ATE490916T1 - Motormontagestruktur mit einstückigem rahmen - Google Patents
Motormontagestruktur mit einstückigem rahmenInfo
- Publication number
- ATE490916T1 ATE490916T1 AT06793826T AT06793826T ATE490916T1 AT E490916 T1 ATE490916 T1 AT E490916T1 AT 06793826 T AT06793826 T AT 06793826T AT 06793826 T AT06793826 T AT 06793826T AT E490916 T1 ATE490916 T1 AT E490916T1
- Authority
- AT
- Austria
- Prior art keywords
- mounting structure
- framework
- engine mounting
- piece frame
- fittings
- Prior art date
Links
- 238000003723 Smelting Methods 0.000 abstract 1
- 239000002131 composite material Substances 0.000 abstract 1
- 238000004519 manufacturing process Methods 0.000 abstract 1
- 230000002787 reinforcement Effects 0.000 abstract 1
- 238000003466 welding Methods 0.000 abstract 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
- B64D27/40—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
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49616—Structural member making
- Y10T29/49622—Vehicular structural member making
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Connection Of Plates (AREA)
- Body Structure For Vehicles (AREA)
- Standing Axle, Rod, Or Tube Structures Coupled By Welding, Adhesion, Or Deposition (AREA)
- Butt Welding And Welding Of Specific Article (AREA)
- Vehicle Body Suspensions (AREA)
- Automatic Cycles, And Cycles In General (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Passenger Equipment (AREA)
- Wire Processing (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0552934A FR2891252B1 (fr) | 2005-09-28 | 2005-09-28 | Mat a ossature monolithique |
PCT/EP2006/066731 WO2007036516A1 (fr) | 2005-09-28 | 2006-09-26 | Mât à ossature monolithique |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE490916T1 true ATE490916T1 (de) | 2010-12-15 |
Family
ID=36425256
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT06793826T ATE490916T1 (de) | 2005-09-28 | 2006-09-26 | Motormontagestruktur mit einstückigem rahmen |
Country Status (11)
Country | Link |
---|---|
US (1) | US20080217502A1 (de) |
EP (1) | EP1928741B1 (de) |
JP (1) | JP2009509842A (de) |
CN (1) | CN101272954B (de) |
AT (1) | ATE490916T1 (de) |
BR (1) | BRPI0616143A2 (de) |
CA (1) | CA2624000A1 (de) |
DE (1) | DE602006018755D1 (de) |
FR (1) | FR2891252B1 (de) |
RU (1) | RU2418720C2 (de) |
WO (1) | WO2007036516A1 (de) |
Families Citing this family (41)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20070251751A1 (en) * | 2006-05-01 | 2007-11-01 | Textron Inc. | Cast Aluminum Frame Component for Golf Cars and Small Utility Vehicles |
US8205825B2 (en) * | 2008-02-27 | 2012-06-26 | Spirit Aerosystems, Inc. | Engine pylon made from composite material |
FR2929245B1 (fr) * | 2008-03-28 | 2010-05-14 | Aircelle Sa | Structure primaire d'un mat d'accrochage. |
FR2931133B1 (fr) * | 2008-05-14 | 2010-06-18 | Airbus France | Mat d'accrochage de moteur comprenant des moyens de fixation des longerons et des panneaux agences en dehors de l'espace interieur de caisson |
ES2363952B1 (es) * | 2008-10-30 | 2012-07-04 | Airbus Operations, S.L. | Sistema de integración de semipartes de superficies sustentadoras en aeronaves. |
US8342444B2 (en) * | 2008-12-16 | 2013-01-01 | The Boeing Company | Fail safe extended torque box strut-to-wing mount |
FR2954278B1 (fr) * | 2009-12-18 | 2012-01-20 | Aircelle 7303 | Structure support pour inverseur de poussee notamment a grilles |
FR2960522B1 (fr) * | 2010-05-27 | 2012-06-29 | Airbus Operations Sas | Procede de fabrication par formage superplastique et par eclissage d'une nervure pour carenage aerodynamique de mat d'accrochage de moteur d'aeronef |
