CN1993268A - 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
- CN1993268A CN1993268A CNA2005800263171A CN200580026317A CN1993268A CN 1993268 A CN1993268 A CN 1993268A CN A2005800263171 A CNA2005800263171 A CN A2005800263171A CN 200580026317 A CN200580026317 A CN 200580026317A CN 1993268 A CN1993268 A CN 1993268A
- Authority
- CN
- China
- Prior art keywords
- attaching parts
- engine
- power
- recover
- anterior
- 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
- 238000010276 construction Methods 0.000 claims description 17
- 230000008878 coupling Effects 0.000 claims description 16
- 238000010168 coupling process Methods 0.000 claims description 16
- 238000005859 coupling reaction Methods 0.000 claims description 16
- 238000007664 blowing Methods 0.000 claims description 13
- 230000002093 peripheral effect Effects 0.000 claims description 6
- 238000011084 recovery Methods 0.000 description 13
- 238000009434 installation Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000000712 assembly Effects 0.000 description 2
- 238000000429 assembly Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 239000002184 metal Substances 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)
- Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
- Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
- Vibration Prevention Devices (AREA)
- Air Bags (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Gas-Insulated Switchgears (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Description
Claims (7)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0451784 | 2004-08-04 | ||
FR0451784A FR2873985B1 (fr) | 2004-08-04 | 2004-08-04 | Ensemble moteur pour aeronef |
PCT/FR2005/050637 WO2006021721A1 (fr) | 2004-08-04 | 2005-08-01 | Ensemble moteur pour aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
CN1993268A true CN1993268A (zh) | 2007-07-04 |
CN1993268B CN1993268B (zh) | 2011-06-15 |
Family
ID=34947592
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2005800263171A Expired - Fee Related CN1993268B (zh) | 2004-08-04 | 2005-08-01 | 用于飞行器的发动机组件 |
Country Status (11)
Country | Link |
---|---|
US (1) | US7624945B2 (zh) |
EP (1) | EP1773660B1 (zh) |
JP (1) | JP4676982B2 (zh) |
CN (1) | CN1993268B (zh) |
AT (1) | ATE416975T1 (zh) |
BR (1) | BRPI0513867A (zh) |
CA (1) | CA2576518C (zh) |
DE (1) | DE602005011633D1 (zh) |
FR (1) | FR2873985B1 (zh) |
RU (1) | RU2381149C2 (zh) |
WO (1) | WO2006021721A1 (zh) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102026870A (zh) * | 2008-05-14 | 2011-04-20 | 空中客车运作股份公司 | 包括位于箱体的内部空间外且用于固定翼梁和面板的固定装置的发动机的悬挂架 |
CN112709613A (zh) * | 2020-12-30 | 2021-04-27 | 中国航发沈阳发动机研究所 | 一种航空发动机侧向辅助安装节结构 |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2891243B1 (fr) * | 2005-09-26 | 2009-04-03 | Airbus France Sas | Mat d'accrochage de moteur pour aeronef |
FR2891252B1 (fr) * | 2005-09-28 | 2007-10-26 | Airbus France Sas | Mat a ossature monolithique |
FR2891803B1 (fr) * | 2005-10-07 | 2007-11-30 | Airbus France Sas | Structure rigide pour mat d'accrochage de moteur d'aeronef, et mat comportant une telle structure |
GB2434836B (en) * | 2006-02-04 | 2008-12-10 | Rolls Royce Plc | Mounting system for use in mounting a gas turbine engine |
FI118761B (fi) * | 2006-02-09 | 2008-03-14 | Patria Aerostructures Oy | Ilma-aluksen siipi, kiinnitysjärjestely sekä välituki |
FR2901243B1 (fr) * | 2006-05-16 | 2008-06-27 | Airbus France Sas | Dispositif d'accrochage d'un moteur d'aeronef |
US7770841B2 (en) * | 2006-12-22 | 2010-08-10 | Calvin Burgess | Inverted airfoil pylon for an aircraft |
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. |
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. |
FR2929245B1 (fr) * | 2008-03-28 | 2010-05-14 | Aircelle Sa | Structure primaire d'un mat d'accrochage. |
FR3029504B1 (fr) * | 2014-12-09 | 2018-03-30 | Airbus Operations (S.A.S.) | Attache moteur avant d'aeronef |
FR3040076B1 (fr) * | 2015-08-13 | 2017-08-11 | Airbus Operations Sas | 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 |
FR3040369B1 (fr) * | 2015-09-02 | 2018-07-13 | Airbus Operations Sas | Ensemble moteur d'aeronef comprenant une attache moteur avant amelioree |
