ES2180839T3 - Sistema de eyector de refrigeracion de aceite para un grupo propulsor auxiliar de una aeronave. - Google Patents
Sistema de eyector de refrigeracion de aceite para un grupo propulsor auxiliar de una aeronave.Info
- Publication number
- ES2180839T3 ES2180839T3 ES97104818T ES97104818T ES2180839T3 ES 2180839 T3 ES2180839 T3 ES 2180839T3 ES 97104818 T ES97104818 T ES 97104818T ES 97104818 T ES97104818 T ES 97104818T ES 2180839 T3 ES2180839 T3 ES 2180839T3
- Authority
- ES
- Spain
- Prior art keywords
- mounting chamber
- airplane
- oil
- air
- auxiliary
- 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
- 238000012423 maintenance Methods 0.000 abstract 2
- 239000007789 gas Substances 0.000 abstract 1
- 238000005057 refrigeration Methods 0.000 abstract 1
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
- F02C7/12—Cooling of plants
- F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
-
- 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
-
- 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
- F05D2260/00—Function
- F05D2260/60—Fluid transfer
- F05D2260/601—Fluid transfer using an ejector or a jet pump
-
- 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)
- Jet Pumps And Other Pumps (AREA)
- Cooling Or The Like Of Electrical Apparatus (AREA)
- Supercharger (AREA)
Abstract
SISTEMA EYECTOR DE REFRIGERACION DE ACEITE PARA UN MECANISMO AUXILIAR DE PROPULSION DE AVION (3) QUE SE DISPONE EN LA CAMARA DE MONTAJE (1) DEL FINAL DE LA POPA (2) DE UN AVION, DONDE LA CAMARA DE MONTAJE (1) ES ACCESIBLE POR UNA COMPUERTA DE MANTENIMIENTO (15). UNA BOMBA DE EYECCION (8) UTILIZA LA ENERGIA CINETICA DEL HAZ DE GASES DE ESCAPE (5) DEL MECANISMO AUXILIAR DE PROPULSION (3) PARA GENERAR UNA CORRIENTE DE ASPIRACION QUE HACE PASAR AIRE FRIO DE LA CAMARA DE MONTAJE (1) POR EL REFRIGERADOR DEL ACEITE (10). PARA GARANTIZAR EL FUNCIONAMIENTO CORRECTO DEL REFRIGERADOR DEL ACEITE (10) TANTO EN SERVICIO DE TIERRA COMO EN VUELO, SE HA PREVISTO QUE EN LA COMPUERTA DE MANTENIMIENTO (15) SE PRACTIQUE UNA ENTRADA DE AIRE (4) QUE TERMINA A RAS DE FUSELAJE. EN SERVICIO DE TIERRA, POR ESTA ENTRADA DE AIRE (4) SE ASPIRA AIRE DE ALREDEDOR DEL AVION HACIA LA CAMARA DE MONTAJE (1) HASTA EL REFRIGERADOR DEL ACEITE (10), Y EN SERVICIO DE VUELO UNA PARTE DEL AIRE QUE CIRCULA EN TORNO AL AVION ENTRA ENLA CAMARA DE MONTAJE (1) CON UNA PRESION TAN ALTA QUE EN LA CAMARA DE MONTAJE (1) SE DISPONE DE UN EXCESO DE PRESION FRENTE A LA CONTRAPRESION EXISTENTE EN EL TUBO DE GASES DE ESCAPE (6).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19619535A DE19619535C1 (de) | 1996-05-15 | 1996-05-15 | Ejektor-Ölkühlsystem für ein Flugzeug-Hilfstriebwerk |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2180839T3 true ES2180839T3 (es) | 2003-02-16 |
Family
ID=7794356
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES97104818T Expired - Lifetime ES2180839T3 (es) | 1996-05-15 | 1997-03-21 | Sistema de eyector de refrigeracion de aceite para un grupo propulsor auxiliar de una aeronave. |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0807576B1 (es) |
DE (2) | DE19619535C1 (es) |
ES (1) | ES2180839T3 (es) |
RU (1) | RU2131380C1 (es) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6092360A (en) * | 1998-07-01 | 2000-07-25 | The Boeing Company | Auxiliary power unit passive cooling system |
US6615576B2 (en) | 2001-03-29 | 2003-09-09 | Honeywell International Inc. | Tortuous path quiet exhaust eductor system |
US6651929B2 (en) | 2001-10-29 | 2003-11-25 | Pratt & Whitney Canada Corp. | Passive cooling system for auxiliary power unit installation |
US20060163425A1 (en) * | 2005-01-27 | 2006-07-27 | Honeywell International, Inc. | Aircraft inlet assembly for reducing auxiliary power unit noise |
DE102007061588B4 (de) | 2007-12-20 | 2011-07-21 | Airbus Operations GmbH, 21129 | Flugzeugkühlsystem |
US8444083B2 (en) | 2011-06-30 | 2013-05-21 | Hamilton Sundstrand Corporation | Auxiliary power unit inlet |
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 |
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 |
