BE660204A - - Google Patents
Info
- Publication number
- BE660204A BE660204A BE660204DA BE660204A BE 660204 A BE660204 A BE 660204A BE 660204D A BE660204D A BE 660204DA BE 660204 A BE660204 A BE 660204A
- Authority
- BE
- Belgium
Links
Classifications
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
- F16K31/00—Actuating devices; Operating means; Releasing devices
- F16K31/12—Actuating devices; Operating means; Releasing devices actuated by fluid
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Feeding And Controlling Fuel (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US347818A US3270500A (en) | 1964-02-27 | 1964-02-27 | Afterburner fuel control |
Publications (1)
Publication Number | Publication Date |
---|---|
BE660204A true BE660204A (en) | 1965-06-16 |
Family
ID=23365408
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE660204D BE660204A (en) | 1964-02-27 | 1965-02-24 |
Country Status (4)
Country | Link |
---|---|
US (1) | US3270500A (en) |
BE (1) | BE660204A (en) |
DE (1) | DE1300354B (en) |
GB (1) | GB1029603A (en) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3595021A (en) * | 1968-10-10 | 1971-07-27 | Snecma | Fuel feed system for reheat-combustion in gas turbine power plants |
GB2202904B (en) * | 1987-03-23 | 1991-09-11 | Rolls Royce Plc | A method and apparatus for evaluating the working line characteristics of a compressor of a gas turbine engine |
US4973026A (en) * | 1988-08-01 | 1990-11-27 | Saurwein Albert C | High pressure water jet cutting nozzle on-off valve |
US5020314A (en) * | 1989-06-19 | 1991-06-04 | Williams International Corporation | Multiple fluid speed systems |
EP1909077A1 (en) * | 2006-10-02 | 2008-04-09 | Syngeta Participations AG | Liquid dispensing device |
US9316157B2 (en) * | 2012-02-01 | 2016-04-19 | Hamilton Sundstrand Corporation | Fuel system for starting an APU using a hybrid pump arrangement |
CN103832427B (en) * | 2014-03-18 | 2016-09-14 | 深圳嘉贸气动器材有限公司 | A kind of automobile-used Pneumatic controller |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2640316A (en) * | 1949-11-07 | 1953-06-02 | Westinghouse Electric Corp | Ignition apparatus for turbojet afterburners |
CH290429A (en) * | 1949-11-14 | 1953-04-30 | Rolls Royce | Post-heating fuel supply device in gas turbine systems. |
US2804241A (en) * | 1951-09-15 | 1957-08-27 | Gen Motors Corp | Flow control meter |
US2829489A (en) * | 1952-11-15 | 1958-04-08 | United Aircraft Corp | Repeating cycle igniter control |
DE1045733B (en) * | 1954-08-31 | 1958-12-04 | United Aircraft Corp | Automatic control system of the flame ignition device for after-burners of turbine jet engines |
US3019598A (en) * | 1958-07-23 | 1962-02-06 | Gen Motors Corp | Afterburner fuel igniter |
GB864392A (en) * | 1958-11-10 | 1961-04-06 | Rexall Drug Company Ltd | Improvements in or relating to dispensing devices for aerosols |
US3062005A (en) * | 1959-08-26 | 1962-11-06 | Rolls Royce | Coordinated variable area nozzle and reheat fuel control for a gas turbine engine |
GB928018A (en) * | 1960-11-15 | 1963-06-06 | Rolls Royce | Reheat apparatus for a gas turbine engine |
-
1964
- 1964-02-27 US US347818A patent/US3270500A/en not_active Expired - Lifetime
-
1965
- 1965-02-23 DE DEG42914A patent/DE1300354B/en not_active Withdrawn
- 1965-02-24 BE BE660204D patent/BE660204A/xx unknown
- 1965-02-25 GB GB8132/65A patent/GB1029603A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB1029603A (en) | 1966-05-18 |
DE1300354B (en) | 1969-07-31 |
US3270500A (en) | 1966-09-06 |