GB1524259A - Turbines - Google Patents

Turbines

Info

Publication number
GB1524259A
GB1524259A GB4696675A GB4696675A GB1524259A GB 1524259 A GB1524259 A GB 1524259A GB 4696675 A GB4696675 A GB 4696675A GB 4696675 A GB4696675 A GB 4696675A GB 1524259 A GB1524259 A GB 1524259A
Authority
GB
United Kingdom
Prior art keywords
turbine
compressor
water
combustion
nov
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
GB4696675A
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.)
Lewis V D
Original Assignee
Lewis V D
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 Lewis V D filed Critical Lewis V D
Priority to GB4696675A priority Critical patent/GB1524259A/en
Publication of GB1524259A publication Critical patent/GB1524259A/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
    • 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
    • F02C3/30—Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases
    • F02C3/305—Increasing the power, speed, torque or efficiency of a gas turbine or the thrust of a turbojet engine by injecting or adding water, steam or other fluids
    • 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
    • F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • F02C3/16—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

1524259 Gas turbine plant; combustion chambers V D Lewis 12 Nov 1976 [14 Nov 1975 22 Dec 1975] 46966/75 and 52298/75 Headings FIG and F1L [Also in Division F4] A turbine plant comprises an inward flow compressor 3d supplying air to a rotating combustion chamber 7 into a port-combustion region of which water is injected through ducts 23, the combustion gas/water mixture flowing outwardly to reaction jets so as to drive turbine 2d. As shown, the latter drives compressor 3d via chains and sprockets 75 77 etc., but in a modification Fig. 1, (not shown) the compressor and turbine are rigidly connected. In a further arrangement Fig. 4, (not shown) a separate power output turbine is provided. The turbine exhaust stream pre-heats the water in a direct contact heater (20), Fig. 3, (not shown).
GB4696675A 1976-11-12 1976-11-12 Turbines Expired GB1524259A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB4696675A GB1524259A (en) 1976-11-12 1976-11-12 Turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4696675A GB1524259A (en) 1976-11-12 1976-11-12 Turbines

Publications (1)

Publication Number Publication Date
GB1524259A true GB1524259A (en) 1978-09-06

Family

ID=10443246

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4696675A Expired GB1524259A (en) 1976-11-12 1976-11-12 Turbines

Country Status (1)

Country Link
GB (1) GB1524259A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0163335A1 (en) * 1982-02-03 1985-12-04 Kenji Watanabe Hydrogen fueled gas turbine engine
GB2187273A (en) * 1985-10-31 1987-09-03 Bernard George Ediss A gas turbine binary cycle
WO1990001625A1 (en) * 1988-08-01 1990-02-22 Max Tobler Rotary combustion chamber with water injection and water cooling for a turbine
DE4240871A1 (en) * 1992-08-10 1994-02-17 Graf Werner Compressor operating on fluid piston principle - uses fluid medium to close one side of working chamber
US20130101393A1 (en) * 2011-10-24 2013-04-25 Hybrid Turbine Group Reaction turbine and hybrid impulse reaction turbine
CN104196638A (en) * 2014-08-29 2014-12-10 孙朝宽 Floral axis and combustion gas turbine

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0163335A1 (en) * 1982-02-03 1985-12-04 Kenji Watanabe Hydrogen fueled gas turbine engine
GB2187273A (en) * 1985-10-31 1987-09-03 Bernard George Ediss A gas turbine binary cycle
GB2187273B (en) * 1985-10-31 1990-01-24 Bernard George Ediss A gas turbine binary cycle
WO1990001625A1 (en) * 1988-08-01 1990-02-22 Max Tobler Rotary combustion chamber with water injection and water cooling for a turbine
DE4240871A1 (en) * 1992-08-10 1994-02-17 Graf Werner Compressor operating on fluid piston principle - uses fluid medium to close one side of working chamber
US20130101393A1 (en) * 2011-10-24 2013-04-25 Hybrid Turbine Group Reaction turbine and hybrid impulse reaction turbine
WO2013063115A1 (en) * 2011-10-24 2013-05-02 Hybrid Turbine Group Reaction turbine and hybrid impulse reaction turbine
JP2014530997A (en) * 2011-10-24 2014-11-20 ハイブリッドタービン グループ Reaction turbine and hybrid impulse reaction turbine
EP2771545A4 (en) * 2011-10-24 2015-12-30 Hybrid Turbine Group Reaction turbine and hybrid impulse reaction turbine
US9255478B2 (en) 2011-10-24 2016-02-09 Hybrid Turbine Group Reaction turbine and hybrid impulse reaction turbine
CN104196638A (en) * 2014-08-29 2014-12-10 孙朝宽 Floral axis and combustion gas turbine
CN104196638B (en) * 2014-08-29 2015-12-02 孙朝宽 A kind of floral axis and gas turbine

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Legal Events

Date Code Title Description
PS Patent sealed
746 Register noted 'licences of right' (sect. 46/1977)
PCNP Patent ceased through non-payment of renewal fee