DE69920584D1 - Passives Kühlsystem zur Kühlung der Hilfskrafteinheit eines Flugzeuges - Google Patents
Passives Kühlsystem zur Kühlung der Hilfskrafteinheit eines FlugzeugesInfo
- Publication number
- DE69920584D1 DE69920584D1 DE69920584T DE69920584T DE69920584D1 DE 69920584 D1 DE69920584 D1 DE 69920584D1 DE 69920584 T DE69920584 T DE 69920584T DE 69920584 T DE69920584 T DE 69920584T DE 69920584 D1 DE69920584 D1 DE 69920584D1
- Authority
- DE
- Germany
- Prior art keywords
- cooling
- aircraft
- power unit
- auxiliary power
- cooling system
- 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.)
- Revoked
Links
- 238000001816 cooling Methods 0.000 title 2
Classifications
-
- 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
- F02C7/32—Arrangement, mounting, or driving, of auxiliaries
-
- 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
- B64D33/08—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
-
- 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
- B64D41/00—Power installations for auxiliary purposes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/08—Cooling; Heating; Heat-insulation
- F01D25/12—Cooling
-
- 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
- F02C7/12—Cooling of 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
- 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
- B64D2033/0213—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for auxiliary power units (APU's)
-
- 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
- B64D41/00—Power installations for auxiliary purposes
- B64D2041/002—Mounting arrangements for auxiliary power units (APU's)
-
- 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
- F05D2220/00—Application
- F05D2220/50—Application for auxiliary power units (APU's)
-
- 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
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
-
- 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
- Y02T50/40—Weight reduction
-
- 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)
- Jet Pumps And Other Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/108,900 US6092360A (en) | 1998-07-01 | 1998-07-01 | Auxiliary power unit passive cooling system |
US108900 | 1998-07-01 |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69920584D1 true DE69920584D1 (de) | 2004-11-04 |
DE69920584T2 DE69920584T2 (de) | 2005-11-17 |
Family
ID=22324705
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69920584T Revoked DE69920584T2 (de) | 1998-07-01 | 1999-07-01 | Kühlsysteme zur Verwendung mit Hilfskrafteinheiten in Flugzeugen |
Country Status (3)
Country | Link |
---|---|
US (1) | US6092360A (de) |
EP (2) | EP0968918B1 (de) |
DE (1) | DE69920584T2 (de) |
Families Citing this family (84)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2788308A1 (fr) * | 1999-01-07 | 2000-07-13 | Snecma | Dispositif de refroidissement d'un reducteur de vitesse de turbomachine |
CA2329555A1 (en) * | 2000-12-22 | 2002-06-22 | Jose Albero | Main propulsion engine system integrated with secondary power unit |
US6575406B2 (en) | 2001-01-19 | 2003-06-10 | The Boeing Company | Integrated and/or modular high-speed aircraft |
US6615576B2 (en) | 2001-03-29 | 2003-09-09 | Honeywell International Inc. | Tortuous path quiet exhaust eductor system |
US6580179B2 (en) | 2001-06-07 | 2003-06-17 | Honeywell International Inc. | Ram air turbine with high power density generator and self-contained fluid cooling loop |
US6651929B2 (en) * | 2001-10-29 | 2003-11-25 | Pratt & Whitney Canada Corp. | Passive cooling system for auxiliary power unit installation |
DE10200459A1 (de) * | 2002-01-09 | 2003-07-24 | Airbus Gmbh | Lufteinlauf für ein Hilfstriebwerk in einem Flugzeug |
