DK0536089T3 - System til udtømning af det opvarmede fluidum fra en afisningsanordning i luftindtaget til en turbojetmotor ved et lavt tryk og med en høj grad af blanding - Google Patents
System til udtømning af det opvarmede fluidum fra en afisningsanordning i luftindtaget til en turbojetmotor ved et lavt tryk og med en høj grad af blandingInfo
- Publication number
- DK0536089T3 DK0536089T3 DK92830507.7T DK92830507T DK0536089T3 DK 0536089 T3 DK0536089 T3 DK 0536089T3 DK 92830507 T DK92830507 T DK 92830507T DK 0536089 T3 DK0536089 T3 DK 0536089T3
- Authority
- DK
- Denmark
- Prior art keywords
- mixing
- high degree
- air intake
- turbojet engine
- discharging
- Prior art date
Links
- 238000007599 discharging Methods 0.000 title 1
- 239000012530 fluid Substances 0.000 title 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)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Jet Pumps And Other Pumps (AREA)
- Separation Of Particles Using Liquids (AREA)
- Supercharger (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
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 |
---|---|
DK0536089T3 true DK0536089T3 (da) | 1998-02-02 |
Family
ID=11409623
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DK92830507.7T DK0536089T3 (da) | 1991-10-03 | 1992-09-22 | System til udtømning af det opvarmede fluidum fra en afisningsanordning i luftindtaget til en turbojetmotor ved et lavt tryk og med en høj grad af blanding |
Country Status (7)
Country | Link |
---|---|
EP (1) | EP0536089B1 (da) |
JP (1) | JP3220258B2 (da) |
AT (1) | ATE154790T1 (da) |
DE (1) | DE69220548T2 (da) |
DK (1) | DK0536089T3 (da) |
ES (1) | ES2107521T3 (da) |
IT (1) | IT1250510B (da) |
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 DE DE69220548T patent/DE69220548T2/de not_active Expired - Fee Related
- 1992-09-22 DK DK92830507.7T patent/DK0536089T3/da active
- 1992-09-22 EP EP92830507A patent/EP0536089B1/en not_active Expired - Lifetime
- 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 |
---|---|
DE69220548D1 (de) | 1997-07-31 |
ATE154790T1 (de) | 1997-07-15 |
ITTO910750A0 (it) | 1991-10-03 |
JPH06221184A (ja) | 1994-08-09 |
EP0536089B1 (en) | 1997-06-25 |
IT1250510B (it) | 1995-04-08 |
EP0536089A1 (en) | 1993-04-07 |
DE69220548T2 (de) | 1998-02-19 |
ITTO910750A1 (it) | 1993-04-04 |
JP3220258B2 (ja) | 2001-10-22 |
ES2107521T3 (es) | 1997-12-01 |
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