GB476195A - Method and device for continuously generating motive fluid and supplying the same to combustion fuel turbines and the like - Google Patents

Method and device for continuously generating motive fluid and supplying the same to combustion fuel turbines and the like

Info

Publication number
GB476195A
GB476195A GB22307/36A GB2230736A GB476195A GB 476195 A GB476195 A GB 476195A GB 22307/36 A GB22307/36 A GB 22307/36A GB 2230736 A GB2230736 A GB 2230736A GB 476195 A GB476195 A GB 476195A
Authority
GB
United Kingdom
Prior art keywords
air
fuel
combustion
supplying
jacket
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
GB22307/36A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB476195A publication Critical patent/GB476195A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/26—Controlling the air flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/005—Combined with pressure or heat exchangers
    • 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)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)

Abstract

476,195. Gas turbines. GOMORY, A. B. Aug. 13, 1936, No. 22307. Convention date, Aug. 13, 1935. [Class 110 (iii)] [Also in Group XII] Fuel and air delivered by pumps 12, 14, Fig. 1, pass through throttle valves 22, 23, controlled from pressure responsive devices in the combustion chambers 1, 2, 3. The fuel is pre-heated by being passed through a jacket 4 around the combustion chambers. In a modification shown in Fig. 2, a single combustion chamber delivers products of combustion to a chamber 29 through coiled pipes 32 immersed in the liquid fuel contained in the jacket 23. Air from the pump 25 passes to the burner nozzle 191 through an outer jacket 27. A constant ignition arc is maintained between electrodes 35, 36. Water may be injected from a pump 49 by pipes 50, 51, 52 and 53 into the combustion chamber, the fuel supply or the air supply and its quantity may be controlled with the fuel and air supplies. An air reservoir 41 is associated with the air supply and may be used for supplying air at starting.
GB22307/36A 1935-08-13 1936-08-13 Method and device for continuously generating motive fluid and supplying the same to combustion fuel turbines and the like Expired GB476195A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH476195X 1935-08-13

Publications (1)

Publication Number Publication Date
GB476195A true GB476195A (en) 1937-12-03

Family

ID=4516162

Family Applications (1)

Application Number Title Priority Date Filing Date
GB22307/36A Expired GB476195A (en) 1935-08-13 1936-08-13 Method and device for continuously generating motive fluid and supplying the same to combustion fuel turbines and the like

Country Status (1)

Country Link
GB (1) GB476195A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2484221A (en) * 1946-06-25 1949-10-11 Westinghouse Electric Corp Chemical type power plant for torpedo propulsion
US3088280A (en) * 1959-04-17 1963-05-07 Rolls Royce Reducing smoke in gas turbine engine exhaust
US3092965A (en) * 1959-05-11 1963-06-11 Thiokol Chemical Corp Automatic pressure control for a gas generating chamber
US3334486A (en) * 1965-06-09 1967-08-08 M A N Turbo G M B H Continuous flow combustion engine
US3651641A (en) * 1969-03-18 1972-03-28 Ginter Corp Engine system and thermogenerator therefor
US4462342A (en) * 1982-02-08 1984-07-31 Welden David P Variable stage direct field boiler
US5305735A (en) * 1993-03-29 1994-04-26 Welden David P Direct fired hot water generator with more than one heat exchange zone
WO2011009452A2 (en) * 2009-07-24 2011-01-27 GETAS GESELLSCHAFT FüR THERMODYNAMISCHE ANTRIEBSSYSTEME MBH Axial-piston motor and method for operating an axial-piston motor

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2484221A (en) * 1946-06-25 1949-10-11 Westinghouse Electric Corp Chemical type power plant for torpedo propulsion
US3088280A (en) * 1959-04-17 1963-05-07 Rolls Royce Reducing smoke in gas turbine engine exhaust
US3092965A (en) * 1959-05-11 1963-06-11 Thiokol Chemical Corp Automatic pressure control for a gas generating chamber
US3334486A (en) * 1965-06-09 1967-08-08 M A N Turbo G M B H Continuous flow combustion engine
US3651641A (en) * 1969-03-18 1972-03-28 Ginter Corp Engine system and thermogenerator therefor
US4462342A (en) * 1982-02-08 1984-07-31 Welden David P Variable stage direct field boiler
US5305735A (en) * 1993-03-29 1994-04-26 Welden David P Direct fired hot water generator with more than one heat exchange zone
US5368474A (en) * 1993-03-29 1994-11-29 Welden; David P. Direct fired hot water generator with more than one heat exchange zone
WO2011009452A2 (en) * 2009-07-24 2011-01-27 GETAS GESELLSCHAFT FüR THERMODYNAMISCHE ANTRIEBSSYSTEME MBH Axial-piston motor and method for operating an axial-piston motor
WO2011009452A3 (en) * 2009-07-24 2011-04-14 GETAS GESELLSCHAFT FüR THERMODYNAMISCHE ANTRIEBSSYSTEME MBH Axial-piston motor and method for operating an axial-piston motor
US9188000B2 (en) 2009-07-24 2015-11-17 Getas Gesellschaft Fuer Thermodynamische Antriebssysteme Mbh Axial-piston motor with continuously working combustion chamber having two combustion air inputs

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