US7644888B2 (en) * | 2002-05-15 | 2010-01-12 | The Boeing Company | High-speed aircraft and methods for their manufacture |
US6651928B1 (en) | 2002-09-05 | 2003-11-25 | The Boeing Company | Aircraft engine nacelles and methods for their manufacture |
US7210653B2 (en) * | 2002-10-22 | 2007-05-01 | The Boeing Company | Electric-based secondary power system architectures for aircraft |
US6851255B2 (en) * | 2002-12-18 | 2005-02-08 | Pratt & Whitney Canada Corp. | Normally open reverse flow flapper valve |
US7337605B2 (en) * | 2003-10-10 | 2008-03-04 | Hamilton Sundstrand Corporation | Thermal management for aircraft auxiliary power unit compartment |
US7150431B2 (en) * | 2004-01-14 | 2006-12-19 | Mjd Innovations, L.L.C. | Electrical generator fluid-flow-coolant filtration |
US20050200858A1 (en) * | 2004-01-28 | 2005-09-15 | Hamilton Sundstrand Corporation | Contoured inspection plug for low pressure drop |
US7231767B2 (en) * | 2004-04-16 | 2007-06-19 | Pratt & Whitney Canada Corp. | Forced air cooling system |
US7152410B2 (en) * | 2004-06-10 | 2006-12-26 | Honeywell International, Inc. | System and method for dumping surge flow into eductor primary nozzle for free turbine |
US20060032974A1 (en) * | 2004-08-16 | 2006-02-16 | Honeywell International Inc. | Modular installation kit for auxiliary power unit |
US7377100B2 (en) * | 2004-08-27 | 2008-05-27 | Pratt & Whitney Canada Corp. | Bypass duct fluid cooler |
US7267297B2 (en) * | 2004-09-02 | 2007-09-11 | The Boeing Company | Integrated axially varying engine muffler, and associated methods and systems |
US20060059891A1 (en) * | 2004-09-23 | 2006-03-23 | Honeywell International, Inc. | Quiet chevron/tab exhaust eductor system |
US7364116B2 (en) * | 2004-09-27 | 2008-04-29 | The Boeing Company | Automatic control systems for aircraft auxiliary power units, and associated methods |
US7344107B2 (en) * | 2004-10-26 | 2008-03-18 | The Boeing Company | Dual flow APU inlet and associated systems and methods |
US8127527B2 (en) * | 2004-11-22 | 2012-03-06 | General Electric Company | Methods and systems for operating oxidizer systems |
US20060157613A1 (en) * | 2005-01-19 | 2006-07-20 | Adamson Eric E | Supersonic aircraft with active lift distribution control for reducing sonic boom |
US20060163425A1 (en) * | 2005-01-27 | 2006-07-27 | Honeywell International, Inc. | Aircraft inlet assembly for reducing auxiliary power unit noise |
US7513119B2 (en) * | 2005-02-03 | 2009-04-07 | The Boeing Company | Systems and methods for starting aircraft engines |
US7698896B2 (en) * | 2005-07-27 | 2010-04-20 | Honeywell International Inc. | Compact, light weight eductor oil cooler plenum and surge flow plenum design |
US8371521B2 (en) * | 2006-03-16 | 2013-02-12 | Pratt & Whitney | Low noise exhaust ducting system |
US7600714B2 (en) * | 2006-04-20 | 2009-10-13 | Honeywell International Inc. | Diffusing air inlet door assembly |
US20080053060A1 (en) * | 2006-08-29 | 2008-03-06 | Pratt & Whitney Canada Corp. | Bypass lip seal |
US7861512B2 (en) * | 2006-08-29 | 2011-01-04 | Pratt & Whitney Canada Corp. | Turbofan bypass duct air cooled fluid cooler installation |
US7857257B2 (en) * | 2006-09-01 | 2010-12-28 | United Technologies Corporation | Aircraft thermal management system with reduced exhaust re-ingestion |
US7690598B1 (en) * | 2006-09-11 | 2010-04-06 | Plattner Wesley M | Aircraft exhaust vent assembly |
DE102006042584B4 (de) | 2006-09-11 | 2008-11-20 | Airbus Deutschland Gmbh | Luftzufuhrsystem eines Flugzeuges sowie Verfahren zum Vermischen zweier Luftströme in einem Luftzufuhrsystem |
US7765784B2 (en) * | 2006-09-25 | 2010-08-03 | The Boeing Company | Thermally compliant APU exhaust duct arrangements and associated systems and methods |
