GB1195987A - Improvements in Fuel Control System for Gas Turbine Engines. - Google Patents
Improvements in Fuel Control System for Gas Turbine Engines.Info
- Publication number
- GB1195987A GB1195987A GB52466/67A GB5246667A GB1195987A GB 1195987 A GB1195987 A GB 1195987A GB 52466/67 A GB52466/67 A GB 52466/67A GB 5246667 A GB5246667 A GB 5246667A GB 1195987 A GB1195987 A GB 1195987A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fuel
- valve
- flow
- reheat
- piston
- 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
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
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/16—Control of working fluid flow
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
- F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
-
- 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)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Feeding And Controlling Fuel (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US618429A US3402556A (en) | 1967-02-24 | 1967-02-24 | Fuel control systems for gas turbine engines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1195987A true GB1195987A (en) | 1970-06-24 |
Family
ID=24477629
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB52466/67A Expired GB1195987A (en) | 1967-02-24 | 1967-11-17 | Improvements in Fuel Control System for Gas Turbine Engines. |
Country Status (4)
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2511374A (en) * | 2011-01-07 | 2014-09-03 | Honeywell Int Inc | System and method for controlling a gas turbine engine afterburner |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE755269A (fr) * | 1969-08-25 | 1971-02-01 | Westinghouse Electric Corp | Systeme de regulation d'epaisseur du produit lamine sortant d'un laminoir |
US4244183A (en) * | 1978-04-27 | 1981-01-13 | United Technologies Corporation | Control means for an augmentor for a gas turbine engine |
FR2732407B1 (fr) * | 1995-03-29 | 1997-04-30 | Snecma | Procede pour eviter les instabilites dues a la combustion dans un turboreacteur |
CN102979630B (zh) * | 2012-12-12 | 2014-10-08 | 北京动力机械研究所 | 基于模块化能量控制的燃气轮机控制系统 |
CN105631110B (zh) * | 2015-12-25 | 2019-04-23 | 潍柴动力扬州柴油机有限责任公司 | 一种活塞冷却喷嘴关键结构参数的设计方法 |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3011308A (en) * | 1956-01-04 | 1961-12-05 | Thompson Ramo Wooldridge Inc | Fuel and afterburner pump system |
US2987877A (en) * | 1956-12-12 | 1961-06-13 | United Aircraft Corp | Coordinated control of afterburner fuel supply and exhaust nozzle area in a multispool gas turbine power plant |
US3086581A (en) * | 1960-01-08 | 1963-04-23 | Orenda Engines Ltd | Fuel pumping systems for aircraft engines |
-
1967
- 1967-02-24 US US618429A patent/US3402556A/en not_active Expired - Lifetime
- 1967-11-17 GB GB52466/67A patent/GB1195987A/en not_active Expired
- 1967-11-20 DE DE19671601572 patent/DE1601572A1/de active Pending
- 1967-11-23 BE BE706960D patent/BE706960A/xx unknown
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2511374A (en) * | 2011-01-07 | 2014-09-03 | Honeywell Int Inc | System and method for controlling a gas turbine engine afterburner |
GB2511374B (en) * | 2011-01-07 | 2014-12-24 | Honeywell Int Inc | System and method for controlling a gas turbine engine afterburner |
Also Published As
Publication number | Publication date |
---|---|
BE706960A (US20090163788A1-20090625-C00002.png) | 1968-04-01 |
DE1601572A1 (de) | 1970-04-09 |
US3402556A (en) | 1968-09-24 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PLNP | Patent lapsed through nonpayment of renewal fees |