GB0921958D0 - Fuel injector - Google Patents
Fuel injectorInfo
- Publication number
- GB0921958D0 GB0921958D0 GBGB0921958.5A GB0921958A GB0921958D0 GB 0921958 D0 GB0921958 D0 GB 0921958D0 GB 0921958 A GB0921958 A GB 0921958A GB 0921958 D0 GB0921958 D0 GB 0921958D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- fuel injector
- injector
- fuel
- 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.)
- Withdrawn
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D15/00—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
- F28D15/02—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes
- F28D15/04—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes with tubes having a capillary structure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/36—Details, e.g. burner cooling means, noise reduction means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/46—Details, e.g. noise reduction means
- F23D14/72—Safety devices, e.g. operative in case of failure of gas supply
- F23D14/78—Cooling burner parts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D15/00—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
- F28D15/02—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2214/00—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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E20/00—Combustion technologies with mitigation potential
- Y02E20/30—Technologies for a more efficient combustion or heat usage
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0921958A GB2476253A (en) | 2009-12-17 | 2009-12-17 | Fuel Injector Cooled by a Heat Pipe |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0921958A GB2476253A (en) | 2009-12-17 | 2009-12-17 | Fuel Injector Cooled by a Heat Pipe |
Publications (2)
Publication Number | Publication Date |
---|---|
GB0921958D0 true GB0921958D0 (en) | 2010-02-03 |
GB2476253A GB2476253A (en) | 2011-06-22 |
Family
ID=41717026
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0921958A Withdrawn GB2476253A (en) | 2009-12-17 | 2009-12-17 | Fuel Injector Cooled by a Heat Pipe |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2476253A (en) |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2971684B1 (en) * | 2013-03-14 | 2018-07-18 | United Technologies Corporation | Hollow-wall heat shield for fuel injector component |
DE102013014988A1 (en) * | 2013-09-07 | 2015-03-26 | Messer Austria Gmbh | burner |
US10660236B2 (en) | 2014-04-08 | 2020-05-19 | General Electric Company | Systems and methods for using additive manufacturing for thermal management |
CN105202577B (en) * | 2014-06-25 | 2017-10-20 | 中国航发商用航空发动机有限责任公司 | Fuel nozzle and combustion chamber |
US10356945B2 (en) | 2015-01-08 | 2019-07-16 | General Electric Company | System and method for thermal management using vapor chamber |
US9909448B2 (en) | 2015-04-15 | 2018-03-06 | General Electric Company | Gas turbine engine component with integrated heat pipe |
US10830150B2 (en) | 2016-01-28 | 2020-11-10 | Rolls-Royce Corporation | Fuel heat exchanger with leak management |
CA2955613A1 (en) * | 2016-01-28 | 2017-07-28 | Rolls-Royce North American Technologies, Inc. | Heat exchanger integrated with fuel nozzle |
US11118784B2 (en) | 2016-01-28 | 2021-09-14 | Rolls-Royce North American Technologies Inc. | Heat exchanger integrated with fuel nozzle |
US10458331B2 (en) * | 2016-06-20 | 2019-10-29 | United Technologies Corporation | Fuel injector with heat pipe cooling |
US10209009B2 (en) | 2016-06-21 | 2019-02-19 | General Electric Company | Heat exchanger including passageways |
US11073282B2 (en) * | 2017-08-25 | 2021-07-27 | Delavan Inc. | Gas turbine combustion liner comprising heat transfer cell heat pipes |
US10775046B2 (en) | 2017-10-18 | 2020-09-15 | Rolls-Royce North American Technologies Inc. | Fuel injection assembly for gas turbine engine |
US11260976B2 (en) | 2019-11-15 | 2022-03-01 | General Electric Company | System for reducing thermal stresses in a leading edge of a high speed vehicle |
US11427330B2 (en) | 2019-11-15 | 2022-08-30 | General Electric Company | System and method for cooling a leading edge of a high speed vehicle |
US11352120B2 (en) | 2019-11-15 | 2022-06-07 | General Electric Company | System and method for cooling a leading edge of a high speed vehicle |
US11260953B2 (en) | 2019-11-15 | 2022-03-01 | General Electric Company | System and method for cooling a leading edge of a high speed vehicle |
US11267551B2 (en) | 2019-11-15 | 2022-03-08 | General Electric Company | System and method for cooling a leading edge of a high speed vehicle |
FR3106373B1 (en) * | 2020-01-20 | 2021-12-10 | Safran Aircraft Engines | INJECTOR FOR A TURBOMACHINE |
US11745847B2 (en) | 2020-12-08 | 2023-09-05 | General Electric Company | System and method for cooling a leading edge of a high speed vehicle |
US11407488B2 (en) | 2020-12-14 | 2022-08-09 | General Electric Company | System and method for cooling a leading edge of a high speed vehicle |
US11577817B2 (en) | 2021-02-11 | 2023-02-14 | General Electric Company | System and method for cooling a leading edge of a high speed vehicle |
US11519332B1 (en) | 2021-05-11 | 2022-12-06 | Rolls-Royce North American Technologies Inc. | Fuel injector with integrated heat exchanger for use in gas turbine engines |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4052144A (en) * | 1976-03-31 | 1977-10-04 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Fuel combustor |
CA1195187A (en) * | 1981-11-04 | 1985-10-15 | Cornelius R. Russell | Nozzle cooled by heat pipe means |
US4736693A (en) * | 1987-07-31 | 1988-04-12 | Shell Oil Company | Partial combustion burner with heat pipe-cooled face |
US7900438B2 (en) * | 2006-07-28 | 2011-03-08 | General Electric Company | Heat transfer system and method for turbine engine using heat pipes |
-
2009
- 2009-12-17 GB GB0921958A patent/GB2476253A/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
GB2476253A (en) | 2011-06-22 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |