IT1096411B - Turbomotore a gas e mezzi per raffreddare il medesimo - Google Patents
Turbomotore a gas e mezzi per raffreddare il medesimoInfo
- Publication number
- IT1096411B IT1096411B IT24102/78A IT2410278A IT1096411B IT 1096411 B IT1096411 B IT 1096411B IT 24102/78 A IT24102/78 A IT 24102/78A IT 2410278 A IT2410278 A IT 2410278A IT 1096411 B IT1096411 B IT 1096411B
- Authority
- IT
- Italy
- Prior art keywords
- turbomotor
- cool
- vehicles
- gas
- same
- Prior art date
Links
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
- F02C7/16—Cooling of plants characterised by cooling medium
-
- 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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
-
- 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
-
- 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)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/803,167 US4190398A (en) | 1977-06-03 | 1977-06-03 | Gas turbine engine and means for cooling same |
Publications (2)
Publication Number | Publication Date |
---|---|
IT7824102A0 IT7824102A0 (it) | 1978-06-01 |
IT1096411B true IT1096411B (it) | 1985-08-26 |
Family
ID=25185757
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT24102/78A IT1096411B (it) | 1977-06-03 | 1978-06-01 | Turbomotore a gas e mezzi per raffreddare il medesimo |
Country Status (5)
Country | Link |
---|---|
US (1) | US4190398A (it) |
JP (1) | JPS5413809A (it) |
DE (1) | DE2823956A1 (it) |
FR (1) | FR2393151A1 (it) |
IT (1) | IT1096411B (it) |
Families Citing this family (53)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS55133997A (en) * | 1979-11-17 | 1980-10-18 | Yoshio Midorikawa | Capillary body |
JPS55130798A (en) * | 1979-11-17 | 1980-10-09 | Yoshio Midorikawa | Autographing pen |
JPS576580U (it) * | 1980-06-13 | 1982-01-13 | ||
GB2252368B (en) * | 1981-03-20 | 1993-02-17 | Rolls Royce | Liquid cooled aerofoil blade |
GB2254379B (en) * | 1981-04-28 | 1993-04-14 | Rolls Royce | Cooled aerofoil blade |
CA1235583A (en) * | 1983-06-20 | 1988-04-26 | Marius A. Paul | Processes of intensification of the thermoenergetical cycle and air jet propulsion engines |
US5177954A (en) * | 1984-10-10 | 1993-01-12 | Paul Marius A | Gas turbine engine with cooled turbine blades |
US5003766A (en) * | 1984-10-10 | 1991-04-02 | Paul Marius A | Gas turbine engine |
US4824327A (en) * | 1987-12-15 | 1989-04-25 | United Technologies Corporation | Gas turbine engine oil drain slot |
US5122033A (en) * | 1990-11-16 | 1992-06-16 | Paul Marius A | Turbine blade unit |
US5271711A (en) * | 1992-05-11 | 1993-12-21 | General Electric Company | Compressor bore cooling manifold |
US5318404A (en) * | 1992-12-30 | 1994-06-07 | General Electric Company | Steam transfer arrangement for turbine bucket cooling |
KR100389990B1 (ko) * | 1995-04-06 | 2003-11-17 | 가부시끼가이샤 히다치 세이사꾸쇼 | 가스터빈 |
US5782076A (en) * | 1996-05-17 | 1998-07-21 | Westinghouse Electric Corporation | Closed loop air cooling system for combustion turbines |
JPH10238301A (ja) * | 1997-02-21 | 1998-09-08 | Mitsubishi Heavy Ind Ltd | ガスタービン翼の冷却通路 |
US6014855A (en) * | 1997-04-30 | 2000-01-18 | Stewart & Stevenson Services, Inc. | Light hydrocarbon fuel cooling system for gas turbine |
