GB588096A - Improvements in or relating to internal combustion turbine power plants - Google Patents

Improvements in or relating to internal combustion turbine power plants

Info

Publication number
GB588096A
GB588096A GB7010/44A GB701044A GB588096A GB 588096 A GB588096 A GB 588096A GB 7010/44 A GB7010/44 A GB 7010/44A GB 701044 A GB701044 A GB 701044A GB 588096 A GB588096 A GB 588096A
Authority
GB
United Kingdom
Prior art keywords
turbine
air
compressor
plant
relating
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
GB7010/44A
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development 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 Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Publication of GB588096A publication Critical patent/GB588096A/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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/20—Adaptations of gas-turbine plants for driving vehicles
    • F02C6/206—Adaptations of gas-turbine plants for driving vehicles the vehicles being airscrew driven
    • 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
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/10—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor
    • 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
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • 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
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/062—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with aft fan
    • 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
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/072—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with counter-rotating, e.g. fan rotors

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

588,096. Gas turbines. POWER JETS (RESEARCH & DEVELOPMENT), Ltd., HOWELL, A. R., and HAWTHORNE, W. R. April 15, 1944, No. 7010. Drawings to Specification. [Class 110 (iii)] In a gas turbine plant in which L.P. and H.P. compressors are driven respectively by L.P. and H.P. turbines, the whole of the air taken in by the L.P. compressor passes to the H.P. compressor and the combustion chamber. The combustion chambers may surround the H.P. compressor, the air flow having two reversals, or they may be between the H.P. compressor and turbine with a straight air-flow. In jetpropulsion plant, a ducted jet-augmentor is provided by blades carried by a contra-rotating stator of the L.P. turbine or by contra-rotating bladings carried on the rotors of an additional exhaust turbine. The discharge of the jetaugmentor may be further energized by burning fuel in it. In a plant having air-screws and a jet, the air-screws may be driven by a separate exhaust turbine, or by the low-pressure turbine.
GB7010/44A 1944-04-15 1944-04-15 Improvements in or relating to internal combustion turbine power plants Expired GB588096A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB263473X 1944-04-15

Publications (1)

Publication Number Publication Date
GB588096A true GB588096A (en) 1947-05-14

Family

ID=10242240

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7010/44A Expired GB588096A (en) 1944-04-15 1944-04-15 Improvements in or relating to internal combustion turbine power plants

Country Status (3)

Country Link
BE (1) BE462340A (en)
CH (1) CH263473A (en)
GB (1) GB588096A (en)

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2586054A (en) * 1948-08-21 1952-02-19 Northrop Aircraft Inc Pusher turboprop exhaust system
US2627927A (en) * 1947-05-29 1953-02-10 Curtiss Wright Corp Propeller temperature control means
US2638744A (en) * 1948-12-09 1953-05-19 Lockheed Aircraft Corp Turbine power plant having auxiliary units
US2645412A (en) * 1949-09-28 1953-07-14 United Aircraft Corp Locking device for split-compressor type turbopower plants
US2689681A (en) * 1949-09-17 1954-09-21 United Aircraft Corp Reversely rotating screw type multiple impeller compressor
US2720078A (en) * 1948-03-01 1955-10-11 Solar Aircraft Co Burner for use in high velocity ducts
US2930544A (en) * 1955-11-02 1960-03-29 Alun R Howell Aircraft having vertical lifting jet engines
US2990108A (en) * 1957-03-04 1961-06-27 Curtiss Wright Corp Compressor with annular discharge diffuser
US2989843A (en) * 1953-07-24 1961-06-27 Curtiss Wright Corp Engine for supersonic flight
DE1126196B (en) * 1958-11-24 1962-03-22 Rolls Royce Gas turbine jet engine with bypass compressor
DE1131949B (en) * 1958-09-05 1962-06-20 Gen Electric Runner for a two-circuit turbo jet engine
DE1181005B (en) * 1959-11-26 1964-11-05 Rolls Royce Gas turbine engine
US3465524A (en) * 1966-03-02 1969-09-09 Rolls Royce Fan gas turbine engine
GB2117054A (en) * 1982-02-17 1983-10-05 Rolls Royce Aircraft propulsion engine having a rear mounted propfan
FR2581423A1 (en) * 1985-05-01 1986-11-07 Gen Electric COUNTER-ROTATION WORKING TURBINE
US4767270A (en) * 1986-04-16 1988-08-30 The Boeing Company Hoop fan jet engine
US4767271A (en) * 1986-07-02 1988-08-30 Rolls-Royce Plc Gas turbine engine power turbine
US4934139A (en) * 1986-07-02 1990-06-19 Rolls-Royce Plc Turbofan gas turbine engine
EP0394102A1 (en) * 1989-04-18 1990-10-24 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Counter-rotating engine with high bypass fans fore and aft
EP0860593A1 (en) * 1997-02-20 1998-08-26 SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION -Snecma Compression system for a turbomachine

