GB1408309A - Gas turbine jet engine for an aircraft - Google Patents

Gas turbine jet engine for an aircraft

Info

Publication number
GB1408309A
GB1408309A GB4583972A GB4583972A GB1408309A GB 1408309 A GB1408309 A GB 1408309A GB 4583972 A GB4583972 A GB 4583972A GB 4583972 A GB4583972 A GB 4583972A GB 1408309 A GB1408309 A GB 1408309A
Authority
GB
United Kingdom
Prior art keywords
turbine
fan
compressor
air
duct
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
GB4583972A
Other languages
English (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.)
MTU Aero Engines AG
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
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 MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Publication of GB1408309A publication Critical patent/GB1408309A/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
    • 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
    • F02K3/077—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 the plant being of the multiple flow type, i.e. having three or more flows

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)
GB4583972A 1971-10-05 1972-10-04 Gas turbine jet engine for an aircraft Expired GB1408309A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19712149619 DE2149619A1 (de) 1971-10-05 1971-10-05 Turbinenstrahltriebwerk fuer senkrechtoder kurzstartende bzw. landende flugzeuge

Publications (1)

Publication Number Publication Date
GB1408309A true GB1408309A (en) 1975-10-01

Family

ID=5821510

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4583972A Expired GB1408309A (en) 1971-10-05 1972-10-04 Gas turbine jet engine for an aircraft

Country Status (4)

Country Link
US (1) US3867813A (enExample)
DE (1) DE2149619A1 (enExample)
FR (1) FR2156083B1 (enExample)
GB (1) GB1408309A (enExample)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2149016A (en) * 1983-10-31 1985-06-05 Gen Electric Air control system
US4543785A (en) * 1982-07-07 1985-10-01 Hugh Patrick Turbo-ram-jet engine
GB2157371A (en) * 1984-02-10 1985-10-23 Hugh Patrick Combined turbo-jet and ram-jet engine

Families Citing this family (51)

