GB8610559D0 - Gas turbine engines - Google Patents

Gas turbine engines

Info

Publication number
GB8610559D0
GB8610559D0 GB868610559A GB8610559A GB8610559D0 GB 8610559 D0 GB8610559 D0 GB 8610559D0 GB 868610559 A GB868610559 A GB 868610559A GB 8610559 A GB8610559 A GB 8610559A GB 8610559 D0 GB8610559 D0 GB 8610559D0
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engines
engines
gas
turbine
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.)
Withdrawn
Application number
GB868610559A
Other versions
GB2189844A (en
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB08610559A priority Critical patent/GB2189844A/en
Publication of GB8610559D0 publication Critical patent/GB8610559D0/en
Publication of GB2189844A publication Critical patent/GB2189844A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K3/00Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02Plants 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
    • F02K3/04Plants 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
    • F02K3/065Plants 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 front and aft fans
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C5/00Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/02Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K3/00Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02Plants 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
    • F02K3/04Plants 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
    • F02K3/072Plants 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/56Combustion chambers having rotary flame tubes
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
GB08610559A 1986-04-30 1986-04-30 Gas turbine engines Withdrawn GB2189844A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08610559A GB2189844A (en) 1986-04-30 1986-04-30 Gas turbine engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB08610559A GB2189844A (en) 1986-04-30 1986-04-30 Gas turbine engines

Publications (2)

Publication Number Publication Date
GB8610559D0 true GB8610559D0 (en) 1986-11-26
GB2189844A GB2189844A (en) 1987-11-04

Family

ID=10597108

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08610559A Withdrawn GB2189844A (en) 1986-04-30 1986-04-30 Gas turbine engines

Country Status (1)

Country Link
GB (1) GB2189844A (en)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2192234B (en) * 1986-07-02 1991-04-17 Rolls Royce Plc A turbofan gas turbine engine
US5010729A (en) * 1989-01-03 1991-04-30 General Electric Company Geared counterrotating turbine/fan propulsion system
FR2645911B1 (en) * 1989-04-18 1991-06-07 Snecma HIGH DILUTION MOTOR WITH UPSTREAM BLOWER AND DOWNSTREAM BLOWER
DE4234248A1 (en) * 1992-10-10 1994-04-14 Asea Brown Boveri Gas turbine group
RU2052145C1 (en) * 1993-08-08 1996-01-10 Анатолий Михайлович Рахмаилов Method of converting heat energy into mechanical work
WO2005008043A2 (en) * 2003-07-23 2005-01-27 Eugene Thomas David Archery Tangentially exhausting revolving combustion chamber in a revolving ramjet, turbojet, turbofan, gas turbine or other jet engine
FR2866074B1 (en) * 2004-02-11 2006-04-28 Snecma Moteurs ARCHITECTURE OF A TURBOJET ENGINE HAVING A DOUBLE BLOWER FORWARD
US7185484B2 (en) 2004-08-11 2007-03-06 General Electric Company Methods and apparatus for assembling a gas turbine engine
ES2342586B1 (en) * 2008-04-30 2011-06-14 Futur Investment Partners, S.A. AERONAUTICAL TURBOPROPULSOR.
DE102014226696A1 (en) * 2014-12-19 2016-06-23 Rolls-Royce Deutschland Ltd & Co Kg Pre-compressor device, retrofit kit and aircraft engine
FR3067056B1 (en) * 2017-06-01 2019-07-26 Safran Aircraft Engines NON-CAREN ROTOR TYPE TURBOREACTOR
GB201813674D0 (en) 2018-08-22 2018-10-03 Rolls Royce Plc Turbomachine
GB201813672D0 (en) 2018-08-22 2018-10-03 Rolls Royce Plc Turbomachine
GB201813671D0 (en) 2018-08-22 2018-10-03 Rolls Royce Plc Turbomachine
GB201813675D0 (en) 2018-08-22 2018-10-03 Rolls Royce Plc Turbomachine
GB201813670D0 (en) 2018-08-22 2018-10-03 Rolls Royce Plc Turbomachine

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1321657A (en) * 1970-09-16 1973-06-27 Secr Defence Ducted fan gas turbine jet propulsion engine
NL8303401A (en) * 1982-11-01 1984-06-01 Gen Electric DRIVE TURBINE FOR OPPOSITE ROTATING PROPELLERS.

Also Published As

Publication number Publication date
GB2189844A (en) 1987-11-04

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)