US9027875B2 (en) * | 2010-10-28 | 2015-05-12 | Spirit Aerosystems, Inc. | Pylon arrangement for open structure |
CN102407936A (zh) * | 2011-09-06 | 2012-04-11 | 苏氏工业科学技术(北京)有限公司 | 整体龙骨与蒙皮复合型的自走式装备舱体结构 |
US20140151497A1 (en) * | 2012-12-04 | 2014-06-05 | Ge Aviation Systems Llc | Engine pylon for an aircraft |
CN103057692A (zh) * | 2012-12-19 | 2013-04-24 | 江西洪都航空工业集团有限责任公司 | 一种飞机挂梁 |
US10708319B2 (en) | 2012-12-31 | 2020-07-07 | Dish Technologies Llc | Methods and apparatus for providing social viewing of media content |
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 |
JP6137846B2 (ja) * | 2013-01-25 | 2017-05-31 | 三菱航空機株式会社 | パイロンと翼を連結するリンク部材、航空機のパイロンおよび航空機 |
US9248921B2 (en) * | 2013-07-11 | 2016-02-02 | Spirit Aerosystems, Inc. | Method for mounting a pylon to an aircraft |
WO2015010315A1 (en) | 2013-07-26 | 2015-01-29 | Mra Systems, Inc. | Aircraft engine pylon |
FR3013678B1 (fr) * | 2013-11-25 | 2015-11-20 | Airbus Operations Sas | Carenage aerodynamique |
FR3014840B1 (fr) | 2013-12-17 | 2017-10-13 | Airbus Operations Sas | Ensemble pour aeronef comprenant un corps d'attache moteur equipe d'au moins une ferrure de support de manille penetrant dans le caisson du mat d'accrochage |
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 |
FR3015431B1 (fr) | 2013-12-19 | 2017-12-15 | Airbus Operations Sas | Structure primaire de mat d'accrochage renforcee. |
FR3015433B1 (fr) | 2013-12-23 | 2016-02-12 | Airbus Operations Sas | Ensemble pour aeronef comprenant un mat d'accrochage integre a la nacelle et agence en partie arriere du fuselage |
US9238511B2 (en) * | 2014-03-04 | 2016-01-19 | Mra Systems, Inc. | Engine pylon structure |
FR3032180B1 (fr) * | 2015-01-30 | 2018-05-18 | Airbus Operations | Ensemble propulsif comportant un turboreacteur et un mat d'accrochage permettant une nouvelle distribution des efforts entre le turboreacteur et la voilure |
FR3040043B1 (fr) * | 2015-08-12 | 2019-04-12 | Sogeclair Sa | Mat de moteur d'aeronef a ossature multifonctionnelle integree |
FR3042475B1 (fr) * | 2015-10-16 | 2018-07-13 | Airbus Operations (S.A.S.) | Mat porteur de moteur d'aeronef |
US9896217B2 (en) * | 2016-01-07 | 2018-02-20 | The Boeing Company | Enhanced performance jet engine mounting struts |
FR3052745B1 (fr) | 2016-06-15 | 2018-05-25 | Airbus Operations | Mat d'aeronef comprenant au moins un cadre lateral en forme de treillis et aeronef comprenant ledit mat |
FR3059648B1 (fr) * | 2016-12-06 | 2019-05-17 | Airbus Operations | Procede de fabrication d'un element d'aeronef et element d'aeronef mettant en oeuvre une impression tridimensionnelle |
FR3061149B1 (fr) * | 2016-12-27 | 2023-11-03 | Airbus Operations Sas | Structure primaire d'un mat pour groupe propulseur d'aeronef comportant une partie pyramidale a montants convergents |
FR3072945B1 (fr) * | 2017-10-27 | 2020-11-20 | Airbus Operations Sas | Structure primaire de mat de support d'un groupe propulseur d'aeronef comportant une partie inferieure en u obtenue de maniere monobloc ou par soudage |
FR3072946A1 (fr) * | 2017-10-27 | 2019-05-03 | Airbus Operations | Structure primaire de mat de support d'un groupe propulseur d'aeronef en caisson formee par assemblage de deux demi-coquilles |
FR3076283B1 (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 |
CN109606703A (zh) * | 2019-01-16 | 2019-04-12 | 中国商用飞机有限责任公司 | 飞机静定吊挂系统 |
CN109733623A (zh) * | 2019-01-28 | 2019-05-10 | 河南正大航空工业股份有限公司 | 一种用于无人机的发动机支撑结构 |
FR3092821A1 (fr) * | 2019-02-18 | 2020-08-21 | Airbus Operations | Ensemble pour aeronef comprenant un mat d’accrochage, une aile et deux systemes de fixation fixant le mat d’accrochage a l’aile |
CN109795699A (zh) * | 2019-03-15 | 2019-05-24 | 中国商用飞机有限责任公司 | 飞机吊挂接头组件 |