* Cited by examiner, † Cited by third party
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US4043121A (en) * 1975-01-02 1977-08-23 General Electric Company Two-spool variable cycle engine
GB1535765A (en) * 1975-01-02 1978-12-13 Gen Electric Variable cycle turbofan engines
US4085583A (en) * 1975-03-31 1978-04-25 The Boeing Company Method for selectively switching motive fluid supply to an aft turbine of a multicycle engine
US4064692A (en) * 1975-06-02 1977-12-27 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Variable cycle gas turbine engines
US4044973A (en) * 1975-12-29 1977-08-30 The Boeing Company Nacelle assembly and mounting structures for a turbofan jet propulsion engine
GB1545365A (en) * 1977-02-24 1979-05-10 Rolls Royce Gas turbine engines
US4222233A (en) * 1977-08-02 1980-09-16 General Electric Company Auxiliary lift propulsion system with oversized front fan
US4240250A (en) * 1977-12-27 1980-12-23 The Boeing Company Noise reducing air inlet for gas turbine engines
US4306412A (en) * 1978-11-24 1981-12-22 The Boeing Company Jet engine and method of operating the same
US4598543A (en) * 1985-02-06 1986-07-08 The United States Of America As Represented By The Secretary Of The Air Force Variable cycle engine for high altitude aircraft
US5184460A (en) * 1991-01-30 1993-02-09 The United States Of America As Represented By The Administrator, National Aeronautics And Space Administration Multi-heat addition turbine engine
US5261227A (en) * 1992-11-24 1993-11-16 General Electric Company Variable specific thrust turbofan engine
GB9313905D0 (en) * 1993-07-06 1993-08-25 Rolls Royce Plc Shaft power transfer in gas turbine engines
GB2435743B (en) * 1994-11-29 2008-02-06 British Aerospace Gas turbine powerplant
RU2165547C2 (ru) * 1998-03-17 2001-04-20 Владимир Иосифович Белоус Многоступенчатый осевой компрессор авиационного двигателя
US6385959B1 (en) 1999-08-24 2002-05-14 MONTOYA CéSAR AGUILERA Gas turbine engine with increased fuel efficiency and method for accomplishing the same
GB2353983B (en) * 2000-07-04 2003-10-15 Adrian Alexander Hubbard Variable mode jet engine-suitable for STOVL
US6837038B2 (en) * 2001-10-16 2005-01-04 United Technologies Corporation Variable cycle boost propulsor
US6739120B2 (en) * 2002-04-29 2004-05-25 General Electric Company Counterrotatable booster compressor assembly for a gas turbine engine
RU2237176C1 (ru) * 2002-12-20 2004-09-27 Открытое акционерное общество "Научно-производственное объединение "Сатурн" Двухконтурный турбореактивный двигатель
US7254951B2 (en) * 2003-01-07 2007-08-14 Lockwood Jr Hanford N High compression gas turbine with superheat enhancement
US7055306B2 (en) * 2003-04-30 2006-06-06 Hamilton Sundstrand Corporation Combined stage single shaft turbofan engine
US7246484B2 (en) * 2003-08-25 2007-07-24 General Electric Company FLADE gas turbine engine with counter-rotatable fans
FR2866387B1 (fr) * 2004-02-12 2008-03-14 Snecma Moteurs Adaptation aerodynamique de la soufflante arriere d'un turboreacteur double soufflante
US7353647B2 (en) * 2004-05-13 2008-04-08 General Electric Company Methods and apparatus for assembling gas turbine engines
FR2875866B1 (fr) * 2004-09-30 2006-12-08 Snecma Moteurs Sa Procede de circulation d'air dans un compresseur de turbomachine, agencement de compresseur le mettant en oeuvre , etage de compression et compresseur comportant un tel agencement, et moteur d'aeronef equipe d'un tel compresseur
US7134271B2 (en) * 2004-11-05 2006-11-14 General Electric Company Thrust vectoring aft FLADE engine
US7730714B2 (en) * 2005-11-29 2010-06-08 General Electric Company Turbofan gas turbine engine with variable fan outlet guide vanes
US7614210B2 (en) * 2006-02-13 2009-11-10 General Electric Company Double bypass turbofan
RU2312239C1 (ru) * 2006-02-20 2007-12-10 Николай Борисович Болотин Силовая установка газотурбовоза
US7685805B2 (en) 2006-11-20 2010-03-30 Pratt & Whitney Canada Corp. Turbofan gas turbine engine and nacelle arrangement
US20080148708A1 (en) * 2006-12-20 2008-06-26 General Electric Company Turbine engine system with shafts for improved weight and vibration characteristic
US8061119B2 (en) * 2007-11-29 2011-11-22 United Technologies Corporation Actuation mechanism for a convertible gas turbine propulsion system
US8511058B2 (en) * 2007-11-29 2013-08-20 United Technologies Corporation Convertible gas turbine propulsion system
US20100170221A1 (en) * 2009-01-08 2010-07-08 Toyota Jidosha Kabushiki Kaisha Turbo fan engine
US8667775B1 (en) * 2009-08-05 2014-03-11 The Boeing Company Reverse flow engine core having a ducted fan with integrated secondary flow blades
US8689538B2 (en) * 2009-09-09 2014-04-08 The Boeing Company Ultra-efficient propulsor with an augmentor fan circumscribing a turbofan
US9581084B2 (en) 2010-03-24 2017-02-28 Thomas Lucian Hurlburt System and method for preventing objects from entering the intake of a jet engine
US9156561B2 (en) * 2010-03-24 2015-10-13 Thomas Lucian Hurlburt System and method for preventing objects from entering the intake of a jet engine
US8382030B2 (en) 2010-09-02 2013-02-26 Patrick A. Kosheleff Variable cycle VTOL powerplant
US9279388B2 (en) 2011-11-01 2016-03-08 United Technologies Corporation Gas turbine engine with two-spool fan and variable vane turbine
EP2904218B1 (en) * 2012-10-01 2021-10-27 Raytheon Technologies Corporation Low compressor having variable vanes
US20160047304A1 (en) * 2013-12-19 2016-02-18 United Technologies Corporation Ultra high overall pressure ratio gas turbine engine
US20150176530A1 (en) * 2013-12-19 2015-06-25 United Technologies Corporation Ultra high overall pessure ratio gas turbine engine
GB201813671D0 (en) 2018-08-22 2018-10-03 Rolls Royce Plc Turbomachine
GB201813674D0 (en) 2018-08-22 2018-10-03 Rolls Royce Plc Turbomachine
GB201813672D0 (en) 2018-08-22 2018-10-03 Rolls Royce Plc Turbomachine
GB201813670D0 (en) 2018-08-22 2018-10-03 Rolls Royce Plc Turbomachine
GB201813675D0 (en) 2018-08-22 2018-10-03 Rolls Royce Plc Turbomachine
US11453488B2 (en) * 2019-09-30 2022-09-27 Rolls-Royce Corporation Lightweight parallel combustion lift system for vertical takeoff aircraft
US12025141B1 (en) * 2023-11-10 2024-07-02 Cyclazoom, LLC Fan compressor supercharger/water pump

Family Cites Families (11)

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Publication number Priority date Publication date Assignee Title
US2504181A (en) * 1950-04-18 Double compound independent rotor
US2528635A (en) * 1943-06-22 1950-11-07 Rolls Royce Power gas generator for internalcombustion power units
US2587649A (en) * 1946-10-18 1952-03-04 Pope Francis Selective turbopropeller jet power plant for aircraft
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
US3093968A (en) * 1960-05-05 1963-06-18 Cornell Aeronautical Labor Inc Method and apparatus for augmenting the drive of a gas turbine
NL130254C (enExample) * 1960-12-15
US3122343A (en) * 1961-12-02 1964-02-25 M A N Turbomotoren G M B H Vertical take-off and landing aircraft
GB992931A (en) * 1964-02-21 1965-05-26 Rolls Royce Gas turbine jet propulsion engine
US3318095A (en) * 1964-05-14 1967-05-09 Bristol Siddeley Engines Ltd Jet propulsion plant for aircraft with gas turbine engine and with fan driven by exhaust of such engine
US3489338A (en) * 1966-04-12 1970-01-13 Dowty Rotol Ltd Gas turbine engines
GB1120658A (en) * 1967-04-20 1968-07-24 Rolls Royce Power plant for a helicopter

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4543785A (en) * 1982-07-07 1985-10-01 Hugh Patrick Turbo-ram-jet engine
GB2149016A (en) * 1983-10-31 1985-06-05 Gen Electric Air control system
GB2157371A (en) * 1984-02-10 1985-10-23 Hugh Patrick Combined turbo-jet and ram-jet engine

Also Published As

Publication number Publication date
US3867813A (en) 1975-02-25
FR2156083A1 (enExample) 1973-05-25
FR2156083B1 (enExample) 1977-01-14
DE2149619A1 (de) 1973-04-19

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PLNP Patent lapsed through nonpayment of renewal fees