ATE500132T1 - Befestigungsvorrichtung für flugzeugtriebwerk und mindestens eine solche vorrichtung enthaltendes flugzeug - Google Patents
Befestigungsvorrichtung für flugzeugtriebwerk und mindestens eine solche vorrichtung enthaltendes flugzeugInfo
- Publication number
- ATE500132T1 ATE500132T1 AT08736388T AT08736388T ATE500132T1 AT E500132 T1 ATE500132 T1 AT E500132T1 AT 08736388 T AT08736388 T AT 08736388T AT 08736388 T AT08736388 T AT 08736388T AT E500132 T1 ATE500132 T1 AT E500132T1
- Authority
- AT
- Austria
- Prior art keywords
- rigid structure
- engine
- aircraft
- mechanically connected
- balance beam
- Prior art date
Links
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
- B64D27/406—Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links
-
- 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
- B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Clamps And Clips (AREA)
- Connection Of Plates (AREA)
- Handcart (AREA)
- Transmission Devices (AREA)
- Load-Engaging Elements For Cranes (AREA)
- Mutual Connection Of Rods And Tubes (AREA)
- Pivots And Pivotal Connections (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0754618A FR2915177B1 (fr) | 2007-04-20 | 2007-04-20 | Dispositif d'accrochage de moteur d'aeronef et aeronef comportant au moins un tel dispositif |
| PCT/EP2008/054743 WO2008135366A1 (fr) | 2007-04-20 | 2008-04-18 | Dispositif d'accrochage de moteur d'aeronef et aeronef comportant au moins un tel dispositif |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE500132T1 true ATE500132T1 (de) | 2011-03-15 |
Family
ID=38657658
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT08736388T ATE500132T1 (de) | 2007-04-20 | 2008-04-18 | Befestigungsvorrichtung für flugzeugtriebwerk und mindestens eine solche vorrichtung enthaltendes flugzeug |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US8146856B2 (de) |
| EP (1) | EP2142430B1 (de) |
| AT (1) | ATE500132T1 (de) |
| DE (1) | DE602008005290D1 (de) |
| FR (1) | FR2915177B1 (de) |
| WO (1) | WO2008135366A1 (de) |
Families Citing this family (27)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2915175B1 (fr) * | 2007-04-20 | 2009-07-17 | Airbus France Sa | Mat d'accrochage de moteur pour aeronef disposant d'une poutre d'attache moteur arriere deportee du caisson |
| FR2917713B1 (fr) * | 2007-06-21 | 2009-09-25 | Airbus France Sas | Dispositif d'accrochage de moteur d'aeronef et aeronef comportant au moins un tel dispositif. |
| GB0810585D0 (en) * | 2008-06-11 | 2008-07-16 | Rolls Royce Plc | Engine mounting arrangement |
| GB0810791D0 (en) * | 2008-06-13 | 2008-07-23 | Rolls Royce Plc | Thrust mounting arrangement |
| GB0902909D0 (en) * | 2009-02-23 | 2009-04-08 | Rolls Royce Plc | A thrust mount arrangement for an aircraft engine |
| FR2954277B1 (fr) * | 2009-12-17 | 2012-03-23 | Snecma | Suspension d'un turboreacteur a un aeronef |
| FR2958267B1 (fr) | 2010-04-02 | 2012-03-23 | Airbus Operations Sas | Systeme d'axe pour ensemble de liaison d'un mat-reacteur sous une voilure d'aeronef |
| FR2959210B1 (fr) * | 2010-04-21 | 2013-08-23 | Snecma | Palonnier de suspension de turboreacteur d'aeronef et suspension avec accroche-soufflante ainsi equipee |
| US8727269B2 (en) * | 2011-06-06 | 2014-05-20 | General Electric Company | System and method for mounting an aircraft engine |
| US8567745B2 (en) * | 2011-12-15 | 2013-10-29 | United Technologies Corporation | Apparatuses and systems with vertically and longitudinally offset mounting flanges |
| FR2987401B1 (fr) * | 2012-02-28 | 2017-05-12 | Snecma | Procede pour maintenir une piece d'adaptation sur un carter tubulaire d'un turbomoteur, piece d'adaptation et systeme de maintien correspondants. |
| US8985509B2 (en) * | 2012-08-31 | 2015-03-24 | United Technologies Corporation | Assembly for mounting a turbine engine to a pylon |
| CN105392700B (zh) | 2013-07-26 | 2018-12-18 | Mra系统有限责任公司 | 飞行器发动机吊架 |