FR3099464B1 (fr) | 2019-07-31 | 2024-06-21 | Airbus Operations Sas | Mat reacteur pour coupler un turboreacteur a une aile d’un aeronef |
FR3102151B1 (fr) * | 2019-10-21 | 2021-10-29 | Airbus Operations Sas | Aéronef comprenant une attache voilure arrière présentant au moins deux bielles latérales et un pion de cisaillement |
FR3102741B1 (fr) * | 2019-10-30 | 2022-05-06 | Airbus Operations Sas | Mât d’accrochage comportant une structure primaire formée d’au moins un longeron et un panneau assemblés par soudure et procédé de soudure. |
FR3114801A1 (fr) * | 2020-10-02 | 2022-04-08 | Airbus Operations | Assemblage d’un mat avec une aile d’un aeronef |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4437627A (en) * | 1982-03-12 | 1984-03-20 | The Boeing Company | Integrated power plant installation system |
FR2698068B1 (fr) * | 1992-11-16 | 1995-02-03 | Airbus Ind | Avion et autre aéronef à moteur pourvu d'ailes. |
US5484120A (en) * | 1994-03-11 | 1996-01-16 | Sundstrand Corporation | Support strut for ram air driven turbine |
US6126110A (en) * | 1997-12-22 | 2000-10-03 | Mcdonnell Douglas Corporation | Horizontally opposed trunnion forward engine mount system supported beneath a wing pylon |
US7083143B2 (en) * | 2003-10-17 | 2006-08-01 | The Boeing Company | Apparatuses and methods for attaching engines and other structures to aircraft wings |
FR2862945B1 (fr) * | 2003-12-01 | 2006-04-28 | Airbus France | Dispositif d'accrochage d'un turbopropulseur sous une voilure d'aeronef. |
FR2862944B1 (fr) * | 2003-12-01 | 2006-02-24 | Airbus France | Dispositif d'accrochage d'un turbopropulseur sous une voilure d'aeronef |
US7104306B2 (en) * | 2004-06-14 | 2006-09-12 | The Boeing Company | Cast unitized primary truss structure and method |
FR2873985B1 (fr) * | 2004-08-04 | 2006-11-24 | Airbus France Sas | Ensemble moteur pour aeronef |
FR2891244B1 (fr) * | 2005-09-26 | 2009-04-03 | Airbus France Sas | Mat d'accrochage de moteur pour aeronef |
FR2891251B1 (fr) * | 2005-09-28 | 2009-04-03 | Airbus France Sas | Mat d'accrochage de moteur pour aeronef |
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 |
US8469309B2 (en) * | 2008-12-24 | 2013-06-25 | General Electric Company | Monolithic structure for mounting aircraft engine |
-
2005
- 2005-09-28 FR FR0552934A patent/FR2891252B1/fr not_active Expired - Fee Related
-
2006
- 2006-09-26 BR BRPI0616143-0A patent/BRPI0616143A2/pt not_active IP Right Cessation
- 2006-09-26 JP JP2008532761A patent/JP2009509842A/ja active Pending
- 2006-09-26 US US12/066,916 patent/US20080217502A1/en not_active Abandoned
- 2006-09-26 AT AT06793826T patent/ATE490916T1/de not_active IP Right Cessation
- 2006-09-26 DE DE602006018755T patent/DE602006018755D1/de active Active
- 2006-09-26 CN CN2006800358778A patent/CN101272954B/zh not_active Expired - Fee Related
- 2006-09-26 RU RU2008116568/11A patent/RU2418720C2/ru not_active IP Right Cessation
- 2006-09-26 EP EP06793826A patent/EP1928741B1/de not_active Ceased
- 2006-09-26 WO PCT/EP2006/066731 patent/WO2007036516A1/fr active Application Filing
- 2006-09-26 CA CA002624000A patent/CA2624000A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
CA2624000A1 (en) | 2007-04-05 |
CN101272954A (zh) | 2008-09-24 |
JP2009509842A (ja) | 2009-03-12 |
FR2891252A1 (fr) | 2007-03-30 |
FR2891252B1 (fr) | 2007-10-26 |
CN101272954B (zh) | 2011-02-23 |
RU2418720C2 (ru) | 2011-05-20 |
WO2007036516A1 (fr) | 2007-04-05 |
EP1928741A1 (de) | 2008-06-11 |
DE602006018755D1 (de) | 2011-01-20 |
RU2008116568A (ru) | 2010-01-20 |
BRPI0616143A2 (pt) | 2011-06-07 |
EP1928741B1 (de) | 2010-12-08 |
US20080217502A1 (en) | 2008-09-11 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |