CA2473033A1 - Methode d'amelioration de l'efficacite d'une turbine a gaz combustible par le refroidissement de l'air de combustion - Google Patents
Methode d'amelioration de l'efficacite d'une turbine a gaz combustible par le refroidissement de l'air de combustion Download PDFInfo
- Publication number
- CA2473033A1 CA2473033A1 CA 2473033 CA2473033A CA2473033A1 CA 2473033 A1 CA2473033 A1 CA 2473033A1 CA 2473033 CA2473033 CA 2473033 CA 2473033 A CA2473033 A CA 2473033A CA 2473033 A1 CA2473033 A1 CA 2473033A1
- Authority
- CA
- Canada
- Prior art keywords
- fuel gas
- fluid path
- combustion air
- gas turbine
- temperature
- 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.)
- Abandoned
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
- F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
- F02C7/141—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid
- F02C7/143—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid before or between the compressor stages
-
- 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
- F02C7/185—Cooling means for reducing the temperature of the cooling air or gas
-
- 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
- F02C7/22—Fuel supply systems
- F02C7/224—Heating fuel before feeding to the burner
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA 2473033 CA2473033A1 (fr) | 2004-06-30 | 2004-06-30 | Methode d'amelioration de l'efficacite d'une turbine a gaz combustible par le refroidissement de l'air de combustion |
PCT/CA2005/000996 WO2006002523A1 (fr) | 2004-06-30 | 2005-06-30 | Procede permettant d'augmenter l'efficacite d'une turbine a gaz combustible par refroidissement de l'air de combustion |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA 2473033 CA2473033A1 (fr) | 2004-06-30 | 2004-06-30 | Methode d'amelioration de l'efficacite d'une turbine a gaz combustible par le refroidissement de l'air de combustion |
Publications (1)
Publication Number | Publication Date |
---|---|
CA2473033A1 true CA2473033A1 (fr) | 2005-12-30 |
Family
ID=35589019
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA 2473033 Abandoned CA2473033A1 (fr) | 2004-06-30 | 2004-06-30 | Methode d'amelioration de l'efficacite d'une turbine a gaz combustible par le refroidissement de l'air de combustion |
Country Status (2)
Country | Link |
---|---|
CA (1) | CA2473033A1 (fr) |
WO (1) | WO2006002523A1 (fr) |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2718753A (en) * | 1951-01-02 | 1955-09-27 | Phillips Petroleum Co | Improved operation of internal combustion engine operating on liquid petroleum gas fuel |
US4104873A (en) * | 1976-11-29 | 1978-08-08 | The United States Of America As Represented By The Administrator Of The United States National Aeronautics And Space Administration | Fuel delivery system including heat exchanger means |
US5095693A (en) * | 1989-08-04 | 1992-03-17 | United Technologies Corporation | High-efficiency gas turbine engine |
JP3499258B2 (ja) * | 1992-10-16 | 2004-02-23 | 株式会社神戸製鋼所 | 液化天然ガスを燃料として用いるガスタービンの運転方法およびガスタービン機構 |
-
2004
- 2004-06-30 CA CA 2473033 patent/CA2473033A1/fr not_active Abandoned
-
2005
- 2005-06-30 WO PCT/CA2005/000996 patent/WO2006002523A1/fr active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2006002523A1 (fr) | 2006-01-12 |
WO2006002523B1 (fr) | 2006-03-02 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP5154822B2 (ja) | ガスタービン吸気調整システム及び方法 | |
US5622044A (en) | Apparatus for augmenting power produced from gas turbines | |
JP6571491B2 (ja) | ヒートポンプ | |
KR100874508B1 (ko) | 개스 터빈용 과급 시스템 | |
US6332321B1 (en) | Apparatus for augmenting power produced from gas turbines | |
WO2001000975A1 (fr) | Systeme de suralimentation pour turbines a gaz | |
CA2589781A1 (fr) | Procede et appareil de production d'energie avec chaleur residuelle | |
WO2008091502A2 (fr) | Augmentation de puissance de turbines à combustion par injection d'air froid en amont du compresseur | |
JP6621348B2 (ja) | 圧縮空気貯蔵発電装置 | |
JP6913044B2 (ja) | 圧縮空気貯蔵発電装置 | |
JP7134688B2 (ja) | 蓄熱システムを備えた中間冷却式タービン | |
KR20120026569A (ko) | 흡기 온도 조절 장치 및 그의 작동 방법 | |
US6119445A (en) | Method of and apparatus for augmenting power produced from gas turbines | |
JP5651366B2 (ja) | 空気圧縮機排熱回収システム | |
JP6689616B2 (ja) | 圧縮空気貯蔵発電装置および圧縮空気貯蔵発電方法 | |
US11092075B2 (en) | High-capacity electric energy storage system for gas turbine based power plants | |
CA2473033A1 (fr) | Methode d'amelioration de l'efficacite d'une turbine a gaz combustible par le refroidissement de l'air de combustion | |
WO2006002523A9 (fr) | Procede permettant d'augmenter l'efficacite d'une turbine a gaz combustible par refroidissement de l'air de combustion | |
Alfani et al. | Sizing Criteria and Performance Evaluation of Direct Air Cooled Heat Rejection Units for Supercritical CO2 Power Plants | |
KR20170117663A (ko) | 스크류 압축기의 공기열 및 오일열 회수 일체형 온수 발생기 | |
US20030070432A1 (en) | Natural gas depressurization temperature maintenance expansion system with production of useful work | |
JP6906013B2 (ja) | ヒートポンプ | |
US11808205B2 (en) | Turbine inlet air cooling systems with condensate water recovery | |
CN117365916A (zh) | 一种配置斜温层储罐的压缩空气储能系统 | |
JP2019019812A (ja) | 膨張機及び圧縮空気システム |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
FZDE | Dead |