FR3061480B1 (fr) * | 2016-12-30 | 2019-05-31 | Airbus Operations | Ensemble moteur pour aeronef comprenant une attache moteur avant facilitant son montage |
FR3075174B1 (fr) * | 2017-12-18 | 2020-12-11 | Safran Aircraft Engines | Structure porteuse destinee au montage sur un generateur de gaz |
FR3076282B1 (fr) * | 2017-12-29 | 2020-02-07 | Airbus Operations | Ensemble pour aeronef comprenant une structure primaire de mat d'accrochage fixee a un caisson de voilure par des attaches presentant un encombrement reduit dans la zone de bord d'attaque |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1516980A (en) * | 1974-12-24 | 1978-07-05 | Rolls Royce | Mounting ducted fan gas turbine engines on aircraft |
US4634081A (en) * | 1983-12-30 | 1987-01-06 | The Boeing Company | Aft engine mount with vibration isolators |
EP0431800B1 (en) * | 1989-12-05 | 1994-08-31 | ROLLS-ROYCE plc | Failure tolerant engine mounting |
FR2676707B1 (fr) * | 1991-05-23 | 1993-08-13 | Snecma | Nacelle pour suspendre sous l'aile d'un avion un groupe turboreacteur du type a double flux. |
FR2680353B1 (fr) * | 1991-08-14 | 1993-10-15 | Snecma | Structure d'accrochage arriere d'un turboreacteur. |
US5320307A (en) * | 1992-03-25 | 1994-06-14 | General Electric Company | Aircraft engine thrust mount |
DE69415696T2 (de) * | 1994-10-18 | 1999-07-29 | United Technologies Corp | Gondel und ihre halterungsvorrichtung auf einem flugzeug |
US5725181A (en) * | 1996-05-01 | 1998-03-10 | The Boeing Company | Aircraft engine thrust mount |
US5921500A (en) * | 1997-10-08 | 1999-07-13 | General Electric Company | Integrated failsafe engine mount |
FR2770486B1 (fr) * | 1997-11-06 | 2000-01-28 | Aerospatiale | Dispositif d'accrochage d'un moteur sur un aeronef |
US6189830B1 (en) * | 1999-02-26 | 2001-02-20 | The Boeing Company | Tuned engine mounting system for jet aircraft |
FR2793767B1 (fr) * | 1999-05-17 | 2001-09-21 | Aerospatiale Airbus | Dispositif d'accrochage d'un moteur d'aeronef |
FR2793768B1 (fr) * | 1999-05-17 | 2001-09-07 | Aerospatiale Airbus | Dispositif de montage sur un mat d'un ensemble propulsif d'aeronef et mat adapte a ce dispositif |
FR2793769B1 (fr) * | 1999-05-19 | 2001-09-07 | Aerospatiale Airbus | Dispositif d'accrochage d'un moteur d'aeronef a un mat |
-
2004
- 2004-08-04 FR FR0451784A patent/FR2873985B1/fr not_active Expired - Fee Related
-
2005
- 2005-08-01 CA CA2576518A patent/CA2576518C/en not_active Expired - Fee Related
- 2005-08-01 DE DE602005011633T patent/DE602005011633D1/de active Active
- 2005-08-01 US US11/571,666 patent/US7624945B2/en not_active Expired - Fee Related
- 2005-08-01 EP EP05797577A patent/EP1773660B1/fr not_active Not-in-force
- 2005-08-01 JP JP2007524380A patent/JP4676982B2/ja not_active Expired - Fee Related
- 2005-08-01 WO PCT/FR2005/050637 patent/WO2006021721A1/fr active Application Filing
- 2005-08-01 CN CN2005800263171A patent/CN1993268B/zh not_active Expired - Fee Related
- 2005-08-01 BR BRPI0513867-1A patent/BRPI0513867A/pt not_active IP Right Cessation
- 2005-08-01 RU RU2007107929/11A patent/RU2381149C2/ru not_active IP Right Cessation
- 2005-08-01 AT AT05797577T patent/ATE416975T1/de not_active IP Right Cessation
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102026870A (zh) * | 2008-05-14 | 2011-04-20 | 空中客车运作股份公司 | 包括位于箱体的内部空间外且用于固定翼梁和面板的固定装置的发动机的悬挂架 |
CN112709613A (zh) * | 2020-12-30 | 2021-04-27 | 中国航发沈阳发动机研究所 | 一种航空发动机侧向辅助安装节结构 |
Also Published As
Publication number | Publication date |
---|---|
JP4676982B2 (ja) | 2011-04-27 |
US7624945B2 (en) | 2009-12-01 |
JP2008509318A (ja) | 2008-03-27 |
DE602005011633D1 (de) | 2009-01-22 |
FR2873985A1 (fr) | 2006-02-10 |
WO2006021721A1 (fr) | 2006-03-02 |
EP1773660B1 (fr) | 2008-12-10 |
EP1773660A1 (fr) | 2007-04-18 |
US20070228213A1 (en) | 2007-10-04 |
FR2873985B1 (fr) | 2006-11-24 |
RU2381149C2 (ru) | 2010-02-10 |
CA2576518C (en) | 2014-02-25 |
RU2007107929A (ru) | 2008-09-10 |
CA2576518A1 (en) | 2006-03-02 |
CN1993268B (zh) | 2011-06-15 |
BRPI0513867A (pt) | 2008-05-20 |
ATE416975T1 (de) | 2008-12-15 |
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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 |
|
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20110615 Termination date: 20200801 |
|
CF01 | Termination of patent right due to non-payment of annual fee |