ES2563437T3 - Turboventilador de aeronave - Google Patents
Turboventilador de aeronave Download PDFInfo
- Publication number
- ES2563437T3 ES2563437T3 ES11774209.8T ES11774209T ES2563437T3 ES 2563437 T3 ES2563437 T3 ES 2563437T3 ES 11774209 T ES11774209 T ES 11774209T ES 2563437 T3 ES2563437 T3 ES 2563437T3
- Authority
- ES
- Spain
- Prior art keywords
- turbofan
- fairing
- wings
- turbo fan
- fan
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
-
- 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
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
- F02K1/006—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector within one plane only
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/12—Fluid guiding means, e.g. vanes
-
- 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
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Toys (AREA)
Abstract
Turboventilador de aeronave, estando el turboventilador compuesto por un ventilador (1), un estator (2), un carenado interno (4) y un carenado externo (3), apropiado para envolver el ventilador y el estator, que comprende al menos dos alas (5) dispuestas en el interior del turboventilador, entre el carenado externo y el carenado interno del turboventilador y externamente al carenado interno (4) del turboventilador, caracterizado por que cada una de las alas (5) está conectada por dos soportes articulados (6) o soportes no articulados (6), que fijan cada una de las alas (5) sobre la estructura del turboventilador, estando los soportes situados aproximadamente en la misma sección transversal de la ubicación del centro de gravedad del turboventilador, y aproximadamente en la misma sección transversal de la ubicación del centro de sustentación de cada una de las dos pequeñas alas (5), internamente al carenado externo (3) del turboventilador (1).
Description
Claims (1)
-
imagen1
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BRPI1001223 | 2010-04-27 | ||
BRPI1001223-0A2A BRPI1001223A2 (pt) | 2010-04-27 | 2010-04-27 | Conjunto de aerofólio para turbo ventilador de avião |
PCT/BR2011/000122 WO2011134031A1 (en) | 2010-04-27 | 2011-04-27 | Airfoil combination for aircraft turbofan |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2563437T3 true ES2563437T3 (es) | 2016-03-15 |
Family
ID=44860682
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES11774209.8T Active ES2563437T3 (es) | 2010-04-27 | 2011-04-27 | Turboventilador de aeronave |
Country Status (5)
Country | Link |
---|---|
US (1) | US9222436B2 (es) |
EP (1) | EP2564051B1 (es) |
BR (1) | BRPI1001223A2 (es) |
ES (1) | ES2563437T3 (es) |
WO (1) | WO2011134031A1 (es) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10730635B1 (en) * | 2019-08-23 | 2020-08-04 | Raytheon Technologies Corporation | Engine wing |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2991961A (en) | 1959-05-06 | 1961-07-11 | Francis M Rogallo | Jet aircraft configuration |
US3248878A (en) * | 1963-09-18 | 1966-05-03 | Gen Electric | Thrust deflector and reverser |
GB1071764A (en) | 1964-08-31 | 1967-06-14 | Graham Watt | Improvements in or relating to aircraft or other vehicles having a sustaining or lift effect airfoil |
US3330500A (en) * | 1965-03-22 | 1967-07-11 | Ltv Aerospace Corp | Propulsive wing airplane |
FR2129994B1 (es) * | 1971-03-25 | 1975-01-17 | Snecma | |
US4019696A (en) | 1973-12-28 | 1977-04-26 | The Boeing Company | Method of and apparatus for enhancing Coanda flow attachment over a wing and flap surface |
US3997132A (en) * | 1974-12-11 | 1976-12-14 | The Garrett Corporation | Method and apparatus for controlling tip vortices |
US4117995A (en) | 1977-02-28 | 1978-10-03 | Runge Thomas M | Aircraft wing lift augmentation device |
GB2019793B (en) * | 1978-04-29 | 1982-05-12 | British Aerospace | Flow detector blades |
US4205813A (en) * | 1978-06-19 | 1980-06-03 | General Electric Company | Thrust vectoring apparatus for a VTOL aircraft |
US4505443A (en) * | 1978-12-29 | 1985-03-19 | General Dynamics Corporation | Propulsion system for a V/STOL airplane |
US4326686A (en) | 1980-02-15 | 1982-04-27 | Runge Thomas M | Fan jet engine bypass air delivery system for blown wing aircraft lift augmentation device |
US4392621A (en) | 1981-04-07 | 1983-07-12 | Hermann Viets | Directional control of engine exhaust thrust vector in a STOL-type aircraft |
US4506850A (en) * | 1983-01-04 | 1985-03-26 | The Boeing Company | Engine installation for aircraft |
US7293401B2 (en) * | 2002-03-20 | 2007-11-13 | The Regents Of The University Of California | Jet engine noise suppressor |
-
2010
- 2010-04-27 BR BRPI1001223-0A2A patent/BRPI1001223A2/pt not_active Application Discontinuation
-
2011
- 2011-04-27 US US13/643,448 patent/US9222436B2/en not_active Expired - Fee Related
- 2011-04-27 WO PCT/BR2011/000122 patent/WO2011134031A1/en active Application Filing
- 2011-04-27 ES ES11774209.8T patent/ES2563437T3/es active Active
- 2011-04-27 EP EP11774209.8A patent/EP2564051B1/en not_active Not-in-force
Also Published As
Publication number | Publication date |
---|---|
US20130045087A1 (en) | 2013-02-21 |
EP2564051B1 (en) | 2015-12-16 |
BRPI1001223A2 (pt) | 2014-03-25 |
EP2564051A1 (en) | 2013-03-06 |
US9222436B2 (en) | 2015-12-29 |
EP2564051A4 (en) | 2013-12-25 |
WO2011134031A1 (en) | 2011-11-03 |
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