BR112014010496A2 - torre de fixação para um motor de turbina - Google Patents
torre de fixação para um motor de turbinaInfo
- Publication number
- BR112014010496A2 BR112014010496A2 BR112014010496A BR112014010496A BR112014010496A2 BR 112014010496 A2 BR112014010496 A2 BR 112014010496A2 BR 112014010496 A BR112014010496 A BR 112014010496A BR 112014010496 A BR112014010496 A BR 112014010496A BR 112014010496 A2 BR112014010496 A2 BR 112014010496A2
- Authority
- BR
- Brazil
- Prior art keywords
- turbine engine
- fixing tower
- tower
- fixing
- turbine
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C7/00—Structures or fairings not otherwise provided for
- B64C7/02—Nacelles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
- B64C21/10—Influencing air flow over aircraft surfaces by affecting boundary layer flow using other surface properties, e.g. roughness
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
-
- 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
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/16—Aircraft characterised by the type or position of power plants of jet type
- B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
-
- 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
- B64D29/02—Power-plant nacelles, fairings, or cowlings associated with wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C2230/00—Boundary layer controls
- B64C2230/14—Boundary layer controls achieving noise reductions
-
- 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
- Y02T50/10—Drag reduction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1159953A FR2982236B1 (fr) | 2011-11-03 | 2011-11-03 | Pylone d'accrochage pour turbomachine |
| FR1159953 | 2011-11-03 | ||
| PCT/FR2012/052439 WO2013064768A2 (fr) | 2011-11-03 | 2012-10-24 | Pylone d'accrochage pour turbomachine |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| BR112014010496A2 true BR112014010496A2 (pt) | 2017-04-25 |
| BR112014010496B1 BR112014010496B1 (pt) | 2021-07-06 |
| BR112014010496B8 BR112014010496B8 (pt) | 2021-12-28 |
Family
ID=47221475
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BR112014010496A BR112014010496B8 (pt) | 2011-11-03 | 2012-10-24 | Pilar de afixação para turbomáquina |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US9938901B2 (pt) |
| EP (1) | EP2773557B1 (pt) |
| CN (1) | CN103917444B (pt) |
| BR (1) | BR112014010496B8 (pt) |
| CA (1) | CA2853903C (pt) |
| FR (1) | FR2982236B1 (pt) |
| RU (1) | RU2607715C2 (pt) |
| WO (1) | WO2013064768A2 (pt) |
Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9533754B2 (en) | 2014-04-19 | 2017-01-03 | The Boeing Company | Wing aerial refueling system |
| US11001378B2 (en) | 2016-08-08 | 2021-05-11 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
| US10464668B2 (en) | 2015-09-02 | 2019-11-05 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
| CN108137150B (zh) | 2015-09-02 | 2021-07-06 | 杰托普特拉股份有限公司 | 流体推进系统 |
| US10829206B2 (en) * | 2016-02-10 | 2020-11-10 | General Electric Company | Wing leading edge features to attenuate propeller wake-wing acoustic interactions |
| FR3050721B1 (fr) * | 2016-04-28 | 2018-04-13 | Airbus Operations | Ensemble moteur pour aeronef comprenant un bord d'attaque de mat integre a une rangee annulaire d'aubes directrices de sortie non carenees |
| EP3585683B1 (en) * | 2017-02-27 | 2021-12-15 | General Electric Company | Downstream surface features to attenuate propeller wake acoustic interactions |
| JP7155174B2 (ja) | 2017-06-27 | 2022-10-18 | ジェトプテラ、インコーポレイテッド | 航空機の垂直離着陸システムの構成 |
| CN114516404B (zh) * | 2022-02-14 | 2024-04-09 | 中国商用飞机有限责任公司 | 吊挂整流罩 |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4172574A (en) * | 1976-06-16 | 1979-10-30 | National Research Development Corporation | Fluid stream deflecting members for aircraft bodies or the like |
| US4298089A (en) * | 1976-12-23 | 1981-11-03 | The Boeing Company | Vortex generators for internal mixing in a turbofan engine |
| US4314681A (en) * | 1979-08-31 | 1982-02-09 | General Electric Company | Drag-reducing component |
| US4466587A (en) * | 1981-12-21 | 1984-08-21 | General Electric Company | Nacelle installation |
| US4966338A (en) * | 1987-08-05 | 1990-10-30 | General Electric Company | Aircraft pylon |
| US5216879A (en) * | 1991-08-30 | 1993-06-08 | United Technologies Corporation | Propulsion system assembly |
| US7802752B2 (en) * | 2002-03-20 | 2010-09-28 | The Regents Of The University Of California | Jet engine noise suppressor |
| RU2261821C2 (ru) * | 2003-12-05 | 2005-10-10 | Воронежский государственный технический университет | Щелевой закрылок |
