SE8406514L - Kylsystem for gasturbinmotorkomponenter - Google Patents
Kylsystem for gasturbinmotorkomponenterInfo
- Publication number
- SE8406514L SE8406514L SE8406514A SE8406514A SE8406514L SE 8406514 L SE8406514 L SE 8406514L SE 8406514 A SE8406514 A SE 8406514A SE 8406514 A SE8406514 A SE 8406514A SE 8406514 L SE8406514 L SE 8406514L
- Authority
- SE
- Sweden
- Prior art keywords
- gas turbine
- fins
- front frame
- turbine engine
- cooling system
- Prior art date
Links
Classifications
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K7/00—Constructional details common to different types of electric apparatus
- H05K7/20—Modifications to facilitate cooling, ventilating, or heating
- H05K7/20009—Modifications to facilitate cooling, ventilating, or heating using a gaseous coolant in electronic enclosures
- H05K7/20136—Forced ventilation, e.g. by fans
- H05K7/20154—Heat dissipaters coupled to components
- H05K7/20163—Heat dissipaters coupled to components the components being isolated from air flow, e.g. hollow heat sinks, wind tunnels or funnels
-
- 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
- F01D17/00—Regulating or controlling by varying flow
- F01D17/02—Arrangement of sensing elements
-
- 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
-
- 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
- F02C7/16—Cooling of plants characterised by cooling medium
- F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
-
- 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
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
-
- 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)
- Microelectronics & Electronic Packaging (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/565,942 US4608819A (en) | 1983-12-27 | 1983-12-27 | Gas turbine engine component cooling system |
Publications (3)
Publication Number | Publication Date |
---|---|
SE8406514D0 SE8406514D0 (sv) | 1984-12-20 |
SE8406514L true SE8406514L (sv) | 1985-06-28 |
SE454008B SE454008B (sv) | 1988-03-21 |
Family
ID=24260745
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE8406514A SE454008B (sv) | 1983-12-27 | 1984-12-20 | System for att kyla en motorkomponent i en gasturbinmotor |
Country Status (8)
Country | Link |
---|---|
US (1) | US4608819A (sv) |
JP (1) | JPS60169632A (sv) |
CA (1) | CA1226446A (sv) |
DE (1) | DE3446205C2 (sv) |
FR (1) | FR2557204B1 (sv) |
GB (1) | GB2152147B (sv) |
IT (1) | IT1177449B (sv) |
SE (1) | SE454008B (sv) |
Families Citing this family (43)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB8526726D0 (en) * | 1985-10-30 | 1985-12-04 | Rolls Royce | Failsafe electronic control system |
IT1188101B (it) * | 1986-04-22 | 1987-12-30 | Weber Spa | Sistema di alloggiamento di una centralina elettronica per un motore endotermico |
US5123242A (en) * | 1990-07-30 | 1992-06-23 | General Electric Company | Precooling heat exchange arrangement integral with mounting structure fairing of gas turbine engine |
US5203163A (en) * | 1990-08-01 | 1993-04-20 | General Electric Company | Heat exchange arrangement in a gas turbine engine fan duct for cooling hot bleed air |
US5269135A (en) * | 1991-10-28 | 1993-12-14 | General Electric Company | Gas turbine engine fan cooled heat exchanger |
US5357742A (en) * | 1993-03-12 | 1994-10-25 | General Electric Company | Turbojet cooling system |
US5649418A (en) * | 1995-08-07 | 1997-07-22 | Solar Turbines Incorporated | Integrated power converter cooling system using turbine intake air |
US7941993B2 (en) * | 2003-10-14 | 2011-05-17 | Rolls-Royce Plc | Engine cooling |
GB0323993D0 (en) * | 2003-10-14 | 2003-11-19 | Rolls Royce Plc | Engine cooling |
EP1928734A4 (en) * | 2005-09-20 | 2012-03-28 | Volvo Aero Corp | COOLING SYSTEM FOR A PLANE, THE COOLING SYSTEM COMPRISING PLANE AND COOLING PROCESS |
US7779811B1 (en) * | 2006-09-13 | 2010-08-24 | General Electric Company | Thermoelectrically cooled components for distributed electronics control system for gas turbine engines |
US7665310B2 (en) * | 2006-12-27 | 2010-02-23 | General Electric Company | Gas turbine engine having a cooling-air nacelle-cowl duct integral with a nacelle cowl |
US7856824B2 (en) * | 2007-06-25 | 2010-12-28 | Honeywell International Inc. | Cooling systems for use on aircraft |
