GB1173566A - Gas Turbine Improvements. - Google Patents

Gas Turbine Improvements.

Info

Publication number
GB1173566A
GB1173566A GB3586566A GB3586566A GB1173566A GB 1173566 A GB1173566 A GB 1173566A GB 3586566 A GB3586566 A GB 3586566A GB 3586566 A GB3586566 A GB 3586566A GB 1173566 A GB1173566 A GB 1173566A
Authority
GB
United Kingdom
Prior art keywords
turbine
compressor
rotor
gas turbine
rotor assembly
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
GB3586566A
Inventor
William Hartley
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 GB3586566A priority Critical patent/GB1173566A/en
Publication of GB1173566A publication Critical patent/GB1173566A/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
    • 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
    • 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
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/38—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising rotary fuel injection means

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

1,173,566. Gas turbine plant. W. HARTLEY. Aug.16, 1967 [Aug. 10, 1966], No.35865/66. Heading F1G. The invention relates to a gas turbine engine which comprises a centrifugal type air compressor G, a plurality of combustion spaces M, and a radial inward flow turbine K, these parts being formed as a single rotary assembly and being enclosed within a casing or shroud so that the working fluid duct is completely enclosed except for air intake at the compressor inlet and gas discharge at the turbine outlet. A fixed stator casing O is disposed around the rotor assembly, the space therebetween being excavated. A starting device L comprising a bladed rotor rotatably mounted on bearings C adjacent the compressor inlet is provided, the rotor being driven off starting. The compressor and turbine rotor assembly is mounted in bearings B, fuel supply and ignition devices being provided in duct D. The space N between the rotor assembly and the stator casing O is excavated by means of a suction pump connected to the point P. Leakage preventing seals are provided at Q. Four combustion spaces M are provided in the embodiment but any number may be provided.
GB3586566A 1966-08-10 1966-08-10 Gas Turbine Improvements. Expired GB1173566A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3586566A GB1173566A (en) 1966-08-10 1966-08-10 Gas Turbine Improvements.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3586566A GB1173566A (en) 1966-08-10 1966-08-10 Gas Turbine Improvements.

Publications (1)

Publication Number Publication Date
GB1173566A true GB1173566A (en) 1969-12-10

Family

ID=10382405

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3586566A Expired GB1173566A (en) 1966-08-10 1966-08-10 Gas Turbine Improvements.

Country Status (1)

Country Link
GB (1) GB1173566A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5395908U (en) * 1977-01-05 1978-08-04
DE2715161A1 (en) * 1977-04-05 1978-10-12 Steffens Juergen Rotary casing gas turbine - has central fuel supply, peripheral air entry, compressor and turbine blades coaxial within housing
JPS53149104U (en) * 1977-04-30 1978-11-24
GB2339854A (en) * 1998-07-27 2000-02-09 Dilip Daniel James Rotary internal combustion engine
WO2002059469A1 (en) * 2001-01-26 2002-08-01 Academy Projects Limited Turbine engine
GB2379956A (en) * 2001-06-29 2003-03-26 Brian Sowards Rotary internal combustion engine

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5395908U (en) * 1977-01-05 1978-08-04
DE2715161A1 (en) * 1977-04-05 1978-10-12 Steffens Juergen Rotary casing gas turbine - has central fuel supply, peripheral air entry, compressor and turbine blades coaxial within housing
JPS53149104U (en) * 1977-04-30 1978-11-24
GB2339854A (en) * 1998-07-27 2000-02-09 Dilip Daniel James Rotary internal combustion engine
WO2002059469A1 (en) * 2001-01-26 2002-08-01 Academy Projects Limited Turbine engine
GB2379956A (en) * 2001-06-29 2003-03-26 Brian Sowards Rotary internal combustion engine
GB2379956B (en) * 2001-06-29 2004-10-27 Brian Sowards Internal combustion engine

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Legal Events

Date Code Title Description
PS Patent sealed
PLNP Patent lapsed through nonpayment of renewal fees