| 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 |
| US10351224B2 (en) * | 2015-09-23 | 2019-07-16 | The Boeing Company | External structure mounting system for use with an aircraft |
| FR3049264B1 (fr) * | 2016-03-25 | 2019-07-05 | Airbus Operations | Systeme de montage pour un aeronef, destine a la fixation d’un moteur sur un mat d’attache. |
| SG10202106080XA (en) | 2017-10-12 | 2021-07-29 | Fraunhofer Ges Forschung | Optimizing audio delivery for virtual reality applications |
| USD880279S1 (en) * | 2017-12-11 | 2020-04-07 | Marchesan Implementos E Maquinas Agricolas Tatu S.A. | Support bracket |
| FR3079212B1 (fr) * | 2018-03-26 | 2020-09-11 | Airbus Operations Sas | Ensemble de motorisation pour un aeronef |
| GB201808978D0 (en) * | 2018-06-01 | 2018-07-18 | Airbus Operations Ltd | Barrel nut |
| GB2579048A (en) * | 2018-11-16 | 2020-06-10 | Airbus Operations Ltd | Fittings for connecting structures |
| US11479104B2 (en) | 2019-07-24 | 2022-10-25 | Honeywell International Inc. | System and method for gas turbine engine mount with seal |
| FR3100530B1 (fr) | 2019-09-11 | 2021-07-30 | Airbus Operations Sas | Ensemble de motorisation d’aéronef comprenant un dispositif de reprise d’efforts de poussée |
| FR3127202A1 (fr) * | 2021-09-20 | 2023-03-24 | Airbus Operations (S.A.S.) | Ensemble de motorisation d’aéronef comprenant un dispositif de reprise d’efforts de poussée |
| FR3140068A1 (fr) * | 2022-09-23 | 2024-03-29 | Airbus Operations | Ensemble de motorisation d’aéronef comportant un dispositif de reprise d’efforts de poussée |
| CN116447015B (zh) * | 2023-04-10 | 2025-09-23 | 北京航空航天大学 | 一种基于金属橡胶的发动机安装节结构系统 |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3844115A (en) * | 1973-02-14 | 1974-10-29 | Gen Electric | Load distributing thrust mount |
| GB1521847A (en) * | 1976-04-30 | 1978-08-16 | Rolls Royce | Attachment for attaching jet propulsion engines to vehicle structure |
| GB2010969A (en) * | 1977-12-22 | 1979-07-04 | Rolls Royce | Mounting for Gas Turbine Jet Propulsion Engine |
| US5320307A (en) * | 1992-03-25 | 1994-06-14 | General Electric Company | Aircraft engine thrust mount |
| FR2755944B1 (fr) * | 1996-11-21 | 1998-12-24 | Snecma | Suspension avant redondante pour turbomachine |
| FR2755942B1 (fr) * | 1996-11-21 | 1998-12-24 | Snecma | Suspension avant redondante pour turbomachine |
| US6296203B1 (en) * | 2000-05-24 | 2001-10-02 | General Electric Company | Snubber thrust mount |
| DE10249517B4 (de) * | 2002-10-23 | 2008-11-20 | Eurocopter Deutschland Gmbh | Stoßabsorbierende, lastbegrenzende Verbindungsvorrichtung sowie Drehflügelflugzeug mit einer solchen Verbindungsvorrichtung |
| US7083143B2 (en) * | 2003-10-17 | 2006-08-01 | The Boeing Company | Apparatuses and methods for attaching engines and other structures to aircraft wings |
| FR2903383B1 (fr) | 2006-07-10 | 2009-05-15 | Airbus France Sas | Dispositif d'accrochage d'un moteur d'aeronef comportant deux bielles de reprise de poussee a double liaison mecanique arriere |
-
2007
- 2007-04-20 FR FR0754618A patent/FR2915177B1/fr not_active Expired - Fee Related
-
2008
- 2008-04-18 DE DE602008005290T patent/DE602008005290D1/de active Active
- 2008-04-18 US US12/596,555 patent/US8146856B2/en active Active
- 2008-04-18 EP EP08736388A patent/EP2142430B1/de not_active Ceased
- 2008-04-18 WO PCT/EP2008/054743 patent/WO2008135366A1/fr not_active Ceased
- 2008-04-18 AT AT08736388T patent/ATE500132T1/de not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| EP2142430B1 (de) | 2011-03-02 |
| FR2915177B1 (fr) | 2009-07-10 |
| US8146856B2 (en) | 2012-04-03 |
| US20100127118A1 (en) | 2010-05-27 |
| WO2008135366A1 (fr) | 2008-11-13 |
| DE602008005290D1 (de) | 2011-04-14 |
| EP2142430A1 (de) | 2010-01-13 |
| FR2915177A1 (fr) | 2008-10-24 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |