BRPI0917701A2 - nacela de motor turbojato - Google Patents
nacela de motor turbojatoInfo
- Publication number
- BRPI0917701A2 BRPI0917701A2 BRPI0917701A BRPI0917701A BRPI0917701A2 BR PI0917701 A2 BRPI0917701 A2 BR PI0917701A2 BR PI0917701 A BRPI0917701 A BR PI0917701A BR PI0917701 A BRPI0917701 A BR PI0917701A BR PI0917701 A2 BRPI0917701 A2 BR PI0917701A2
- Authority
- BR
- Brazil
- Prior art keywords
- turbojet engine
- engine nacelle
- nacelle
- turbojet
- engine
- 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
- B64D29/00—Power-plant nacelles, fairings or cowlings
- B64D29/08—Inspection panels for power plants
-
- 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
- B64D29/00—Power-plant nacelles, fairings or cowlings
- B64D29/06—Attaching of nacelles, fairings or cowlings
-
- 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
- B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
-
- 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
- B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0266—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
- B64D2033/0286—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for turbofan engines
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Wind Motors (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0805421A FR2936492B1 (fr) | 2008-10-01 | 2008-10-01 | Nacelle pour turboreacteur. |
| PCT/FR2009/001141 WO2010037923A1 (fr) | 2008-10-01 | 2009-09-25 | Nacelle pour turboreacteur |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BRPI0917701A2 true BRPI0917701A2 (pt) | 2016-02-10 |
Family
ID=40637017
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BRPI0917701A BRPI0917701A2 (pt) | 2008-10-01 | 2009-09-25 | nacela de motor turbojato |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US8753072B2 (pt) |
| EP (1) | EP2328808B1 (pt) |
| CN (1) | CN102164820B (pt) |
| BR (1) | BRPI0917701A2 (pt) |
| CA (1) | CA2735530A1 (pt) |
| ES (1) | ES2431000T3 (pt) |
| FR (1) | FR2936492B1 (pt) |
| RU (1) | RU2509688C2 (pt) |
| WO (1) | WO2010037923A1 (pt) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20180208297A1 (en) * | 2017-01-20 | 2018-07-26 | General Electric Company | Nacelle for an aircraft aft fan |
| FR3075761A1 (fr) * | 2017-12-21 | 2019-06-28 | Airbus Operations | Partie anterieure de nacelle d'un ensemble propulsif comportant un cadre de rigidification incline |
| FR3086643B1 (fr) * | 2018-09-28 | 2021-05-28 | Safran Nacelles | Nacelle pour aeronef et entree d'air associee |
| FR3094698B1 (fr) | 2019-04-02 | 2022-09-09 | Safran Aircraft Engines | Manche d’entree d’air pour une nacelle d’un ensemble propulsif d’aeronef |
| US11390393B2 (en) * | 2019-06-04 | 2022-07-19 | Rohr, Inc. | Nacelle with a translatable inlet for an aircraft propulsion system |
| CN110466782B (zh) * | 2019-07-26 | 2022-12-20 | 中国航发沈阳发动机研究所 | 一种航空发动机用弹性连接组件 |
| FR3118481B1 (fr) * | 2020-12-28 | 2023-04-21 | Safran Nacelles | Entrée d’air d’ensemble propulsif d’aéronef comprenant un organe de déplacement d’une partie amont mobile et procédé d’utilisation d’une telle entrée d’air |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1514305A (en) * | 1975-09-12 | 1978-06-14 | Rolls Royce | Ejector sleeves for aircraft mounted gas turbine engines |
| SU590914A1 (ru) * | 1976-09-21 | 2005-11-27 | А.А. Верченов | Силовая установка летательного аппарата |
| US4688757A (en) | 1986-08-11 | 1987-08-25 | Dresser Industries, Inc. | Soft seat Y pattern globe valve |
| GB9301457D0 (en) * | 1993-01-26 | 1993-03-17 | Short Brothers Plc | An aircraft propulsuve power unit |
| FR2757823B1 (fr) * | 1996-12-26 | 1999-03-12 | Aerospatiale | Nacelle de turboreacteur a ecoulement laminaire |
