ES2107521T3 - Sistema para descargar a baja presion y con un alto grado de dilucion; el fluido caliente de un dispositivo de deshielo a la entrada de aire de un turbo-reactor. - Google Patents
Sistema para descargar a baja presion y con un alto grado de dilucion; el fluido caliente de un dispositivo de deshielo a la entrada de aire de un turbo-reactor.Info
- Publication number
- ES2107521T3 ES2107521T3 ES92830507T ES92830507T ES2107521T3 ES 2107521 T3 ES2107521 T3 ES 2107521T3 ES 92830507 T ES92830507 T ES 92830507T ES 92830507 T ES92830507 T ES 92830507T ES 2107521 T3 ES2107521 T3 ES 2107521T3
- Authority
- ES
- Spain
- Prior art keywords
- low pressure
- high degree
- air inlet
- turbo
- dilution
- 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.)
- Expired - Lifetime
Links
- 238000010790 dilution Methods 0.000 title 1
- 239000012895 dilution Substances 0.000 title 1
- 239000012530 fluid Substances 0.000 title 1
- 230000015572 biosynthetic process Effects 0.000 abstract 1
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
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/02—De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid
- B64D15/04—Hot gas application
-
- 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
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/047—Heating to prevent icing
-
- 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—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0233—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing means
-
- 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)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Jet Pumps And Other Pumps (AREA)
- Separation Of Particles Using Liquids (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
- Supercharger (AREA)
Abstract
LA CARCASA HUECA (4) QUE CONSTITUYE LA TOMA DE AIRE DE UN MOTOR A REACCION TIENE UNA SALIDA PARA EL AIRE CALIENTE QUE SE USA PARA EVITAR LA FORMACION DE HIELO SOBRE EL BORDE FRONTAL DE LA CARCASA. LA SALIDA ESTA CONSTITUIDA POR UNA PLURALIDAD DE RANURAS (15) QUE ESTAN DISPUESTAS Y CONFORMADAS DE MANERA TAL QUE GENERAN UN CHORRO DE BAJA PRESION DE AIRE CALIENTE QUE SUFRE UN ALTO GRADO DE MEZCLA CON EL AIRE EXTERNO Y QUE CONSECUENTEMENTE SE ENFRIA DE FORMA QUE NO QUEME LOS PANELES QUE CONSTITUYEN LA PARED EXTERIOR DEL ALOJAMIENTO DEL MOTOR QUE SE ENCUENTRAN INMEDIATAMENTE DEBAJO DE LA CORRIENTE QUE FORMA LA SALIDA DEL AIRE CALIENTE.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ITTO910750A IT1250510B (it) | 1991-10-03 | 1991-10-03 | Sistema di scarico a bassa pressione ed alta miscelazione per il fluido di riscaldamento di un dispositivo anti-ghiaccio previsto nella presa d'aria di un motore turbo-getto. |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2107521T3 true ES2107521T3 (es) | 1997-12-01 |
Family
ID=11409623
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES92830507T Expired - Lifetime ES2107521T3 (es) | 1991-10-03 | 1992-09-22 | Sistema para descargar a baja presion y con un alto grado de dilucion; el fluido caliente de un dispositivo de deshielo a la entrada de aire de un turbo-reactor. |
Country Status (7)
Country | Link |
---|---|
EP (1) | EP0536089B1 (es) |
JP (1) | JP3220258B2 (es) |
AT (1) | ATE154790T1 (es) |
DE (1) | DE69220548T2 (es) |
DK (1) | DK0536089T3 (es) |
ES (1) | ES2107521T3 (es) |
IT (1) | IT1250510B (es) |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2771451B1 (fr) * | 1997-11-21 | 2000-04-14 | Aerospatiale | Dispositif de protection pour capot d'entree d'air de moteur a reaction, pourvu d'un systeme de degivrage |
