GB586557A - Improvements in internal combustion turbine plant for propulsion - Google Patents

Improvements in internal combustion turbine plant for propulsion

Info

Publication number
GB586557A
GB586557A GB47242A GB47242A GB586557A GB 586557 A GB586557 A GB 586557A GB 47242 A GB47242 A GB 47242A GB 47242 A GB47242 A GB 47242A GB 586557 A GB586557 A GB 586557A
Authority
GB
United Kingdom
Prior art keywords
contra
turbine
exhaust
rotational
airscrew
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
GB47242A
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.)
Metropolitan Vickers Electrical Co Ltd
Original Assignee
Metropolitan Vickers Electrical Co 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
Priority to BE468782D priority Critical patent/BE468782A/xx
Application filed by Metropolitan Vickers Electrical Co Ltd filed Critical Metropolitan Vickers Electrical Co Ltd
Priority to GB47242A priority patent/GB586557A/en
Priority to FR942481D priority patent/FR942481A/en
Priority to ES175239A priority patent/ES175239A1/en
Publication of GB586557A publication Critical patent/GB586557A/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
    • 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)
  • Gear Transmission (AREA)
  • Hybrid Electric Vehicles (AREA)

Abstract

586,557. Gas turbines. BAUMANN, K., and METROPOLITAN-VICKERS ELECTRICAL CO., Ltd. Jan. 12, 1942, No. 472. [Class 110 (iii)] [Also in Group XXXIII] The rotors of a contra-rotational turbine 2 drive a contra-rotational pair of air-screws 3 through reduction gear including pinions 20 mounted on fixed shafts 19 and internallytoothed wheels 24 resiliently attached to the airscrew bosses. The turbine exhaust passes through annular channels 25 in the bosses and these channels may be bladed merely to pass the exhaust or to extract power from the exhaust. Beyond the airscrews, the exhaust passes to a reaction propulsion jet 1. The contra-rotational turbine rotors may drive a single airscrew through appropriate gearing and a single rotation turbine may drive either a single airscrew or a contra-rotational pair. Specification 586,556 is referred to in the Provisional Specification.
GB47242A 1942-01-12 1942-01-12 Improvements in internal combustion turbine plant for propulsion Expired GB586557A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
BE468782D BE468782A (en) 1942-01-12
GB47242A GB586557A (en) 1942-01-12 1942-01-12 Improvements in internal combustion turbine plant for propulsion
FR942481D FR942481A (en) 1942-01-12 1946-08-28 Improvements to internal combustion turbo-engines for propulsion
ES175239A ES175239A1 (en) 1942-01-12 1946-10-09 AN INTERNAL COMBUSTION TURBINE INSTALLATION

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB47242A GB586557A (en) 1942-01-12 1942-01-12 Improvements in internal combustion turbine plant for propulsion

Publications (1)

Publication Number Publication Date
GB586557A true GB586557A (en) 1947-03-24

Family

ID=9704953

Family Applications (1)

Application Number Title Priority Date Filing Date
GB47242A Expired GB586557A (en) 1942-01-12 1942-01-12 Improvements in internal combustion turbine plant for propulsion

Country Status (4)

Country Link
BE (1) BE468782A (en)
ES (1) ES175239A1 (en)
FR (1) FR942481A (en)
GB (1) GB586557A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3381475A (en) * 1965-06-28 1968-05-07 Bristol Siddeley Engines Ltd Jet propulsion engines
FR2521639A1 (en) * 1982-02-17 1983-08-19 Rolls Royce HIGH PERFORMANCE PROPELLER AIRPLANE PROPULSION ENGINE
GB2173863A (en) * 1985-04-17 1986-10-22 Rolls Royce A propeller module for an aero gas turbine engine
FR2620107A1 (en) * 1987-09-05 1989-03-10 Rolls Royce Plc GEARBOX SYSTEM FOR DRIVING MULTIPLE AUBES ROTORS IN OPPOSITE ROTATION
US4817382A (en) * 1985-12-31 1989-04-04 The Boeing Company Turboprop propulsion apparatus
US4936748A (en) * 1988-11-28 1990-06-26 General Electric Company Auxiliary power source in an unducted fan gas turbine engine
FR2641333A1 (en) * 1989-01-03 1990-07-06 Gen Electric DOUBLE FLOW TURBOREACTOR COMPRISING A CONTRAROTATIVE TURBINE FOR THE DRIVE OF THE BLOWER
US5108259A (en) * 1988-12-19 1992-04-28 General Electric Company Flexible connector for use in aircraft
WO2010070066A1 (en) * 2008-12-19 2010-06-24 Snecma System including counter-rotating propellers driven by an epicyclic train ensuring a balanced couple distribution between the two propellers
FR2948921A1 (en) * 2009-11-25 2011-02-11 Snecma Contrarotating propeller system for e.g. jet-prop engine of aircraft, has blades designed to apply engine torque to propeller in same direction of another torque when annular array of blades is traversed by air stream from turbine
WO2011083137A1 (en) * 2010-01-08 2011-07-14 Snecma Contra-rotating propeller system for an aircraft turbine engine

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4815273A (en) * 1985-12-31 1989-03-28 Peter Rudolph Single propeller turboprop propulsion apparatus

