CN1993267A - 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
- CN1993267A CN1993267A CNA2005800262272A CN200580026227A CN1993267A CN 1993267 A CN1993267 A CN 1993267A CN A2005800262272 A CNA2005800262272 A CN A2005800262272A CN 200580026227 A CN200580026227 A CN 200580026227A CN 1993267 A CN1993267 A CN 1993267A
- Authority
- CN
- China
- Prior art keywords
- arch
- aircraft
- attaching parts
- turbine engine
- assembly
- 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.)
- Granted
Links
- 238000011084 recovery Methods 0.000 claims abstract description 14
- 238000007664 blowing Methods 0.000 claims description 29
- 238000010276 construction Methods 0.000 claims description 26
- 230000002093 peripheral effect Effects 0.000 claims description 18
- 238000012423 maintenance Methods 0.000 claims description 9
- 230000000712 assembly Effects 0.000 claims 1
- 238000000429 assembly Methods 0.000 claims 1
- 230000015572 biosynthetic process Effects 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 true CN1993267A (zh) | 2007-07-04 |
CN1993267B 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) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101945808A (zh) * | 2008-02-28 | 2011-01-12 | 空中客车运作股份公司 | 包括在风扇壳体上向下偏移的发动机紧固件的用于飞行器的发动机组件 |
CN101959758A (zh) * | 2008-02-28 | 2011-01-26 | 空中客车运作股份公司 | 包括包围涡轮喷气发动机的中央机壳的用于传递力的环形结构的用于飞行器的发动机组件 |
CN102076563A (zh) * | 2008-06-25 | 2011-05-25 | 斯奈克玛 | 飞行器推进*** |
CN102498038A (zh) * | 2009-09-22 | 2012-06-13 | 空中客车营运有限公司 | 飞行器发动机的悬挂支柱,包括所述支柱的组件及相关联的飞行器 |
CN101469647B (zh) * | 2007-11-23 | 2012-11-28 | 斯奈克玛 | 悬挂在飞机外挂梁上的涡轮喷气发动机 |
CN101959759B (zh) * | 2008-02-28 | 2013-03-06 | 空中客车运作股份公司 | 包括具有将风扇壳体连接至中央壳体的加固结构的涡轮喷气发动机的用于飞行器的发动机组件 |
CN102066198B (zh) * | 2008-06-25 | 2013-07-31 | 埃尔塞乐公司 | 飞行器发动机舱进气口组件 |
CN103277194A (zh) * | 2011-12-22 | 2013-09-04 | 劳斯莱斯有限公司 | 维修燃气涡轮发动机的方法 |
CN102026871B (zh) * | 2008-05-14 | 2013-12-18 | 空中客车运作股份公司 | 包括具有圆形或椭圆形截面的箱体的用于飞行器发动机的悬挂架 |
Families Citing this family (18)
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 |
US8205825B2 (en) * | 2008-02-27 | 2012-06-26 | Spirit Aerosystems, Inc. | Engine pylon made from composite material |
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 |
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 |
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 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3848832A (en) * | 1973-03-09 | 1974-11-19 | Boeing Co | Aircraft engine installation |
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 |
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 |
GB2303884B (en) * | 1995-04-13 | 1999-07-14 | Rolls Royce Plc | A mounting for coupling a turbofan gas turbine engine to an aircraft structure |
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
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101469647B (zh) * | 2007-11-23 | 2012-11-28 | 斯奈克玛 | 悬挂在飞机外挂梁上的涡轮喷气发动机 |
CN101945808A (zh) * | 2008-02-28 | 2011-01-12 | 空中客车运作股份公司 | 包括在风扇壳体上向下偏移的发动机紧固件的用于飞行器的发动机组件 |
CN101959758A (zh) * | 2008-02-28 | 2011-01-26 | 空中客车运作股份公司 | 包括包围涡轮喷气发动机的中央机壳的用于传递力的环形结构的用于飞行器的发动机组件 |
CN101959759B (zh) * | 2008-02-28 | 2013-03-06 | 空中客车运作股份公司 | 包括具有将风扇壳体连接至中央壳体的加固结构的涡轮喷气发动机的用于飞行器的发动机组件 |
CN102026871B (zh) * | 2008-05-14 | 2013-12-18 | 空中客车运作股份公司 | 包括具有圆形或椭圆形截面的箱体的用于飞行器发动机的悬挂架 |
CN102076563A (zh) * | 2008-06-25 | 2011-05-25 | 斯奈克玛 | 飞行器推进*** |
CN102066198B (zh) * | 2008-06-25 | 2013-07-31 | 埃尔塞乐公司 | 飞行器发动机舱进气口组件 |
CN102076563B (zh) * | 2008-06-25 | 2014-11-05 | 斯奈克玛 | 飞行器推进*** |
CN102498038A (zh) * | 2009-09-22 | 2012-06-13 | 空中客车营运有限公司 | 飞行器发动机的悬挂支柱,包括所述支柱的组件及相关联的飞行器 |
CN102498038B (zh) * | 2009-09-22 | 2014-11-12 | 空中客车营运有限公司 | 飞行器发动机的悬挂支柱,包括所述支柱的组件及相关联的飞行器 |
CN103277194A (zh) * | 2011-12-22 | 2013-09-04 | 劳斯莱斯有限公司 | 维修燃气涡轮发动机的方法 |
CN103277194B (zh) * | 2011-12-22 | 2016-12-28 | 劳斯莱斯有限公司 | 维修燃气涡轮发动机的方法 |
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 |
CN1993267B (zh) | 2011-07-06 |
WO2006090031A1 (fr) | 2006-08-31 |
CA2576095C (fr) | 2013-09-24 |
JP2008509320A (ja) | 2008-03-27 |
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 |