| FR2868131B1 (fr) | 2004-03-25 | 2006-06-09 | Airbus France Sas | Tuyere primaire a chevrons pour turboreacteur a double flux d'aeronef et aeronef comportant une telle tuyere |
| UA15361U (en) * | 2006-02-22 | 2006-06-15 | Oleksandr Ivanovych Bykh | Aerohydrodynamic propeller |
| FR2905930B1 (fr) * | 2006-09-18 | 2009-05-15 | Airbus France Sa | Generateur de tourbillon en sortie de gaz chauds |
| DE102009003084B4 (de) * | 2009-05-13 | 2013-03-14 | Airbus Operations Gmbh | Verkleidung für eine Auftriebshilfe |
| FR2952349B1 (fr) * | 2009-11-06 | 2012-02-17 | Airbus Operations Sas | Procede de fabrication d'un mat reacteur equipe d'un generateur de tourbillons |
| US8651426B2 (en) | 2010-07-01 | 2014-02-18 | Rolls-Royce Plc | Jet engine installation |
-
2011
- 2011-11-03 FR FR1159953A patent/FR2982236B1/fr active Active
-
2012
- 2012-10-24 WO PCT/FR2012/052439 patent/WO2013064768A2/fr active Application Filing
- 2012-10-24 CN CN201280054191.9A patent/CN103917444B/zh active Active
- 2012-10-24 RU RU2014122331A patent/RU2607715C2/ru active
- 2012-10-24 US US14/356,045 patent/US9938901B2/en active Active
- 2012-10-24 EP EP12790614.7A patent/EP2773557B1/fr active Active
- 2012-10-24 CA CA2853903A patent/CA2853903C/fr active Active
- 2012-10-24 BR BR112014010496A patent/BR112014010496B8/pt active Search and Examination
Also Published As
| Publication number | Publication date |
|---|---|
| CA2853903A1 (fr) | 2013-05-10 |
| CA2853903C (fr) | 2019-11-12 |
| FR2982236A1 (fr) | 2013-05-10 |
| FR2982236B1 (fr) | 2014-06-27 |
| BR112014010496B8 (pt) | 2021-12-28 |
| RU2014122331A (ru) | 2015-12-10 |
| EP2773557B1 (fr) | 2020-07-15 |
| WO2013064768A3 (fr) | 2013-12-27 |
| CN103917444A (zh) | 2014-07-09 |
| EP2773557A2 (fr) | 2014-09-10 |
| US9938901B2 (en) | 2018-04-10 |
| WO2013064768A2 (fr) | 2013-05-10 |
| BR112014010496B1 (pt) | 2021-07-06 |
| US20140290270A1 (en) | 2014-10-02 |
| RU2607715C2 (ru) | 2017-01-10 |
| CN103917444B (zh) | 2016-05-11 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| BR112014007288A2 (pt) | motor de turbina a gás | |
| BR112014010747A2 (pt) | aparelho de cobertura para um motor de turbina a gás | |
| BR112014010496A2 (pt) | torre de fixação para um motor de turbina | |
| BR112014016305A8 (pt) | motor de turbina a gás | |
| BR112014016277A2 (pt) | motor de turbina a gás | |
| BR112014007878A2 (pt) | motor de turbina a gás | |
| BR112014016303A2 (pt) | motor de turbina a gás | |
| BR112014016273A2 (pt) | motor de turbina a gás | |
| BR112014016281A2 (pt) | motor de turbina a gás | |
| BR112014016300A2 (pt) | motor de turbina a gás | |
| DK2527649T3 (da) | Fremgangsmåde til inspektion af komponenter af en vindmølle | |
| DK2520533T4 (da) | Servicekran til en vindmølle | |
| CO6970572A2 (es) | Álabe para un generador eólico y método para el montaje de dicho álabe | |
| DK2665942T4 (da) | Rotorleje til en vindmølle | |
| BR112015010425A2 (pt) | aparelhos de invólucro de turbina para um motor de turbina a gás | |
| EP2794182A4 (en) | SUPPORT STRUCTURE FOR A GAS TURBINE ENGINE | |
| BR112014026803A2 (pt) | montagem de invólucro para um motor de turbina a gás | |
| BR112015002954A2 (pt) | sistema de resfriamento integrado para uma nacele de uma turbina eólica | |
| DK2551512T3 (da) | Forbindelsesanordning på en vindmøllevinge | |
| DK2520798T3 (da) | Køleindretning hos en vindmølle | |
| GB2490216B (en) | A turbine wheel for a turbine engine | |
| GB201114669D0 (en) | Turbine engine | |
| DK2595308T3 (da) | System til forbedret vindmøllegeneratorydelse | |
| BR112014026258A2 (pt) | conjunto de recipiente, método para montar um conjunto de recipiente e motor de turbina a gás | |
| DK2573387T4 (da) | Nacelle til en vindmølle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| B06F | Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette] | ||
| B06U | Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette] | ||
| B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
| B16A | Patent or certificate of addition of invention granted [chapter 16.1 patent gazette] |
Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 24/10/2012, OBSERVADAS AS CONDICOES LEGAIS. |
|
| B09W | Correction of the decision to grant [chapter 9.1.4 patent gazette] |
Free format text: RETIFICACAO NO PARECER DE DEFERIMENTO. |
|
| B16C | Correction of notification of the grant [chapter 16.3 patent gazette] |
Free format text: REFERENTE AO DESPACHO 16.1 PUBLICADO NA RPI 2635 DE 06.07.2021, QUANTO AO TITULO E AS REIVINDICACOES |
|
| B16C | Correction of notification of the grant [chapter 16.3 patent gazette] |
Free format text: REFERENTE AO DESPACHO 16.1 PUBLICADO NA RPI 2635 DE 06.07.2021, QUANTO AO TITULO E AS REIVINDICACOES. |