GB2019943A - Gas turbine engine - Google Patents

Gas turbine engine

Info

Publication number
GB2019943A
GB2019943A GB7914767A GB7914767A GB2019943A GB 2019943 A GB2019943 A GB 2019943A GB 7914767 A GB7914767 A GB 7914767A GB 7914767 A GB7914767 A GB 7914767A GB 2019943 A GB2019943 A GB 2019943A
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engine
rotor
chambers
compressor
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Withdrawn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
GB7914767A
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.)
Stidworthy F M
Original Assignee
Stidworthy F M
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 Stidworthy F M filed Critical Stidworthy F M
Publication of GB2019943A publication Critical patent/GB2019943A/en
Withdrawn legal-status Critical Current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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • F02C3/16—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant
    • F02C3/165—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant the combustion chamber contributes to the driving force by creating reactive thrust

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)

Abstract

The engine includes a rotor (100) for discharging combustion products from one or more combustion chambers (1) in a substantially tangential direction to rotate the rotor (100), which latter drives compressor (4) supplying air to the combustion chamber or chambers (1) and may also drive a power output shaft (2).The compressor can be of centrifugal centripetal or axial flow type. A fan 16 may be provided. Numerous modifications are described. <IMAGE>
GB7914767A 1978-04-29 1979-04-27 Gas turbine engine Withdrawn GB2019943A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1714478 1978-04-29

Publications (1)

Publication Number Publication Date
GB2019943A true GB2019943A (en) 1979-11-07

Family

ID=10090065

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7914767A Withdrawn GB2019943A (en) 1978-04-29 1979-04-27 Gas turbine engine

Country Status (2)

Country Link
JP (1) JPS551483A (en)
GB (1) GB2019943A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4625509A (en) * 1980-04-21 1986-12-02 Sheppard Sr Darrel J Combustion engine
GB2231622A (en) * 1989-03-16 1990-11-21 Harold Birkett Engine for v.t.o.l. and other aircraft
GB2388406A (en) * 2002-03-12 2003-11-12 Mark O'keeffe Rotary reaction generator
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
WO2008020758A1 (en) * 2006-08-18 2008-02-21 Micro Turbine Technology B.V. Reaction turbine engine
WO2014210409A1 (en) * 2013-06-28 2014-12-31 Exxonmobil Upstream Research Company Systems and methods of utilizing axial flow expanders
EP2400137A3 (en) * 2010-06-28 2017-12-20 RJT GmbH & Co KG Rotating ram-jet turbine with exhaust turbocharger
CN108119258A (en) * 2017-10-12 2018-06-05 邹国泉 Aeroengine combining centrifugal compressor, piston compressor, internal combustion engine and spray pipe
US10036265B2 (en) 2013-06-28 2018-07-31 Mitsubishi Heavy Industries Compressor Corporation Axial flow expander

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4625509A (en) * 1980-04-21 1986-12-02 Sheppard Sr Darrel J Combustion engine
GB2231622A (en) * 1989-03-16 1990-11-21 Harold Birkett Engine for v.t.o.l. and other aircraft
GB2231622B (en) * 1989-03-16 1993-10-27 Harold Birkett Engine for V.T.O.L. Aircraft
GB2388406A (en) * 2002-03-12 2003-11-12 Mark O'keeffe Rotary reaction generator
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
WO2005008043A3 (en) * 2003-07-23 2005-02-24 Eugene Thomas David Archery Tangentially exhausting revolving combustion chamber in a revolving ramjet, turbojet, turbofan, gas turbine or other jet engine
WO2008020758A1 (en) * 2006-08-18 2008-02-21 Micro Turbine Technology B.V. Reaction turbine engine
EP2400137A3 (en) * 2010-06-28 2017-12-20 RJT GmbH & Co KG Rotating ram-jet turbine with exhaust turbocharger
WO2014210409A1 (en) * 2013-06-28 2014-12-31 Exxonmobil Upstream Research Company Systems and methods of utilizing axial flow expanders
CN105579686A (en) * 2013-06-28 2016-05-11 埃克森美孚上游研究公司 Systems and methods of utilizing axial flow expanders
CN105579686B (en) * 2013-06-28 2018-02-23 埃克森美孚上游研究公司 Utilize the system and method for axially stream expanding machine
US10036265B2 (en) 2013-06-28 2018-07-31 Mitsubishi Heavy Industries Compressor Corporation Axial flow expander
US10385832B2 (en) 2013-06-28 2019-08-20 Exxonmobil Upstream Research Company Systems and methods of utilizing axial flow expanders
CN108119258A (en) * 2017-10-12 2018-06-05 邹国泉 Aeroengine combining centrifugal compressor, piston compressor, internal combustion engine and spray pipe
CN108119258B (en) * 2017-10-12 2020-06-23 邹国泉 Aeroengine combining centrifugal compressor, piston compressor, internal combustion engine and spray pipe

Also Published As

Publication number Publication date
JPS551483A (en) 1980-01-08

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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)