BRPI0908987A2 - estrutura de fixação de um motor turbojato, sistema de fixação para um motor turbojato, sistema de propulsão - Google Patents
estrutura de fixação de um motor turbojato, sistema de fixação para um motor turbojato, sistema de propulsãoInfo
- Publication number
- BRPI0908987A2 BRPI0908987A2 BRPI0908987-0A BRPI0908987A BRPI0908987A2 BR PI0908987 A2 BRPI0908987 A2 BR PI0908987A2 BR PI0908987 A BRPI0908987 A BR PI0908987A BR PI0908987 A2 BRPI0908987 A2 BR PI0908987A2
- Authority
- BR
- Brazil
- Prior art keywords
- turbojet engine
- engine mounting
- mounting frame
- propulsion system
- propulsion
- 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
- B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0801264A FR2928347B1 (fr) | 2008-03-07 | 2008-03-07 | Structure d'accrochage pour turboreacteur |
| FR0801264 | 2008-03-07 | ||
| PCT/FR2009/000022 WO2009112669A1 (fr) | 2008-03-07 | 2009-01-09 | Structure d'accrochage pour turboréacteur |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BRPI0908987A2 true BRPI0908987A2 (pt) | 2019-09-24 |
Family
ID=39832580
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BRPI0908987-0A BRPI0908987A2 (pt) | 2008-03-07 | 2009-01-09 | estrutura de fixação de um motor turbojato, sistema de fixação para um motor turbojato, sistema de propulsão |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US20110308257A1 (pt) |
| EP (1) | EP2247503B1 (pt) |
| CN (1) | CN101959757A (pt) |
| BR (1) | BRPI0908987A2 (pt) |
| CA (1) | CA2716742A1 (pt) |
| ES (1) | ES2527303T3 (pt) |
| FR (1) | FR2928347B1 (pt) |
| RU (1) | RU2492117C2 (pt) |
| WO (1) | WO2009112669A1 (pt) |
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN102849218A (zh) * | 2012-09-04 | 2013-01-02 | 西安飞机工业(集团)有限责任公司 | 一种飞机辅助动力装置安装梁 |
| FR2994942B1 (fr) * | 2012-09-06 | 2015-08-07 | Airbus Operations Sas | Ensemble propulsif lateral pour aeronef comprenant un arceau de support d'un turbomoteur. |
| FR3095417B1 (fr) | 2019-04-26 | 2021-09-24 | Safran Nacelles | Entrée d’air de nacelle et nacelle comportant une telle entrée d’air |
| FR3096352B1 (fr) * | 2019-05-24 | 2021-06-11 | Airbus Operations Sas | Ensemble de motorisation pour un aeronef comprenant un support de charge |
| US11697506B2 (en) * | 2020-05-15 | 2023-07-11 | General Electric Company | Methods and apparatus for gas turbine bending isolation |
Family Cites Families (21)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3201069A (en) * | 1962-05-31 | 1965-08-17 | Haskin Simon | Jet-propelled aircraft engine mounting |
| US3561707A (en) * | 1969-06-24 | 1971-02-09 | United Aircraft Corp | Thrust mount |
| 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 |
| DE2544272C3 (de) * | 1975-10-03 | 1979-02-22 | Avions Marcel Dassault-Breguet Aviation S.A., Vaucresson (Frankreich) | Triebwerksaufhängung an Luftfahrzeugen |
| US4044973A (en) * | 1975-12-29 | 1977-08-30 | The Boeing Company | Nacelle assembly and mounting structures for a turbofan jet propulsion engine |
| GB9116986D0 (en) * | 1991-08-07 | 1991-10-09 | Rolls Royce Plc | Gas turbine engine nacelle assembly |
| US5524847A (en) * | 1993-09-07 | 1996-06-11 | United Technologies Corporation | Nacelle and mounting arrangement for an aircraft engine |
| CN1212324A (zh) * | 1997-09-19 | 1999-03-31 | 何海江 | 组合式喷气发动机 |
| FR2775465B1 (fr) * | 1998-03-02 | 2000-05-26 | Aerospatiale | Dispositif d'accrochage d'un moteur sur un pylone 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 |
| FR2799432A1 (fr) * | 1999-10-07 | 2001-04-13 | Snecma | Suspension a securite integree pour groupes motopropulseurs d'aeronefs |
| FR2867157B1 (fr) * | 2004-03-04 | 2006-06-02 | Airbus France | Systeme de montage interpose entre un moteur d'aeronef et une structure rigide d'un mat d'accrochage fixe sous une voilure de cet aeronef. |
| FR2885877B1 (fr) * | 2005-05-23 | 2008-12-12 | Airbus France Sas | Mat d'accrochage de turboreacteur pour aeronef |
| FR2885878B1 (fr) * | 2005-05-23 | 2007-06-29 | Airbus France Sas | Ensemble moteur pour aeronef |
| FR2887521B1 (fr) * | 2005-06-28 | 2007-08-17 | Airbus France Sas | Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un dispositif d'accrochage d'un tel moteur |
| FR2891245B1 (fr) * | 2005-09-26 | 2007-10-26 | Airbus France Sas | Procede de montage d'un moteur d'aeronef sur une structure rigide d'un mat d'accrochage du moteur |
| FR2891254B1 (fr) * | 2005-09-29 | 2007-10-26 | Airbus France Sas | Ensemble moteur pour aeronef |
| FR2891526B1 (fr) * | 2005-10-03 | 2007-11-02 | Airbus France Sas | Mat d'accrochage de turboreacteur pour aeronef |
| FR2965796B1 (fr) * | 2010-10-07 | 2013-06-07 | Snecma | Suspension d'un moteur a un mat d'aeronef comportant un arceau de suspension |
| US20130233997A1 (en) * | 2012-03-12 | 2013-09-12 | United Technologies Corporation | Turbine engine case mount |
-
2008
- 2008-03-07 FR FR0801264A patent/FR2928347B1/fr not_active Expired - Fee Related
-
2009
- 2009-01-09 CA CA2716742A patent/CA2716742A1/fr not_active Abandoned
- 2009-01-09 CN CN2009801077544A patent/CN101959757A/zh active Pending
- 2009-01-09 EP EP09720401.0A patent/EP2247503B1/fr not_active Not-in-force
- 2009-01-09 US US12/921,239 patent/US20110308257A1/en not_active Abandoned
- 2009-01-09 RU RU2010140703/11A patent/RU2492117C2/ru not_active IP Right Cessation
- 2009-01-09 ES ES09720401.0T patent/ES2527303T3/es active Active
- 2009-01-09 BR BRPI0908987-0A patent/BRPI0908987A2/pt not_active IP Right Cessation
- 2009-01-09 WO PCT/FR2009/000022 patent/WO2009112669A1/fr not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| WO2009112669A1 (fr) | 2009-09-17 |
| US20110308257A1 (en) | 2011-12-22 |
| EP2247503A1 (fr) | 2010-11-10 |
| ES2527303T3 (es) | 2015-01-22 |
| EP2247503B1 (fr) | 2014-10-15 |
| FR2928347B1 (fr) | 2010-06-25 |
| RU2010140703A (ru) | 2012-04-20 |
| RU2492117C2 (ru) | 2013-09-10 |
| FR2928347A1 (fr) | 2009-09-11 |
| CN101959757A (zh) | 2011-01-26 |
| CA2716742A1 (fr) | 2009-09-17 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] | ||
| B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] |
Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2543 DE 01-10-2019 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013. |