US6185924B1 (en) | 1997-10-17 | 2001-02-13 | Hitachi, Ltd. | Gas turbine with turbine blade cooling |
DE60026236T2 (de) * | 1999-08-24 | 2006-11-23 | General Electric Co. | Dampfkühlungssystem für eine Gasturbine |
GB2365930B (en) * | 2000-08-12 | 2004-12-08 | Rolls Royce Plc | A turbine blade support assembly and a turbine assembly |
US6481211B1 (en) | 2000-11-06 | 2002-11-19 | Joel C. Haas | Turbine engine cycling thermo-mechanical stress control |
US6565312B1 (en) | 2001-12-19 | 2003-05-20 | The Boeing Company | Fluid-cooled turbine blades |
DE10303088B4 (de) * | 2002-02-09 | 2015-08-20 | Alstom Technology Ltd. | Abgasgehäuse einer Wärmekraftmaschine |
US6699015B2 (en) * | 2002-02-19 | 2004-03-02 | The Boeing Company | Blades having coolant channels lined with a shape memory alloy and an associated fabrication method |
GB2389174B (en) * | 2002-05-01 | 2005-10-26 | Rolls Royce Plc | Cooling systems |
US6672075B1 (en) * | 2002-07-18 | 2004-01-06 | University Of Maryland | Liquid cooling system for gas turbines |
US6910852B2 (en) * | 2003-09-05 | 2005-06-28 | General Electric Company | Methods and apparatus for cooling gas turbine engine rotor assemblies |
US6988367B2 (en) | 2004-04-20 | 2006-01-24 | Williams International Co. L.L.C. | Gas turbine engine cooling system and method |
EP1875058A4 (en) * | 2005-04-25 | 2011-03-30 | Williams Int Co Llc | SYSTEM AND METHOD FOR COOLING A GAS TURBINE ENGINE |
US10180074B2 (en) * | 2005-12-16 | 2019-01-15 | Mehmet Arik | Wireless monitoring system |
US8387362B2 (en) * | 2006-10-19 | 2013-03-05 | Michael Ralph Storage | Method and apparatus for operating gas turbine engine heat exchangers |
US8215895B2 (en) * | 2008-03-03 | 2012-07-10 | Rolls-Royce Corporation | Vapor phase lubrication system |
US9464527B2 (en) | 2008-04-09 | 2016-10-11 | Williams International Co., Llc | Fuel-cooled bladed rotor of a gas turbine engine |
WO2009126847A1 (en) * | 2008-04-09 | 2009-10-15 | Williams International Co., L.L.C. | Gas turbine engine cooling system and method |
US8627667B2 (en) * | 2008-12-29 | 2014-01-14 | Roll-Royce Corporation | Gas turbine engine duct having a coupled fluid volume |
US20110232298A1 (en) * | 2010-03-23 | 2011-09-29 | General Electric Company | System and method for cooling gas turbine components |
US9279340B2 (en) | 2010-03-23 | 2016-03-08 | General Electric Company | System and method for cooling gas turbine components |
US9353687B1 (en) * | 2012-10-18 | 2016-05-31 | Florida Turbine Technologies, Inc. | Gas turbine engine with liquid metal cooling |
US9677421B2 (en) | 2012-10-24 | 2017-06-13 | United Technologies Corporation | Gas turbine engine rotor drain feature |
FR3013766B1 (fr) * | 2013-11-25 | 2017-11-10 | Snecma | Turbomachine comprenant un fourreau d'arbre et tube de fourreau associe |
WO2015103751A1 (en) * | 2014-01-09 | 2015-07-16 | General Electric Company | Vibration damping assembly for a piping unit |
US10280792B2 (en) | 2014-02-21 | 2019-05-07 | United Technologies Corporation | Bore basket for a gas powered turbine |
EP2910735B1 (en) * | 2014-02-21 | 2020-07-01 | United Technologies Corporation | Bore basket for a gas powered turbine |