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB881662A (en) * 1957-01-29 1961-11-08 Bristol Siddeley Engines Ltd Improvements in or relating to gas turbine jet propulsion engine units for aircraft and also jet propelled aircraft

Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2627927A (en) * 1947-05-29 1953-02-10 Curtiss Wright Corp Propeller temperature control means
US2720078A (en) * 1948-03-01 1955-10-11 Solar Aircraft Co Burner for use in high velocity ducts
US2586054A (en) * 1948-08-21 1952-02-19 Northrop Aircraft Inc Pusher turboprop exhaust system
US2638744A (en) * 1948-12-09 1953-05-19 Lockheed Aircraft Corp Turbine power plant having auxiliary units
US2689681A (en) * 1949-09-17 1954-09-21 United Aircraft Corp Reversely rotating screw type multiple impeller compressor
US2645412A (en) * 1949-09-28 1953-07-14 United Aircraft Corp Locking device for split-compressor type turbopower plants
US2989843A (en) * 1953-07-24 1961-06-27 Curtiss Wright Corp Engine for supersonic flight
US2930544A (en) * 1955-11-02 1960-03-29 Alun R Howell Aircraft having vertical lifting jet engines
US2990108A (en) * 1957-03-04 1961-06-27 Curtiss Wright Corp Compressor with annular discharge diffuser
DE1131949B (en) * 1958-09-05 1962-06-20 Gen Electric Runner for a two-circuit turbo jet engine
DE1126196B (en) * 1958-11-24 1962-03-22 Rolls Royce Gas turbine jet engine with bypass compressor
DE1181005B (en) * 1959-11-26 1964-11-05 Rolls Royce Gas turbine engine
US3465524A (en) * 1966-03-02 1969-09-09 Rolls Royce Fan gas turbine engine
GB2117054A (en) * 1982-02-17 1983-10-05 Rolls Royce Aircraft propulsion engine having a rear mounted propfan
US4488399A (en) * 1982-02-17 1984-12-18 Rolls-Royce Limited Propfan aircraft propulsion engine
FR2581423A1 (en) * 1985-05-01 1986-11-07 Gen Electric COUNTER-ROTATION WORKING TURBINE
US4767270A (en) * 1986-04-16 1988-08-30 The Boeing Company Hoop fan jet engine
US4767271A (en) * 1986-07-02 1988-08-30 Rolls-Royce Plc Gas turbine engine power turbine
US4934139A (en) * 1986-07-02 1990-06-19 Rolls-Royce Plc Turbofan gas turbine engine
EP0394102A1 (en) * 1989-04-18 1990-10-24 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Counter-rotating engine with high bypass fans fore and aft
US5058379A (en) * 1989-04-18 1991-10-22 Societe Nationale D'etude Et De Construction De Moteurs D'aviation High by-pass ratio turbojet engine with counterrotating upstream and downstream fans
EP0860593A1 (en) * 1997-02-20 1998-08-26 SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION -Snecma Compression system for a turbomachine

Also Published As

Publication number Publication date
CH263473A (en) 1949-08-31
BE462340A (en)

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