FR2771776B1 (fr) * | 1997-12-02 | 2000-01-28 | Aerospatiale | Dispositif d'evacuation d'air chaud pour capot d'entree d'air de moteur a reaction, a circuit de degivrage |
FR2772341B1 (fr) | 1997-12-12 | 2000-03-24 | Aerospatiale | Diffuseur d'air chaud pour capot d'entree d'air de moteur a reaction a circuit de degivrage |
US6267328B1 (en) * | 1999-10-21 | 2001-07-31 | Rohr, Inc. | Hot air injection for swirling rotational anti-icing system |
FR2802573B1 (fr) | 1999-12-21 | 2002-02-15 | Aerospatiale Matra Airbus | Dispositif d'evacuation d'air chaud pour capot d'entree d'air de moteur a reaction, a circuit de degivrage |
FR2924409B1 (fr) * | 2007-12-03 | 2010-05-14 | Airbus France | Nacelle d'aeronef comprenant des moyens d'evacuations d'air chaud |
US20120241561A1 (en) * | 2011-03-24 | 2012-09-27 | Cox & Company, Inc. | Method and apparatus for protecting aircraft and aircraft engines against icing |
CN103184935B (zh) * | 2011-12-28 | 2015-06-10 | 中航商用航空发动机有限责任公司 | 发动机进气道用热气防冰装置 |
EP2740905B1 (fr) * | 2012-12-07 | 2020-03-18 | Safran Aero Boosters SA | Bec de séparation d'une turbomachine axiale, compresseur et turbomachine axiale associés |
US9764847B2 (en) * | 2013-10-18 | 2017-09-19 | The Boeing Company | Anti-icing system for aircraft |
US10138811B2 (en) | 2014-03-13 | 2018-11-27 | The Boeing Company | Enhanced temperature control anti-ice nozzle |
US10221765B2 (en) | 2016-08-26 | 2019-03-05 | Honeywell International Inc. | Anti-icing exhaust system |
FR3081926B1 (fr) * | 2018-05-30 | 2021-01-15 | Safran Aircraft Engines | Embouchure d'un conduit de gaz chaud de moteur d'aeronef a travers une paroi du moteur |
US11208952B2 (en) | 2018-07-03 | 2021-12-28 | Rohr, Inc. | Inlet—NAI exhaust hole definition for reduced D-duct resonance noise and diluted exhaust plume for thermal control |
FR3086642A1 (fr) * | 2018-09-28 | 2020-04-03 | Airbus Operations | Dispositif de reduction voire de suppression du bruit tonal pour systeme de degivrage de groupe propulsif d'aeronef |
CN113804394B (zh) * | 2021-11-10 | 2023-03-21 | 中国空气动力研究与发展中心低速空气动力研究所 | 一种喷气防冰装置、冰形在线测量系统及方法 |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4482114A (en) * | 1981-01-26 | 1984-11-13 | The Boeing Company | Integrated thermal anti-icing and environmental control system |
US4782658A (en) * | 1987-05-07 | 1988-11-08 | Rolls-Royce Plc | Deicing of a geared gas turbine engine |
US5114100A (en) * | 1989-12-29 | 1992-05-19 | The Boeing Company | Anti-icing system for aircraft |
-
1991
- 1991-10-03 IT ITTO910750A patent/IT1250510B/it active IP Right Grant
-
1992
- 1992-09-22 AT AT92830507T patent/ATE154790T1/de not_active IP Right Cessation
- 1992-09-22 EP EP92830507A patent/EP0536089B1/en not_active Expired - Lifetime
- 1992-09-22 DK DK92830507.7T patent/DK0536089T3/da active
- 1992-09-22 DE DE69220548T patent/DE69220548T2/de not_active Expired - Fee Related
- 1992-09-22 ES ES92830507T patent/ES2107521T3/es not_active Expired - Lifetime
- 1992-10-02 JP JP28703392A patent/JP3220258B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
JPH06221184A (ja) | 1994-08-09 |
ATE154790T1 (de) | 1997-07-15 |
ITTO910750A0 (it) | 1991-10-03 |
IT1250510B (it) | 1995-04-08 |
EP0536089A1 (en) | 1993-04-07 |
DK0536089T3 (da) | 1998-02-02 |
EP0536089B1 (en) | 1997-06-25 |
DE69220548T2 (de) | 1998-02-19 |
DE69220548D1 (de) | 1997-07-31 |
ITTO910750A1 (it) | 1993-04-04 |
JP3220258B2 (ja) | 2001-10-22 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
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