GB695048A - Liquid fuel combustion apparatus - Google Patents
Liquid fuel combustion apparatusInfo
- Publication number
- GB695048A GB695048A GB481951A GB481951A GB695048A GB 695048 A GB695048 A GB 695048A GB 481951 A GB481951 A GB 481951A GB 481951 A GB481951 A GB 481951A GB 695048 A GB695048 A GB 695048A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fuel
- chamber
- spring
- capsule
- claw
- 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
- 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
- F02C7/26—Starting; Ignition
- F02C7/264—Ignition
-
- 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
- F02C7/26—Starting; Ignition
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Abstract
695,048. Generating combustion products under pressure. LUCAS (INDUSTRIES), Ltd., J. Feb. 8, 1952 [Feb. 28, 1951], No. 4819/51. Class 51(i) [Also in Group XXVI] Combustion apparatus for burning a liquid fuel such as propyl nitrate and supplying motive gas to an engine starting or other turbine comprises a fuel chamber of stepped cylindrical form having a valve controlled inlet, a combustion chamber at or in communication with the larger end of the fuel chamber; a stepped hollow piston in the fuel chamber carrying a spring loaded capsule or piston, means for compressing the spring and a fuel injection nozzle through which the fuel from the fuel chamber can be discharged into the combustion chamber. The stepped cylindrical chamber b is supplied with fuel from a tank c through a valve d. A combustion chamber e with an outlet f and scavenging valve g is situated at the larger end of the fuel chamber. A hollow stepped piston h which is open to the fuel chamber at its smaller end carries an elastic capsule i loaded by a spring j and has a passage k through which fuel is discharged through nozzle m. A slidable ram n which may be electrically operated by a solenoid is provided for compressing the capsule i and spring j. The capsule and spring are returned in the compressed condition by a claw p engaging a stem q. The claw p may be released by the core r of a solenoid s. The capsule i and spring are first compressed by the ram n and retained compressed by the claw p. After the fuel chamber b is filled with fuel the valve d is closed and the claw p released. This causes fuel to be displaced from the fuel chamber to the combustion chamber through the nozzle m. Ignition of this fuel in the combustion chamber forces the stepped piston upwards and causes more fuel to be displaced. The rate of movement of the stepped piston is controlled by the air vent u.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB481951A GB695048A (en) | 1951-02-28 | 1951-02-28 | Liquid fuel combustion apparatus |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB481951A GB695048A (en) | 1951-02-28 | 1951-02-28 | Liquid fuel combustion apparatus |
Publications (1)
Publication Number | Publication Date |
---|---|
GB695048A true GB695048A (en) | 1953-08-05 |
Family
ID=9784398
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB481951A Expired GB695048A (en) | 1951-02-28 | 1951-02-28 | Liquid fuel combustion apparatus |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB695048A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2822667A (en) * | 1954-02-03 | 1958-02-11 | Garrett Corp | Propellant feed system |
US2918791A (en) * | 1956-08-20 | 1959-12-29 | Experiment Inc | Differential area piston pumping system |
US3023573A (en) * | 1959-03-23 | 1962-03-06 | Atlantic Res Corp | Rocket motor with fuel extrusion means |
US3067575A (en) * | 1959-01-02 | 1962-12-11 | Thompson Ramo Wooldridge Inc | Disposable rocket motor |
US3115007A (en) * | 1958-09-22 | 1963-12-24 | Phillips Petroleum Co | Self-actuating hybrid rocket motor |
US3680310A (en) * | 1967-05-19 | 1972-08-01 | Us Navy | Starting device for monopropellant gas generator |
DE3001270A1 (en) * | 1979-01-15 | 1980-07-24 | Rockwell International Corp | ROCKET ENGINE |
-
1951
- 1951-02-28 GB GB481951A patent/GB695048A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2822667A (en) * | 1954-02-03 | 1958-02-11 | Garrett Corp | Propellant feed system |
US2918791A (en) * | 1956-08-20 | 1959-12-29 | Experiment Inc | Differential area piston pumping system |
US3115007A (en) * | 1958-09-22 | 1963-12-24 | Phillips Petroleum Co | Self-actuating hybrid rocket motor |
US3067575A (en) * | 1959-01-02 | 1962-12-11 | Thompson Ramo Wooldridge Inc | Disposable rocket motor |
US3023573A (en) * | 1959-03-23 | 1962-03-06 | Atlantic Res Corp | Rocket motor with fuel extrusion means |
US3680310A (en) * | 1967-05-19 | 1972-08-01 | Us Navy | Starting device for monopropellant gas generator |
DE3001270A1 (en) * | 1979-01-15 | 1980-07-24 | Rockwell International Corp | ROCKET ENGINE |
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