| US7588212B2 (en) | 2003-07-08 | 2009-09-15 | Rohr Inc. | Method and apparatus for noise abatement and ice protection of an aircraft engine nacelle inlet lip |
| FR2868124B1 (fr) * | 2004-03-29 | 2006-06-23 | Airbus France Sas | Structure d'entree d'air pour moteur d'aeronef |
| FR2890378B1 (fr) * | 2005-09-08 | 2009-01-16 | Airbus France Sas | Capot de nacelle pour turboreacteur et nacelle comportant au moins un tel capot. |
| FR2901244B1 (fr) * | 2006-05-16 | 2009-01-09 | Airbus France Sas | Dispositif d'articulation de portes d'une nacelle d'aeronef et nacelle equipee dudit dispositif d'articulation |
| FR2906568B1 (fr) * | 2006-10-02 | 2012-01-06 | Aircelle Sa | Structure d'entree d'air deposable pour nacelle de turboreacteur. |
-
2008
- 2008-10-01 FR FR0805421A patent/FR2936492B1/fr not_active Expired - Fee Related
-
2009
- 2009-09-25 CA CA2735530A patent/CA2735530A1/fr not_active Abandoned
- 2009-09-25 CN CN200980137719.7A patent/CN102164820B/zh not_active Expired - Fee Related
- 2009-09-25 EP EP09748363.0A patent/EP2328808B1/fr not_active Not-in-force
- 2009-09-25 WO PCT/FR2009/001141 patent/WO2010037923A1/fr not_active Ceased
- 2009-09-25 RU RU2011116970/11A patent/RU2509688C2/ru not_active IP Right Cessation
- 2009-09-25 ES ES09748363T patent/ES2431000T3/es active Active
- 2009-09-25 US US13/121,749 patent/US8753072B2/en not_active Expired - Fee Related
- 2009-09-25 BR BRPI0917701A patent/BRPI0917701A2/pt not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| ES2431000T3 (es) | 2013-11-22 |
| CN102164820B (zh) | 2014-01-08 |
| EP2328808A1 (fr) | 2011-06-08 |
| RU2509688C2 (ru) | 2014-03-20 |
| EP2328808B1 (fr) | 2013-07-24 |
| CA2735530A1 (fr) | 2010-04-08 |
| CN102164820A (zh) | 2011-08-24 |
| US20110182727A1 (en) | 2011-07-28 |
| RU2011116970A (ru) | 2012-11-10 |
| FR2936492B1 (fr) | 2011-04-01 |
| FR2936492A1 (fr) | 2010-04-02 |
| US8753072B2 (en) | 2014-06-17 |
| WO2010037923A1 (fr) | 2010-04-08 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| BRPI0821929A2 (pt) | Nacela para motor turbojato | |
| BRPI0910935A2 (pt) | desvio da nacela de motor turbojato e nacela | |
| BRPI0822363A2 (pt) | Nacela de motor turbojato | |
| EP2244357A4 (en) | ENGINE | |
| BRPI0821504A2 (pt) | nacela para motor de avião | |
| BRPI0915985A2 (pt) | conjunto motor transmissão | |
| BRPI0920961A2 (pt) | mecanismo de procura estrutura de emprego | |
| DK2481143T3 (da) | Motor | |
| EP2175116A4 (en) | INTERNAL COMBUSTION ENGINE | |
| BRPI0921691A2 (pt) | motor a gás | |
| EP2341226A4 (en) | MOTOR GENERATOR | |
| EP2438278A4 (en) | INTERNAL COMBUSTION ENGINE | |
| BRPI0911334A2 (pt) | lubrificantes de motor | |
| BRPI1008068A2 (pt) | nacela de motor turbojato | |
| BRPI0908079A2 (pt) | Conjunto motor para aeronave, e, aeronave | |
| BR112012002026A2 (pt) | motor com mecanismo de redução de velocidade | |
| DE602008005797D1 (de) | Motor | |
| BRPI0907771A2 (pt) | Conjunto motor para aeronave, e, aeronave | |
| BRPI0906171A2 (pt) | Nacela de aeronave | |
| BRPI0921772A2 (pt) | nacela de motor turbojato | |
| EP2426341A4 (en) | ENGINE | |
| BRPI0917182A2 (pt) | turbina de combustão com combustão descontínua | |
| BRPI0907959A2 (pt) | Conjunto motor para aeronave, e, aeronave | |
| BRPI0821930A2 (pt) | Conjunto de propulsão para motor turbojato | |
| BRPI0822127A2 (pt) | Nacela para motor turbojato e aeronave |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] |
Free format text: REFERENTE AS 6A E 7A ANUIDADES. PAGAR RESTAURACAO. |
|
| 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 2385 DE 20-09-2016 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. |
|
| B350 | Update of information on the portal [chapter 15.35 patent gazette] |