US20090064684A1 (en) * | 2007-07-13 | 2009-03-12 | United Technologies Corp. | Systems Involving Inlet-Mounted Engine Controls |
US7854547B2 (en) * | 2007-08-07 | 2010-12-21 | International Business Machines Corporation | Bidirectional and expandable heat flow measurement tool for units of air cooled electrical equipment |
US8123460B2 (en) * | 2008-07-23 | 2012-02-28 | Honeywell International Inc. | UAV pod cooling using integrated duct wall heat transfer |
US8197124B2 (en) * | 2009-02-05 | 2012-06-12 | International Business Machines Corporation | Heat flow measurement tool for a rack mounted assembly of electronic equipment |
US20100242492A1 (en) * | 2009-03-30 | 2010-09-30 | Honeywell International Inc. | Distributed engine control systems and gas turbine engines |
US8424285B2 (en) * | 2009-07-31 | 2013-04-23 | Hamilton Sundstrand Corporation | Cooling system for electronic device in a gas turbine engine system |
DE102010047054A1 (de) * | 2010-09-29 | 2011-09-15 | Eads Deutschland Gmbh | Verfahren und Vorrichtung zur Kühlung von elektronischen Bauteilen |
US9670842B2 (en) | 2011-01-14 | 2017-06-06 | Hamilton Sundstrand Corporation | Bleed valve module with position feedback and cooling shroud |
US10266034B2 (en) | 2011-06-16 | 2019-04-23 | Hamilton Sundstrand Corporation | Heat pump for supplemental heat |
GB2497809B (en) | 2011-12-22 | 2014-03-12 | Rolls Royce Plc | Method of servicing a gas turbine engine |
GB2497807B (en) | 2011-12-22 | 2014-09-10 | Rolls Royce Plc | Electrical harness |
US9478896B2 (en) | 2011-12-22 | 2016-10-25 | Rolls-Royce Plc | Electrical connectors |
GB2498006B (en) | 2011-12-22 | 2014-07-09 | Rolls Royce Plc | Gas turbine engine systems |
US9200570B2 (en) * | 2012-02-24 | 2015-12-01 | Pratt & Whitney Canada Corp. | Air-cooled oil cooler for turbofan engine |
FR2992796B1 (fr) * | 2012-07-02 | 2015-05-01 | Snecma | Dispositif de ventilation et d'alimentation electrique d'un calculateur de moteur d'aeronef |
WO2014051678A1 (en) | 2012-09-28 | 2014-04-03 | United Technologies Corporation | Gas turbine engine thermal management system for heat exchanger using bypass flow |
US20140208714A1 (en) * | 2012-12-19 | 2014-07-31 | United Technologies Corporation | Thermal Management for Gas Turbine Engine |
US9416730B2 (en) * | 2013-01-31 | 2016-08-16 | The Boeing Company | Bi-directional ventilation systems for use with aircraft and related methods |
JP2016531032A (ja) * | 2013-06-03 | 2016-10-06 | ユニゾン・インダストリーズ,エルエルシー | 航空機用共形表面熱交換器 |
FR3006996B1 (fr) * | 2013-06-14 | 2016-12-09 | European Aeronautic Defence & Space Co Eads France | Ensemble de propulsion electrique pour aeronef |
FR3019855B1 (fr) * | 2014-04-14 | 2016-04-01 | Airbus Operations Sas | Ensemble propulsif d'aeronef comprenant une vanne d'air a debit variable |
EP2942508B1 (en) * | 2014-05-08 | 2022-08-24 | Rolls-Royce North American Technologies, Inc. | Enhanced heat sink availability on gas turbine engines through the use of solid state heat pumps |
GB201503138D0 (en) | 2015-02-25 | 2015-04-08 | Rolls Royce Controls & Data Services Ltd | Icing prevention of a pressure sensing assembly |
FR3039134B1 (fr) * | 2015-07-22 | 2017-07-21 | Snecma | Aeronef avec un ensemble propulsif comprenant une soufflante a l'arriere du fuselage |
FR3048727B1 (fr) * | 2016-03-14 | 2018-03-02 | Safran Aircraft Engines | Conduit d'entree d'air pour une turbomachine d'aeronef |
FR3064700B1 (fr) | 2017-04-04 | 2019-06-21 | Safran Electrical & Power | Systeme de generation d'air comprenant un dispositif electromecanique, un boitier et une carte electronique |
US10934936B2 (en) * | 2017-07-10 | 2021-03-02 | Rolls-Royce North American Technologies, Inc. | Cooling system in a hybrid electric propulsion gas turbine engine for cooling electrical components therein |
US11134585B2 (en) * | 2019-05-31 | 2021-09-28 | Hamilton Sundstrand Corporation | Aircraft power electronic unit and method of cooling |
DE102019219573A1 (de) | 2019-12-13 | 2021-06-17 | Rolls-Royce Deutschland Ltd & Co Kg | Stromrichterkühlung in der Luftfahrt |
CN113027612B (zh) * | 2021-04-14 | 2022-05-17 | 中国航空发动机研究院 | 一种用于高速预冷发动机的换热器调节机构及发动机 |