US20080203218A1 (en) * | 2007-02-26 | 2008-08-28 | Honeywell International, Inc. | Systems And Methods For Reducing Pressure Loss Of Air Flowing From A First Area To A Second Area |
US20080236939A1 (en) * | 2007-03-30 | 2008-10-02 | Hamilton Sundstrand Corporation | Exhaust silencer assembly |
US7862293B2 (en) * | 2007-05-03 | 2011-01-04 | Pratt & Whitney Canada Corp. | Low profile bleed air cooler |
US9194293B2 (en) * | 2007-09-18 | 2015-11-24 | Hamilton Sundstrand Corporation | Air inlet noise attenuation assembly |
US7578369B2 (en) * | 2007-09-25 | 2009-08-25 | Hamilton Sundstrand Corporation | Mixed-flow exhaust silencer assembly |
DE102007061588B4 (de) * | 2007-12-20 | 2011-07-21 | Airbus Operations GmbH, 21129 | Flugzeugkühlsystem |
US20100005806A1 (en) * | 2008-07-14 | 2010-01-14 | Donnelly Brian G | Eductor system for a gas turbine engine |
US8181443B2 (en) * | 2008-12-10 | 2012-05-22 | Pratt & Whitney Canada Corp. | Heat exchanger to cool turbine air cooling flow |
US8245494B2 (en) * | 2009-02-12 | 2012-08-21 | Hamilton Sundstrand Corporation | Gas turbine engine with eductor and eductor flow distribution shield |
DE102009013159A1 (de) * | 2009-03-16 | 2010-09-23 | Airbus Operations Gmbh | Kühler für ein Flugzeugkühlsystem, Flugzeugkühlsystem und Verfahren zum Betreiben eines Flugzeugkühlsystems |
US8657227B1 (en) | 2009-09-11 | 2014-02-25 | The Boeing Company | Independent power generation in aircraft |
US8621842B2 (en) | 2010-05-05 | 2014-01-07 | Hamilton Sundstrand Corporation | Exhaust silencer convection cooling |
US8602717B2 (en) | 2010-10-28 | 2013-12-10 | United Technologies Corporation | Compression system for turbomachine heat exchanger |
US8738268B2 (en) | 2011-03-10 | 2014-05-27 | The Boeing Company | Vehicle electrical power management and distribution |
US8596568B2 (en) | 2011-04-26 | 2013-12-03 | Hamilton Sundstrand Corporation | Exhaust silencer with baffles |
US8973552B2 (en) | 2011-06-27 | 2015-03-10 | United Technologies Corporation | Integral oil system |
US9188065B2 (en) * | 2011-08-03 | 2015-11-17 | Hamilton Sundstrand Corporation | APU selective cool down cycle |
US9254924B2 (en) | 2011-08-12 | 2016-02-09 | Hamilton Sundstrand Corporation | Pressure influencing assembly for an aircraft auxiliary system |
FR2986275B1 (fr) * | 2012-02-01 | 2016-07-01 | Turbomeca | Procede d'ejection de gaz d'echappement de turbine a gaz et ensemble d'echappement de configuration optimisee |
US9279386B2 (en) | 2012-03-09 | 2016-03-08 | Hamilton Sundstrand Corporation | Jet noise reduction using eduction effect |
CN102673793B (zh) * | 2012-06-08 | 2015-04-29 | 中国航空工业集团公司西安飞机设计研究所 | 一种飞机辅助动力装置排气引射系统 |
US9097134B2 (en) | 2012-09-14 | 2015-08-04 | Pratt & Whitney Canada Corp. | Air cooling design for tail-cone generator installation |
US9458764B2 (en) | 2012-11-26 | 2016-10-04 | Pratt & Whitney Canada Corp. | Air cooled air cooler for gas turbine engine air system |
US9611050B2 (en) | 2013-07-26 | 2017-04-04 | The Boeing Company | Auxiliary power unit inlet apparatus and methods |
US9541030B2 (en) * | 2013-11-27 | 2017-01-10 | Lockheed Martin Corporation | Exhaust plume cooling using periodic interruption of exhaust gas flow to form ambient air entraining vortices |
DE102014208154A1 (de) * | 2014-04-30 | 2015-11-05 | Airbus Operations Gmbh | Flugzeugheckbereich mit einem Kühlsystem und Verfahren zur Kühlung einer wärmeerzeugenden Vorrichtung |
GB201416407D0 (en) | 2014-09-17 | 2014-10-29 | Rolls Royce Plc | Aircraft environmental control system air duct arrangement |
US10253726B2 (en) | 2015-08-07 | 2019-04-09 | Pratt & Whitney Canada Corp. | Engine assembly with combined engine and cooling exhaust |
US10240522B2 (en) * | 2015-08-07 | 2019-03-26 | Pratt & Whitney Canada Corp. | Auxiliary power unit with combined cooling of generator |
