SE8703275D0 - MOTROTERING, EXCHANGE-FREE FRONT LIGHT ENGINE WITH HIGH PREPARATION - Google Patents

MOTROTERING, EXCHANGE-FREE FRONT LIGHT ENGINE WITH HIGH PREPARATION

Info

Publication number
SE8703275D0
SE8703275D0 SE8703275A SE8703275A SE8703275D0 SE 8703275 D0 SE8703275 D0 SE 8703275D0 SE 8703275 A SE8703275 A SE 8703275A SE 8703275 A SE8703275 A SE 8703275A SE 8703275 D0 SE8703275 D0 SE 8703275D0
Authority
SE
Sweden
Prior art keywords
engine
counter rotating
turbine
fan
drive shafts
Prior art date
Application number
SE8703275A
Other languages
Swedish (sv)
Other versions
SE464718B (en
SE8703275L (en
Inventor
J B Taylor
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of SE8703275D0 publication Critical patent/SE8703275D0/en
Publication of SE8703275L publication Critical patent/SE8703275L/en
Publication of SE464718B publication Critical patent/SE464718B/en

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
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • F02C3/067—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages having counter-rotating rotors
    • 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
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

A gas turbine engine has a core gas generator engine 18, 16, 20, 22 for generating combustion gases, a power turbine 34, a front fan section 60, 62, and a booster compressor 64. The power turbine includes two counter rotatable turbine blade rows 38, 42 which are alternately interdigitized and serve to rotate counter rotating first and second drive shafts 46, 48 respectively. The fan section also includes counter rotating spaced apart fan blade sections 60, 62 which are respectively connected to the first and second drive shafts. The booster compressor 64 is axially positioned between the spaced apart fan sections. The booster compressor likewise includes first and second blade rows 68, 72 which are counter rotating alternately interdigitized and are likewise driven by the first and second drive shafts 46, 48. The engine is supported from two frames to permit the nacelle to be non-structural. The core engine is a modular unit so that it can be separable from the counter rotating turbine, fans and booster. A fan duct 56, may be supported via struts 58 (six or eight) which remove swirl from the air. <IMAGE>
SE8703275A 1986-08-29 1987-08-24 MOTORATING EXCHANGE-FREE FRONT FLAFT ENGINE SE464718B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US90234186A 1986-08-29 1986-08-29

Publications (3)

Publication Number Publication Date
SE8703275D0 true SE8703275D0 (en) 1987-08-24
SE8703275L SE8703275L (en) 1988-03-01
SE464718B SE464718B (en) 1991-06-03

Family

ID=25415717

Family Applications (1)

Application Number Title Priority Date Filing Date
SE8703275A SE464718B (en) 1986-08-29 1987-08-24 MOTORATING EXCHANGE-FREE FRONT FLAFT ENGINE

Country Status (6)

Country Link
JP (1) JP2927790B2 (en)
DE (1) DE3728437C2 (en)
FR (1) FR2603343B1 (en)
GB (1) GB2194593B (en)
IT (1) IT1222555B (en)
SE (1) SE464718B (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3812027A1 (en) * 1988-04-11 1989-10-26 Mtu Muenchen Gmbh PROPFAN TURBO ENGINE
US4976102A (en) * 1988-05-09 1990-12-11 General Electric Company Unducted, counterrotating gearless front fan engine
US5010729A (en) * 1989-01-03 1991-04-30 General Electric Company Geared counterrotating turbine/fan propulsion system
US5443590A (en) * 1993-06-18 1995-08-22 General Electric Company Rotatable turbine frame
AU3276397A (en) * 1996-06-28 1998-01-21 Hiroyasu Tanigawa Combined steam and gas turbine engine
DE19824421A1 (en) 1998-05-30 1999-12-02 Bmw Rolls Royce Gmbh Housing formation on a gas turbine
US6666017B2 (en) * 2002-05-24 2003-12-23 General Electric Company Counterrotatable booster compressor assembly for a gas turbine engine
US6684626B1 (en) * 2002-07-30 2004-02-03 General Electric Company Aircraft gas turbine engine with control vanes for counter rotating low pressure turbines
FR2866073B1 (en) * 2004-02-11 2006-07-28 Snecma Moteurs TURBOREACTOR HAVING TWO SOLIDARITY CONTRAROTATIVE BLOWERS OF A CONTRAROTATIVE LOW-PRESSURE COMPRESSOR
US7950220B2 (en) * 2006-06-19 2011-05-31 United Technologies Corporation Turbine engine compressor
DE102008005163B4 (en) 2008-01-19 2009-12-03 Deutsches Zentrum für Luft- und Raumfahrt e.V. Aircraft engine
US10961850B2 (en) * 2017-09-19 2021-03-30 General Electric Company Rotatable torque frame for gas turbine engine
FR3095670B1 (en) * 2019-04-30 2021-12-03 Safran Aircraft Engines Improved architecture of a contra-rotating turbine engine

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2404767A (en) * 1941-10-28 1946-07-23 Armstrong Siddeley Motors Ltd Jet propulsion plant
GB586570A (en) * 1943-03-18 1947-03-24 Karl Baumann Improvements in internal combustion turbine plant for propulsion
US3903690A (en) * 1973-02-12 1975-09-09 Gen Electric Turbofan engine lubrication means
US3861139A (en) * 1973-02-12 1975-01-21 Gen Electric Turbofan engine having counterrotating compressor and turbine elements and unique fan disposition
GB2061389B (en) * 1979-10-23 1983-05-18 Rolls Royce Rod installation for a gas turbine engine
NL8303401A (en) * 1982-11-01 1984-06-01 Gen Electric DRIVE TURBINE FOR OPPOSITE ROTATING PROPELLERS.
DE3507035A1 (en) * 1984-03-02 1985-09-12 General Electric Co., Schenectady, N.Y. GAS TURBINE ENGINE

Also Published As

Publication number Publication date
SE464718B (en) 1991-06-03
GB2194593A (en) 1988-03-09
DE3728437A1 (en) 1988-03-03
IT1222555B (en) 1990-09-05
JP2927790B2 (en) 1999-07-28
JPS63134817A (en) 1988-06-07
DE3728437C2 (en) 2002-01-31
GB8716113D0 (en) 1987-08-12
IT8721739A0 (en) 1987-08-28
GB2194593B (en) 1991-05-15
SE8703275L (en) 1988-03-01
FR2603343A1 (en) 1988-03-04
FR2603343B1 (en) 1994-04-08

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