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GB2017222A - Gas Turbine Unit - Google Patents

Gas Turbine Unit

Info

Publication number
GB2017222A
GB2017222A GB7909616A GB7909616A GB2017222A GB 2017222 A GB2017222 A GB 2017222A GB 7909616 A GB7909616 A GB 7909616A GB 7909616 A GB7909616 A GB 7909616A GB 2017222 A GB2017222 A GB 2017222A
Authority
GB
United Kingdom
Prior art keywords
combustion
blading
turbine
rotor
rotate
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Withdrawn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
GB7909616A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB7909616A priority Critical patent/GB2017222A/en
Publication of GB2017222A publication Critical patent/GB2017222A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D99/00—Subject matter not provided for in other groups of this subclass
    • 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
    • F02C3/045—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having compressor and turbine passages in a single rotor-module
    • F02C3/05—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having compressor and turbine passages in a single rotor-module the compressor and the turbine being of the radial flow type
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

The unit comprises a rotor 1 with turbine blading 7 extending radially to define combustion passages. Inner and outer casing segments 9, 6 respectively define inlet ports and exhaust ports for the combustion passages. Fuel supplied at 16 burns within the enclosed spaces of the combustion passages, with air supplied by axial or centrifugal compressor 3, the burnt gases being expelled under pressure through the exhaust ports to provide a hot gas stream, for example, to rotate a turbine, or other blading, or for use as a heat source in a boiler, or as a propulsive stream. Notches on the inner surface of the outer casing 6 act as combustion stabilizers. The turbine blading 7 is shaped to impart a swirl to the exhaust gases to rotate the rotor. <IMAGE>
GB7909616A 1978-03-20 1979-03-19 Gas Turbine Unit Withdrawn GB2017222A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB7909616A GB2017222A (en) 1978-03-20 1979-03-19 Gas Turbine Unit

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB1085778 1978-03-20
GB7909616A GB2017222A (en) 1978-03-20 1979-03-19 Gas Turbine Unit

Publications (1)

Publication Number Publication Date
GB2017222A true GB2017222A (en) 1979-10-03

Family

ID=26247808

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7909616A Withdrawn GB2017222A (en) 1978-03-20 1979-03-19 Gas Turbine Unit

Country Status (1)

Country Link
GB (1) GB2017222A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4835960A (en) * 1982-07-22 1989-06-06 Skoczkowski Andzej M High compression gas turbine engine
WO1990001625A1 (en) * 1988-08-01 1990-02-22 Max Tobler Rotary combustion chamber with water injection and water cooling for a turbine
WO1998002643A1 (en) * 1996-07-16 1998-01-22 Massachusetts Institute Of Technology Microturbomachinery
NL1022803C2 (en) * 2003-02-28 2004-08-31 Micro Turbine Technology B V Micro reaction turbine with integrated combustion chamber and rotor.
USD576015S1 (en) * 2005-05-26 2008-09-02 Hoffman Enclosures, Inc. Hinge for flush mount enclosure
US7690616B2 (en) 2005-05-26 2010-04-06 Hoffman Enclosures, Inc. Mounting system for enclosure

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4835960A (en) * 1982-07-22 1989-06-06 Skoczkowski Andzej M High compression gas turbine engine
WO1990001625A1 (en) * 1988-08-01 1990-02-22 Max Tobler Rotary combustion chamber with water injection and water cooling for a turbine
WO1998002643A1 (en) * 1996-07-16 1998-01-22 Massachusetts Institute Of Technology Microturbomachinery
US5932940A (en) * 1996-07-16 1999-08-03 Massachusetts Institute Of Technology Microturbomachinery
US6392313B1 (en) 1996-07-16 2002-05-21 Massachusetts Institute Of Technology Microturbomachinery
NL1022803C2 (en) * 2003-02-28 2004-08-31 Micro Turbine Technology B V Micro reaction turbine with integrated combustion chamber and rotor.
USD576015S1 (en) * 2005-05-26 2008-09-02 Hoffman Enclosures, Inc. Hinge for flush mount enclosure
US7690616B2 (en) 2005-05-26 2010-04-06 Hoffman Enclosures, Inc. Mounting system for enclosure

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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)