US9382801B2 (en) | 2014-02-26 | 2016-07-05 | General Electric Company | Method for removing a rotor bucket from a turbomachine rotor wheel |
GB2518715A (en) * | 2014-07-14 | 2015-04-01 | Michael Victor Rodrigues | Jet engine turbine & compressor bolted blades |
US10697371B2 (en) * | 2015-12-28 | 2020-06-30 | General Electric Company | Method and system for a combined air-oil cooler and fuel-oil cooler heat exchanger |
US10260523B2 (en) | 2016-04-06 | 2019-04-16 | Rolls-Royce North American Technologies Inc. | Fluid cooling system integrated with outlet guide vane |
US10041400B2 (en) | 2016-05-20 | 2018-08-07 | Borgwarner Inc. | Hollow filled turbocharger rotor shaft |
FR3054263B1 (fr) * | 2016-07-20 | 2018-08-10 | Safran Aircraft Engines | Carter intermediaire de turbomachine d'aeronef realise d'une seule piece de fonderie avec une canalisation de lubrifiant |
US10428660B2 (en) * | 2017-01-31 | 2019-10-01 | United Technologies Corporation | Hybrid airfoil cooling |
CN106870160B (zh) * | 2017-04-09 | 2018-02-23 | 中国科学院工程热物理研究所 | 一种发动机热端结构 |
CN110318878B (zh) * | 2019-06-13 | 2022-08-09 | 内蒙动力机械研究所 | 基于磁流体能量旁路的空天飞机主动冷却系统 |
US11459909B2 (en) * | 2020-09-15 | 2022-10-04 | Pratt & Whitney Canada Corp. | Rotating heat exchanger |
CN114961868B (zh) * | 2022-06-06 | 2023-08-22 | 中国人民解放军总参谋部第六十研究所 | 一种带芯部冷却结构的微小型涡喷发动机热端转子系统 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2675671A (en) * | 1954-04-20 | Malgieri | ||
US2659529A (en) * | 1945-06-02 | 1953-11-17 | Lockheed Aircraft Corp | Cooling means for the rotors of gas turbine power plants |
US2868500A (en) * | 1949-02-15 | 1959-01-13 | Boulet George | Cooling of blades in machines where blading is employed |
US2595822A (en) * | 1949-10-25 | 1952-05-06 | Young Radiator Co | Spring seal for tube and shell heat exchangers |
CH301140A (de) * | 1951-05-28 | 1954-08-31 | Simmering Graz Pauker Ag | Gasturbinenanlage. |
US2778601A (en) * | 1951-05-28 | 1957-01-22 | Ernst R G Eckert | Fluid cooled turbine blade construction |
US2849210A (en) * | 1953-01-19 | 1958-08-26 | Gen Motors Corp | Turbine blade cooling system |
US2883151A (en) * | 1954-01-26 | 1959-04-21 | Curtiss Wright Corp | Turbine cooling system |
GB997260A (en) * | 1964-05-08 | 1965-07-07 | Rolls Royce | Gas turbine engine fuel heating and oil cooling system |
US3756020A (en) * | 1972-06-26 | 1973-09-04 | Curtiss Wright Corp | Gas turbine engine and cooling system therefor |
US4041697A (en) * | 1975-07-17 | 1977-08-16 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Oil cooling system for a gas turbine engine |
-
1977
- 1977-06-03 US US05/803,167 patent/US4190398A/en not_active Expired - Lifetime
-
1978
- 1978-06-01 IT IT24102/78A patent/IT1096411B/it active
- 1978-06-01 DE DE19782823956 patent/DE2823956A1/de not_active Withdrawn
- 1978-06-01 JP JP6497478A patent/JPS5413809A/ja active Pending
- 1978-06-02 FR FR7816597A patent/FR2393151A1/fr not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
FR2393151A1 (fr) | 1978-12-29 |
DE2823956A1 (de) | 1978-12-07 |
JPS5413809A (en) | 1979-02-01 |
US4190398A (en) | 1980-02-26 |
IT7824102A0 (it) | 1978-06-01 |
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