Family Cites Families (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1019866B (de) * | 1940-06-24 | 1957-11-21 | Bayerische Motoren Werke Ag | Anordnung des Schmierstoffkuehlers eines mit einem die Arbeitsluft foerdernden Geblaese versehenen Strahltriebwerkes |
US2477798A (en) * | 1941-04-08 | 1949-08-02 | Rolls Royce | Contrarotating axial flow high and low pressure turbine and compressor with bladed duct with turbine cooling |
US2597822A (en) * | 1947-07-29 | 1952-05-20 | Rozen Joseph | Shutter for internal-combustion engines |
GB882788A (en) * | 1958-07-05 | 1961-11-22 | Reinold Hagen | Process and apparatus for manufacturing bottles and the like neck-provided articles from thermoplastic material |
US3011105A (en) * | 1958-12-30 | 1961-11-28 | le blanc | |
DE1145860B (de) * | 1960-09-24 | 1963-03-21 | Flugzeugwerft Veb | Kuehler, insbesondere fuer strahlgetriebene Flugzeuge |
US3253646A (en) * | 1964-04-08 | 1966-05-31 | Udylite Corp | Cooling system for power supply apparatus |
US3299946A (en) * | 1965-06-04 | 1967-01-24 | Scott Inc H H | Mounting and heat sink device for electrical components |
FR1504078A (fr) * | 1965-11-09 | 1967-12-01 | Plessey Co Ltd | Dispositif générateur d'électricité pour groupes énergétiques à turbine à gaz |
US3417575A (en) * | 1967-04-10 | 1968-12-24 | Barber Colman Co | Method of and means for cooling semiconductor devices |
US3416597A (en) * | 1967-06-15 | 1968-12-17 | Forbro Design Corp | Heat sink for forced air or convection cooling of semiconductors |
US3623546A (en) * | 1969-11-10 | 1971-11-30 | Avco Corp | Cooling system for an electronic assembly mounted on a gas turbine engine |
GB1358076A (en) * | 1971-06-19 | 1974-06-26 | Rolls Royce | Oil manifolds and coolers for ducted fan gas turbine engines |
US3780798A (en) * | 1972-10-30 | 1973-12-25 | Gte Automatic Electric Lab Inc | Air directing heat sink mounting of electrical components |
US3868625A (en) * | 1972-12-20 | 1975-02-25 | United Aircraft Corp | Surge indicator for turbine engines |
US4050093A (en) * | 1975-06-13 | 1977-09-20 | Chrysler Corporation | Housing for mounting electronic circuit boards on an engine air intake structure |
US4047379A (en) * | 1976-04-28 | 1977-09-13 | General Electric Company | Transient air temperature sensing system |
GB1516041A (en) * | 1977-02-14 | 1978-06-28 | Secr Defence | Multistage axial flow compressor stators |
US4254618A (en) * | 1977-08-18 | 1981-03-10 | General Electric Company | Cooling air cooler for a gas turbofan engine |
US4182119A (en) * | 1977-09-01 | 1980-01-08 | Avco Corporation | Air pump for turbofan fuel control system |
US4351150A (en) * | 1980-02-25 | 1982-09-28 | General Electric Company | Auxiliary air system for gas turbine engine |
GB2085234A (en) * | 1980-10-08 | 1982-04-21 | Clarion Co Ltd | Radiating device for power amplifier |
US4504030A (en) * | 1982-12-06 | 1985-03-12 | United Technologies Corporation | Cooling means |
-
1983
- 1983-12-27 US US06/565,942 patent/US4608819A/en not_active Expired - Lifetime
-
1984
- 1984-11-09 GB GB08428340A patent/GB2152147B/en not_active Expired
- 1984-12-14 FR FR8419141A patent/FR2557204B1/fr not_active Expired
- 1984-12-18 IT IT24116/84A patent/IT1177449B/it active
- 1984-12-19 DE DE3446205A patent/DE3446205C2/de not_active Expired - Lifetime
- 1984-12-20 SE SE8406514A patent/SE454008B/sv not_active IP Right Cessation
- 1984-12-20 CA CA000470750A patent/CA1226446A/en not_active Expired
- 1984-12-26 JP JP59273529A patent/JPS60169632A/ja active Granted
Also Published As
Publication number | Publication date |
---|---|
DE3446205A1 (de) | 1985-07-11 |
FR2557204A1 (fr) | 1985-06-28 |
GB2152147B (en) | 1988-08-03 |
DE3446205C2 (de) | 1998-04-23 |
SE8406514D0 (sv) | 1984-12-20 |
JPH0413528B2 (sv) | 1992-03-10 |
FR2557204B1 (fr) | 1987-08-07 |
IT1177449B (it) | 1987-08-26 |
GB8428340D0 (en) | 1984-12-19 |
JPS60169632A (ja) | 1985-09-03 |
GB2152147A (en) | 1985-07-31 |
CA1226446A (en) | 1987-09-08 |
US4608819A (en) | 1986-09-02 |
IT8424116A0 (it) | 1984-12-18 |
SE454008B (sv) | 1988-03-21 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
NUG | Patent has lapsed |
Ref document number: 8406514-3 Effective date: 19891128 Format of ref document f/p: F |