RU2587733C1 (ru) * | 2015-01-13 | 2016-06-20 | Открытое акционерное общество "Научно-производственное предприятие "Аэросила" | Эжекторная система охлаждения масла в энергетической установке |
RU2632561C2 (ru) * | 2016-02-15 | 2017-10-05 | Владимир Леонидович Письменный | Воздухо-воздушный радиатор и способ повышения его эффективности |
RU2696521C1 (ru) * | 2018-05-17 | 2019-08-02 | Общество с ограниченной ответственностью "Газпром трансгаз Ухта" | Способ снижения температуры воздуха в полости между коническим корпусом силовой турбины двигателя ал-31стн и внутренним корпусом улитки газоперекачивающего агрегата ц1-16л/76-1,44 |
WO2023002131A1 (fr) * | 2021-07-21 | 2023-01-26 | Flying Whales | Systeme pour gerer thermiquement une nacelle externe de production d'energie electrique equipant un dirigeable a propulsion electrique, nacelle et dirigeable equipes de ce systeme |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1803156A (en) * | 1930-03-24 | 1931-04-28 | Wagner Rudolf | Air-cooled condenser for steam-driven vehicles |
DE733564C (de) * | 1938-03-17 | 1943-03-29 | Ettore Bugatti | Kuehleranordnung an Flugzeugen |
GB723406A (en) * | 1952-12-29 | 1955-02-09 | Northrop Aircraft Inc | Improvements in or relating to aircraft jet engine cooling system |
US4504030A (en) * | 1982-12-06 | 1985-03-12 | United Technologies Corporation | Cooling means |
US5265408A (en) * | 1992-02-13 | 1993-11-30 | Allied-Signal Inc. | Exhaust eductor cooling system |
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 |
-
1996
- 1996-05-15 DE DE19619535A patent/DE19619535C1/de not_active Expired - Lifetime
-
1997
- 1997-03-21 ES ES97104818T patent/ES2180839T3/es not_active Expired - Lifetime
- 1997-03-21 EP EP97104818A patent/EP0807576B1/de not_active Expired - Lifetime
- 1997-03-21 DE DE59707946T patent/DE59707946D1/de not_active Expired - Lifetime
- 1997-05-14 RU RU97108163A patent/RU2131380C1/ru active
Also Published As
Publication number | Publication date |
---|---|
EP0807576B1 (de) | 2002-08-14 |
DE19619535C1 (de) | 1997-10-30 |
EP0807576A3 (de) | 1998-05-27 |
RU2131380C1 (ru) | 1999-06-10 |
DE59707946D1 (de) | 2002-09-19 |
EP0807576A2 (de) | 1997-11-19 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
ES2180839T3 (es) | Sistema de eyector de refrigeracion de aceite para un grupo propulsor auxiliar de una aeronave. | |
US7337605B2 (en) | Thermal management for aircraft auxiliary power unit compartment | |
US9254920B2 (en) | Aircraft energy management system including engine fan discharge air boosted environmental control system | |
US2474258A (en) | Turbine apparatus | |
US20160017751A1 (en) | Cooling device for a turbojet engine of an aircraft nacelle | |
US20170002741A1 (en) | Air cooled air cooler for gas turbine engine air system | |
MX9307295A (es) | Mejoras en sistemas de refrigeracion y aire acondicionado que utilizan un criogeno. | |
CN104276287A (zh) | 飞机空调系统和操作飞机空调系统的方法 | |
US2502332A (en) | Aspirator compressor type jet propulsion apparatus | |
CN106697297B (zh) | 一种可同时提供液冷与风冷的环控系统 | |
US2477932A (en) | Aircraft evaporative cooling system | |
US10293946B2 (en) | Hybrid electric | |
US2453923A (en) | Aircraft cooling by air turbine means | |
US20160362188A1 (en) | Fuel tank inerting apparatus for aircraft | |
CN110067673B (zh) | 一种并联式预冷冲压组合推进系统和推进方法 | |
MX9307300A (es) | Mejoras en aparato de refrigeracion y aire acondicionado que utilizan un criogeno. | |
US2439473A (en) | Pressurized protective conduit for hot gas power plants | |
US2789416A (en) | System for cooling a turbine bearing of a gas turbine power plant | |
US6484518B1 (en) | Method and system for feeding a cool air inlet of the cabin of an aircraft propelled by at least one jet engine | |
US2079923A (en) | Thermal power plant | |
US20120322354A1 (en) | Heat pump for supplemental heat | |
US20230339616A1 (en) | Environmental control system with air powered pump | |
US2379541A (en) | Feed of exhaust gases to turbosuperchargers | |
US2086520A (en) | Device for cooling quick firing arms | |
EP3812680B1 (en) | Cooling system |