GB999581A - A gas turbine power plant - Google Patents

A gas turbine power plant

Info

Publication number
GB999581A
GB999581A GB2653261A GB2653261A GB999581A GB 999581 A GB999581 A GB 999581A GB 2653261 A GB2653261 A GB 2653261A GB 2653261 A GB2653261 A GB 2653261A GB 999581 A GB999581 A GB 999581A
Authority
GB
United Kingdom
Prior art keywords
air
fuel
combustion chamber
oxidiser
reservoir
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
GB2653261A
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 GB999581A publication Critical patent/GB999581A/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
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/74—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant
    • F02K9/78—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with an air-breathing jet-propulsion plant
    • 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • 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
    • F02K3/12—Plants including a gas turbine driving a compressor or a ducted fan characterised by having more than one gas turbine
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/16—Composite ram-jet/turbo-jet engines

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)

Abstract

999,581. Gas turbine engines; jet propulsion engines; combustion chambers. A. KORGANOFF. July 21, 1961 [July 22, 1960], No. 26532/61. Headings F1G, F1J and F1L. A gas turbine power plant comprises a combustion chamber having an air intake for feeding air thereto from an ambient medium when the medium contains oxygen to support combustion, a first reservoir containing fuel and having an outlet to the combustion chamber, a second reservoir containing either oxidiser or a monofuel and having an outlet to the combustion chamber, means being provided for regulating the air intake and the outlets from the reservoirs so as to provide either a combustible air/fuel mixture, a combustible fuel/ oxidiser mixture, a combustible air/fuel/ oxidiser mixture, or in the case where monofuel is contained in the second reservoir, monofuel in the combustion chamber, there being a gas turbine drivable by the products of combustion. In Fig. 1 the combustion chamber 1 is connected to an air reservoir 2b having an inlet for air under pressure, a reservoir 4 containing fuel such as kerosene, and a reservoir 6 containing an oxidiser such as liquid hydrogen peroxide. The ducts leading from the reservoirs to the combustion chamber have valves 9, 10 and 8 whereby either fuel and air, or fuel and oxidiser or fuel and air and oxidiser may be supplied to the chamber. The gases from the chamber 1 pass to the turbine 12 which drives a shaft 35. In Fig. 2 the combustion chamber 13 is annular and has inlets 14, 15 and 16 for the supply of fuel, of oxidiser or monopropellant, and of air respectively, the inlets being controlled by valves 19, 21 and 20. Air enters the intake duct 18 and passes through one or more compressors 17 before passing to the inlet 16. Gases from the combustion chamber pass into a turbine 23 which drives the shaft 24, the exhaust gases from the turbine passing through duct 28 and propulsion nozzle 27. Alternatively by adjustment of the deflectors some or all of the gases from the combustion chamber may be passed directly to the propulsion nozzle.
GB2653261A 1960-07-22 1961-07-21 A gas turbine power plant Expired GB999581A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR833681A FR1270683A (en) 1960-07-22 1960-07-22 New combustion engine

Publications (1)

Publication Number Publication Date
GB999581A true GB999581A (en) 1965-07-28

Family

ID=8735990

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2653261A Expired GB999581A (en) 1960-07-22 1961-07-21 A gas turbine power plant

Country Status (2)

Country Link
FR (1) FR1270683A (en)
GB (1) GB999581A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3486699A (en) * 1965-11-22 1969-12-30 Snecma Adjustable exhaust unit for turbojet propulsion engines
US4389842A (en) * 1980-03-29 1983-06-28 Vereinigte Flugtechnische Werke Gmbh Power unit with gas turbine
GB2143280A (en) * 1983-06-24 1985-02-06 John Bernard Attkins Propulsion device
FR2552422A1 (en) * 1983-09-22 1985-03-29 Suzuki Satoru PROPULSIVE AGENT FOR ROCKET ENGINES
EP0247388A2 (en) * 1986-05-30 1987-12-02 ERNO Raumfahrttechnik Gesellschaft mit beschränkter Haftung Rocket propulsion system having air-breathing possibilities
GB2240815A (en) * 1983-12-23 1991-08-14 Alan Bond Dual-mode aerospace propulsion engine.
WO1997037115A1 (en) * 1996-03-29 1997-10-09 Kunkel, Klaus Method of operating a gasturbine with silanol as fuel
WO2009136389A1 (en) * 2008-05-05 2009-11-12 Joshua Waldhorn Turbine driven by predetermined deflagration of anaerobic fuel and method thereof

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3486699A (en) * 1965-11-22 1969-12-30 Snecma Adjustable exhaust unit for turbojet propulsion engines
US4389842A (en) * 1980-03-29 1983-06-28 Vereinigte Flugtechnische Werke Gmbh Power unit with gas turbine
GB2143280A (en) * 1983-06-24 1985-02-06 John Bernard Attkins Propulsion device
FR2552422A1 (en) * 1983-09-22 1985-03-29 Suzuki Satoru PROPULSIVE AGENT FOR ROCKET ENGINES
GB2147052A (en) * 1983-09-22 1985-05-01 Satoru Suzuki Additional propellant for rocket
GB2240815A (en) * 1983-12-23 1991-08-14 Alan Bond Dual-mode aerospace propulsion engine.
GB2240815B (en) * 1983-12-23 1991-12-18 Alan Bond Improvements in aerospace propulsion
US5101622A (en) * 1983-12-23 1992-04-07 Rolls-Royce Plc Aerospace propulsion
EP0247388A2 (en) * 1986-05-30 1987-12-02 ERNO Raumfahrttechnik Gesellschaft mit beschränkter Haftung Rocket propulsion system having air-breathing possibilities
EP0247388A3 (en) * 1986-05-30 1988-09-14 Erno Raumfahrttechnik Gesellschaft Mit Beschrankter Haftung Rocket propulsion system having air-breathing possibilities
WO1997037115A1 (en) * 1996-03-29 1997-10-09 Kunkel, Klaus Method of operating a gasturbine with silanol as fuel
WO2009136389A1 (en) * 2008-05-05 2009-11-12 Joshua Waldhorn Turbine driven by predetermined deflagration of anaerobic fuel and method thereof

Also Published As

Publication number Publication date
FR1270683A (en) 1961-09-01

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