Cited By (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3381475A (en) * 1965-06-28 1968-05-07 Bristol Siddeley Engines Ltd Jet propulsion engines
FR2521639A1 (en) * 1982-02-17 1983-08-19 Rolls Royce HIGH PERFORMANCE PROPELLER AIRPLANE PROPULSION ENGINE
DE3304417A1 (en) * 1982-02-17 1983-09-15 Rolls-Royce Ltd., London AIRCRAFT ENGINE
US4488399A (en) * 1982-02-17 1984-12-18 Rolls-Royce Limited Propfan aircraft propulsion engine
GB2173863B (en) * 1985-04-17 1989-07-19 Rolls Royce Plc A propeller module for an aero gas turbine engine
GB2173863A (en) * 1985-04-17 1986-10-22 Rolls Royce A propeller module for an aero gas turbine engine
US4688995A (en) * 1985-04-17 1987-08-25 Rolls-Royce Plc Propeller module for an aero gas turbine engine
US4817382A (en) * 1985-12-31 1989-04-04 The Boeing Company Turboprop propulsion apparatus
US4964844A (en) * 1987-09-05 1990-10-23 Rolls-Royce Plc Gearbox arrangement for driving coaxial contra rotating multi-bladed rotors
FR2620107A1 (en) * 1987-09-05 1989-03-10 Rolls Royce Plc GEARBOX SYSTEM FOR DRIVING MULTIPLE AUBES ROTORS IN OPPOSITE ROTATION
US4936748A (en) * 1988-11-28 1990-06-26 General Electric Company Auxiliary power source in an unducted fan gas turbine engine
US5108259A (en) * 1988-12-19 1992-04-28 General Electric Company Flexible connector for use in aircraft
FR2641333A1 (en) * 1989-01-03 1990-07-06 Gen Electric DOUBLE FLOW TURBOREACTOR COMPRISING A CONTRAROTATIVE TURBINE FOR THE DRIVE OF THE BLOWER
GB2230298A (en) * 1989-01-03 1990-10-17 Gen Electric Geared counterrotating turbine/fan propulsion system
GB2230298B (en) * 1989-01-03 1993-09-22 Gen Electric Geared counterrotating turbine/fan propulsion system
CN102257260B (en) * 2008-12-19 2013-11-06 斯奈克玛 System including counter-rotating propellers driven by an epicyclic train ensuring a balanced couple distribution between the two propellers
FR2940247A1 (en) * 2008-12-19 2010-06-25 Snecma SYSTEM OF CONTRAROTATIVE PROPELLERS DRAWN BY AN EPICYCLOIDAL TRAIN PROVIDING A BALANCED TORQUE DISTRIBUTION BETWEEN THE TWO PROPELLERS
WO2010070066A1 (en) * 2008-12-19 2010-06-24 Snecma System including counter-rotating propellers driven by an epicyclic train ensuring a balanced couple distribution between the two propellers
RU2509903C2 (en) * 2008-12-19 2014-03-20 Снекма System of propellers running in opposite directions and driven by epicycloidal mechanism that ensures balanced distribution of torque between two propellers
US8876462B2 (en) 2008-12-19 2014-11-04 Snecma System of contra-rotating propellers driven by a planetary gear train providing a balanced distribution of torque between the two propellers
FR2948921A1 (en) * 2009-11-25 2011-02-11 Snecma Contrarotating propeller system for e.g. jet-prop engine of aircraft, has blades designed to apply engine torque to propeller in same direction of another torque when annular array of blades is traversed by air stream from turbine
WO2011083137A1 (en) * 2010-01-08 2011-07-14 Snecma Contra-rotating propeller system for an aircraft turbine engine
FR2955085A1 (en) * 2010-01-08 2011-07-15 Snecma SYSTEM FOR CONTRAROTATIVE PROPELLERS FOR AIRCRAFT TURBOMACHINE
CN102686864A (en) * 2010-01-08 2012-09-19 斯奈克玛 Contra-rotating propeller system for an aircraft turbine engine
CN102686864B (en) * 2010-01-08 2015-09-09 斯奈克玛 For the reversion spiral propeller system of airplane turbine engine
US9611809B2 (en) 2010-01-08 2017-04-04 Snecma Contra-rotating propeller system for an aircraft turbine engine

Also Published As

Publication number Publication date
ES175239A1 (en) 1946-11-16
BE468782A (en)
FR942481A (en) 1949-02-09

Similar Documents

Publication Publication Date Title
GB586557A (en) Improvements in internal combustion turbine plant for propulsion
GB958842A (en) Ducted fan lift engine
GB595357A (en) Improvements in or relating to power plants
GB587563A (en) Improvements relating to mountings for power plant
GB586570A (en) Improvements in internal combustion turbine plant for propulsion
GB581217A (en) Improvements in or relating to power plants for helicopters
GB742288A (en) Improvements in the cooling of turbines
GB602584A (en) Improvements in or relating to internal combustion turbine power plants
GB586551A (en) Improvements in or relating to internal combustion power turbine plant for propulsion in air
GB607839A (en) Improvements in or relating to gas-turbine power-plants
GB588092A (en) Improvements in or relating to internal combustion turbine power plants
GB658550A (en) Improvements in or relating to gas turbine power plants for propelling aircraft
GB586558A (en) Improvements in internal combustion turbine plant for propulsion
GB603283A (en) Improvements in or relating to internal combustion turbine power plants
GB587612A (en) Improvements in or relating to internal combustion turbine power plants
GB828884A (en) Improvements in or relating to aircraft
GB587516A (en) Improvements in or relating to regulating means for gas turbine installations
GB593403A (en) Power plant for the propulsion of aircraft
GB579140A (en) Improvements in or relating to gas turbines
GB588095A (en) Improvements in or relating to internal combustion turbine power plants
GB578005A (en) Improvements in and relating to jet propulsion plant
GB600608A (en) Improvements in or relating to internal combustion turbine power plants
GB638079A (en) Improvements in or relating to aircraft gas-turbine-engine power plants
GB582151A (en) Improvements in or relating to power plants
GB585509A (en) Improvements in or relating to power plants