GB695048A - Liquid fuel combustion apparatus - Google Patents

Liquid fuel combustion apparatus

Info

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
Application number
GB481951A
Inventor
William Fleming
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
ZF International UK Ltd
Original Assignee
Lucas Industries Ltd
Joseph Lucas Industries Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Lucas Industries Ltd, Joseph Lucas Industries Ltd filed Critical Lucas Industries Ltd
Priority to GB481951A priority Critical patent/GB695048A/en
Publication of GB695048A publication Critical patent/GB695048A/en
Expired legal-status Critical Current

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.
GB481951A 1951-02-28 1951-02-28 Liquid fuel combustion apparatus Expired GB695048A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (7)

* Cited by examiner, † Cited by third party
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

Similar Documents

Publication Publication Date Title
GB424955A (en) Apparatus for producing a compressed gaseous medium by combustion
GB1265081A (en)
GB695048A (en) Liquid fuel combustion apparatus
US2838034A (en) Monofuel internal decomposition engine
US1719023A (en) Device for working combustion engines with liquid or pulverized fuels
US1165086A (en) Internal-combustion engine.
US2920444A (en) Pulse reaction combustion engine
GB287938A (en) Method of and apparatus for working explosion turbines by means of coal dust
US785166A (en) Internal-combustion engine.
GB288321A (en) Combined fuel and air admission device for oil explosion turbines
GB793978A (en) Turbine-operated engine starting arrangement
US716794A (en) Method of producing liquids under pressure.
US1026871A (en) Internal-combustion engine.
GB583549A (en) Improvements in or relating to blast propulsion
US2011033A (en) Fuel engine
GB1090131A (en) Improvements in or relating to power units
GB921846A (en) Improvements in pulse jets
JPS5781115A (en) Engine jetting air-fuel mixture
GB701117A (en) Liquid fuel combustion apparatus
GB282342A (en) Improved method of and apparatus for preparing charges containing liquid fuel for use in internal combustion engines
US1418232A (en) charles
GB671965A (en) Process and apparatus for starting engines at high altitudes
GB784121A (en) Improvements in apparatus for generating a flow of gaseous working fluid for a primemover
GB741253A (en) Improvements relating to jet propulsion engines
US711597A (en) Machinery for the production of liquid under pressure.