 | 2010-04-02 | Aircelle Sa | Mat adapte pour supporter un turboracteur d'aeronef et nacelle associee a un mat. |
FR2942513B1 (fr) * | 2009-02-20 | 2011-05-27 | Airbus France | Aube pour recepteur de turbomachine, comprenant une partie pale integrant un fusible mecanique |
FR2950323B1 (fr) * | 2009-09-22 | 2011-11-04 | Airbus Operations Sas | Mat d'accrochage de moteur d'aeronef, ensemble comprenant ce mat et aeronef associe |
FR2950322B1 (fr) | 2009-09-22 | 2012-05-25 | Airbus Operations Sas | Element d'accrochage d'un moteur d'aeronef, ensemble d'aeronef comprenant cet element et aeronef associe |
FR2950860B1 (fr) | 2009-10-01 | 2011-12-09 | Airbus Operations Sas | Dispositif d'accrochage d'un moteur a un mat d'aeronef |
US8672260B2 (en) * | 2009-12-02 | 2014-03-18 | United Technologies Corporation | Single plane mount system for gas turbine engine |
GB2497809B (en) * | 2011-12-22 | 2014-03-12 | Rolls Royce Plc | Method of servicing a gas turbine engine |
FR2994942B1 (fr) * | 2012-09-06 | 2015-08-07 | Airbus Operations Sas | Ensemble propulsif lateral pour aeronef comprenant un arceau de support d'un turbomoteur. |
US9211955B1 (en) * | 2012-12-10 | 2015-12-15 | The Boeing Company | Methods and apparatus for supporting engines and nacelles relative to aircraft wings |
US10266273B2 (en) | 2013-07-26 | 2019-04-23 | Mra Systems, Llc | Aircraft engine pylon |
US9238511B2 (en) | 2014-03-04 | 2016-01-19 | Mra Systems, Inc. | Engine pylon structure |
US20160167798A1 (en) * | 2014-12-12 | 2016-06-16 | General Electric Company | Variable pitch mounting for aircraft gas turbine engine |
FR3045570B1 (fr) | 2015-12-16 | 2017-12-22 | Airbus Operations Sas | Ensemble moteur pour aeronef, comprenant un dispositif d'accrochage du moteur equipe d'une enveloppe structurale fixee sur un caisson central |
FR3106126B1 (fr) * | 2020-01-10 | 2022-01-07 | Safran Aircraft Engines | Assemblage entre un pylône d’aéronef et une turbomachine |
US11613372B2 (en) | 2020-11-09 | 2023-03-28 | Rohr, Inc. | Ducted fan case attachment structure |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3848832A (en) * | 1973-03-09 | 1974-11-19 | Boeing Co | Aircraft engine installation |
US3979087A (en) * | 1975-07-02 | 1976-09-07 | United Technologies Corporation | Engine mount |
US4266741A (en) * | 1978-05-22 | 1981-05-12 | The Boeing Company | Mounting apparatus for fan jet engine having mixed flow nozzle installation |
US5746391A (en) * | 1995-04-13 | 1998-05-05 | Rolls-Royce Plc | Mounting for coupling a turbofan gas turbine engine to an aircraft structure |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3952973A (en) * | 1974-12-20 | 1976-04-27 | The Boeing Company | Engine mounting assembly |
GB1516980A (en) * | 1974-12-24 | 1978-07-05 | Rolls Royce | Mounting ducted fan gas turbine engines on aircraft |
US6309131B1 (en) * | 1998-10-29 | 2001-10-30 | General Electric Company | Redundant clevis pin pair |
-
2004
- 2004-08-05 FR FR0451790A patent/FR2873987B1/fr not_active Expired - Fee Related
-
2005
- 2005-08-03 CN CN2005800262272A patent/CN1993267B/zh active Active
- 2005-08-03 AT AT05856228T patent/ATE428632T1/de not_active IP Right Cessation
- 2005-08-03 JP JP2007524382A patent/JP4699462B2/ja not_active Expired - Fee Related
- 2005-08-03 EP EP05856228A patent/EP1773661B1/fr not_active Not-in-force
- 2005-08-03 WO PCT/FR2005/050644 patent/WO2006090031A1/fr active Application Filing
- 2005-08-03 CA CA2576095A patent/CA2576095C/fr not_active Expired - Fee Related
- 2005-08-03 DE DE602005013965T patent/DE602005013965D1/de active Active
- 2005-08-03 BR BRPI0513893-0A patent/BRPI0513893A/pt active Search and Examination
- 2005-08-03 RU RU2007107928/11A patent/RU2383473C2/ru not_active IP Right Cessation
- 2005-08-03 US US11/572,213 patent/US7740200B2/en not_active Expired - Fee Related
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3848832A (en) * | 1973-03-09 | 1974-11-19 | Boeing Co | Aircraft engine installation |
US3979087A (en) * | 1975-07-02 | 1976-09-07 | United Technologies Corporation | Engine mount |
US4266741A (en) * | 1978-05-22 | 1981-05-12 | The Boeing Company | Mounting apparatus for fan jet engine having mixed flow nozzle installation |
US5746391A (en) * | 1995-04-13 | 1998-05-05 | Rolls-Royce Plc | Mounting for coupling a turbofan gas turbine engine to an aircraft structure |
Also Published As
Publication number | Publication date |
---|---|
EP1773661A1 (fr) | 2007-04-18 |
FR2873987B1 (fr) | 2006-11-24 |
CA2576095A1 (fr) | 2006-08-31 |
RU2383473C2 (ru) | 2010-03-10 |
JP4699462B2 (ja) | 2011-06-08 |
DE602005013965D1 (de) | 2009-05-28 |
WO2006090031A1 (fr) | 2006-08-31 |
CA2576095C (fr) | 2013-09-24 |
JP2008509320A (ja) | 2008-03-27 |
CN1993267A (zh) | 2007-07-04 |
US20080042008A1 (en) | 2008-02-21 |
ATE428632T1 (de) | 2009-05-15 |
FR2873987A1 (fr) | 2006-02-10 |
BRPI0513893A (pt) | 2008-05-20 |
RU2007107928A (ru) | 2008-09-10 |
US7740200B2 (en) | 2010-06-22 |
EP1773661B1 (fr) | 2009-04-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
ASS | Succession or assignment of patent right |
Owner name: AIRBUS OPERATIONS S.A.S. Free format text: FORMER OWNER: AIRBUS FRANCE Effective date: 20120116 |
|
C41 | Transfer of patent application or patent right or utility model | ||
TR01 | Transfer of patent right |
Effective date of registration: 20120116 Address after: France Toulouse Patentee after: Airbus Operations S.A.S. Address before: France Toulouse Patentee before: Airbus France Effective date of registration: 20120116 Address after: France Toulouse Patentee after: AIRBUS FRANCE Address before: France Toulouse Patentee before: Airbus France |