US10676205B2 (en) | 2016-08-19 | 2020-06-09 | General Electric Company | Propulsion engine for an aircraft |
US10800539B2 (en) * | 2016-08-19 | 2020-10-13 | General Electric Company | Propulsion engine for an aircraft |
US11105340B2 (en) | 2016-08-19 | 2021-08-31 | General Electric Company | Thermal management system for an electric propulsion engine |
US10670178B2 (en) | 2017-04-19 | 2020-06-02 | General Electric Company | Slip joint assembly |
US10415502B2 (en) | 2017-09-11 | 2019-09-17 | Honeywell International Inc. | Swirling flow eductor system and method |
EP3476741B1 (de) * | 2017-10-30 | 2021-08-25 | Airbus Operations, S.L. | Flugzeug-tailcone mit einem ringförmigen apu-lufteinlass |
US20190218972A1 (en) * | 2018-01-18 | 2019-07-18 | General Electric Company | Thermally protected thermoplastic duct and assembly |
FR3079820B1 (fr) * | 2018-04-09 | 2020-04-17 | Safran Electrical & Power | Systeme et procede de demarrage/generation pour turbomachine d'aeronef |
US11085372B2 (en) * | 2018-07-18 | 2021-08-10 | The Boeing Company | Anti-ice system exhaust air disruptor |
US11156128B2 (en) | 2018-08-22 | 2021-10-26 | General Electric Company | Embedded electric machine |
CN109573074A (zh) * | 2018-11-30 | 2019-04-05 | 中国航空工业集团公司金城南京机电液压工程研究中心 | 一种用于飞机辅助动力装置的滑油冷却系统 |
EP3926157B1 (de) * | 2019-02-13 | 2024-05-15 | IHI Corporation | Kühlsystem für ein gasturbinentriebwerk eines flugzeugs |
US10967983B2 (en) | 2019-06-05 | 2021-04-06 | Pratt & Whitney Canada Corp. | Aircraft power plant |
US10875660B1 (en) | 2019-06-05 | 2020-12-29 | Pratt & Whitney Canada Corp. | Aircraft power plant |
US11300053B2 (en) | 2019-10-02 | 2022-04-12 | Honeywell International Inc. | Passive flame arrestor system |
CN110901930A (zh) * | 2019-12-06 | 2020-03-24 | 西安爱生技术集团公司 | 一种活塞发动机后置通风冷却装置 |
US11352885B2 (en) | 2020-04-08 | 2022-06-07 | Pratt & Whitney Canada Corp. | Aircraft power plant cooling system |
US11578621B2 (en) | 2020-04-08 | 2023-02-14 | General Electric Company | System for cooling turbine shaft coupling |
EP4155210B1 (de) * | 2021-09-28 | 2024-05-29 | Airbus Operations, S.L.U. | Flugzeug mit einer brennkraftmaschine mit einem auspuff vor seinem lufteinlass |
JP7496812B2 (ja) | 2021-12-28 | 2024-06-07 | 本田技研工業株式会社 | ミキサ及び移動体 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3891248A (en) * | 1974-05-09 | 1975-06-24 | American Air Filter Co | Expansion joint |
ATE146575T1 (de) * | 1991-09-14 | 1997-01-15 | Seetru Ltd | Rohrkupplung |
US5265408A (en) * | 1992-02-13 | 1993-11-30 | Allied-Signal Inc. | Exhaust eductor cooling system |
US5665359A (en) * | 1994-04-29 | 1997-09-09 | Ho; Walter Kwok Keung | Method and compositions for lowering blood lipids |
US5655359A (en) | 1995-05-15 | 1997-08-12 | The Boeing Company | Passive cooling device and method for cooling an auxiliary power unit on an airplane |
DE19524731A1 (de) * | 1995-07-07 | 1997-01-09 | Bmw Rolls Royce Gmbh | Turboprop-Triebwerk mit einem Luft-Ölkühler |
DE19619535C1 (de) * | 1996-05-15 | 1997-10-30 | Daimler Benz Aerospace Airbus | Ejektor-Ölkühlsystem für ein Flugzeug-Hilfstriebwerk |
-
1998
- 1998-07-01 US US09/108,900 patent/US6092360A/en not_active Expired - Fee Related
-
1999
- 1999-07-01 DE DE69920584T patent/DE69920584T2/de not_active Revoked
- 1999-07-01 EP EP99202134A patent/EP0968918B1/de not_active Revoked
- 1999-07-01 EP EP04075128A patent/EP1433703A1/de not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
EP0968918B1 (de) | 2004-09-29 |
EP1433703A1 (de) | 2004-06-30 |
US6092360A (en) | 2000-07-25 |
DE69920584T2 (de) | 2005-11-17 |
EP0968918A2 (de) | 2000-01-05 |
EP0968918A3 (de) | 2001-07-18 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8363 | Opposition against the patent | ||
8331 | Complete revocation |