GB2009855A - Gas turbine plant - Google Patents

Gas turbine plant

Info

Publication number
GB2009855A
GB2009855A GB7844478A GB7844478A GB2009855A GB 2009855 A GB2009855 A GB 2009855A GB 7844478 A GB7844478 A GB 7844478A GB 7844478 A GB7844478 A GB 7844478A GB 2009855 A GB2009855 A GB 2009855A
Authority
GB
United Kingdom
Prior art keywords
rotor
compressor
gas turbine
combustion air
layshaft
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.)
Granted
Application number
GB7844478A
Other versions
GB2009855B (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.)
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 GB7844478A priority Critical patent/GB2009855B/en
Publication of GB2009855A publication Critical patent/GB2009855A/en
Application granted granted Critical
Publication of GB2009855B publication Critical patent/GB2009855B/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
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • F02C3/067—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages having counter-rotating rotors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/32—Non-positive-displacement machines or engines, e.g. steam turbines with pressure velocity transformation exclusively in rotor, e.g. the rotor rotating under the influence of jets issuing from the rotor, e.g. Heron turbines
    • 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

Abstract

In a Barkers mill type gas turbine engine e.g. for a helicopter, combustion air is fed to the combustion chambers d on the rotor c by a centrifugal compressor a driven by the rotor c via a layshaft gear k, the rotor being enclosed in a casing g into which the exhaust gas from jet nozzles f is passed to preheat the combustion air. Drive from the rotor, e.g. for propellors, wheels, fans or electric generators, is taken via a second layshaft n. Ignition via spark plugs e is effected from a battery via an ignition switch, booster coils, and slip rings p. The rotor c and compressor a may rotate in opposite directions. An electric starter motor/generator drives the compressor at starting, with the rotor disconnected therefrom by a clutch or solenoid mechanism. <IMAGE>
GB7844478A 1977-08-16 1978-11-14 Jetshaft power plant Expired GB2009855B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB7844478A GB2009855B (en) 1977-08-16 1978-11-14 Jetshaft power plant

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB3426077 1977-08-16
GB7844478A GB2009855B (en) 1977-08-16 1978-11-14 Jetshaft power plant

Publications (2)

Publication Number Publication Date
GB2009855A true GB2009855A (en) 1979-06-20
GB2009855B GB2009855B (en) 1982-02-24

Family

ID=26262217

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7844478A Expired GB2009855B (en) 1977-08-16 1978-11-14 Jetshaft power plant

Country Status (1)

Country Link
GB (1) GB2009855B (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2169034A (en) * 1984-12-20 1986-07-02 Taha Khalil Aldoss Jet engine having ramjet driven compressor
FR2680385A1 (en) * 1991-08-12 1993-02-19 Rignault Jean Turbine engine with orthogonal circular reaction
WO2008140433A2 (en) * 2007-05-15 2008-11-20 Ahmet Kaan Onay Turbo cyclic integral impulsion motor
WO2009068048A1 (en) * 2007-11-27 2009-06-04 Schneiderbauer-Schwendler, Enno Drive device with compression modification in the form of a thermal rotary engine with internal combustion

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2169034A (en) * 1984-12-20 1986-07-02 Taha Khalil Aldoss Jet engine having ramjet driven compressor
FR2680385A1 (en) * 1991-08-12 1993-02-19 Rignault Jean Turbine engine with orthogonal circular reaction
WO2008140433A2 (en) * 2007-05-15 2008-11-20 Ahmet Kaan Onay Turbo cyclic integral impulsion motor
WO2008140433A3 (en) * 2007-05-15 2008-12-31 Ahmet Kaan Onay Turbo cyclic integral impulsion motor
WO2009068048A1 (en) * 2007-11-27 2009-06-04 Schneiderbauer-Schwendler, Enno Drive device with compression modification in the form of a thermal rotary engine with internal combustion

Also Published As

Publication number Publication date
GB2009855B (en) 1982-02-24

Similar Documents

Publication Publication Date Title
US2962597A (en) Power plant apparatus
GB1509835A (en) Device for starting engines and for driving auxiliary equipment for aircraft
JPS55127221A (en) Driving system of vehicle
US2842937A (en) Aircraft engine cartridge starter control system
GB1057945A (en) Air breathing starters for gas turbine engines
GB2199900A (en) Starting/clutch arrangement in a turboprop/fan gas turbine engine
US4570438A (en) Pulse-controlled turbine
GB891064A (en) New or improved aircraft propulsion installation
GB2009855A (en) Gas turbine plant
GB887328A (en) Improvements in or relating to rotary internal combustion engines
WO2011139339A1 (en) Propulsion system and method
ES459614A1 (en) Electric starter for an engine
EP0101206A1 (en) High compression gas turbine engine
US3077736A (en) Gas generating device
GB1507908A (en) Method of starting a stand-by engine-driven emergency generating set
CN108644015B (en) A kind of self-starting gas-turbine unit burnt based on detonation
GB705611A (en) Improved gas turbine power plant
GB288217A (en) A method of regulating the speed of revolution of blowers for internal combustion engines, the exhaust gases of which are used for driving the blower
GB1179785A (en) Gas Turbine Powerplant
US2613499A (en) Starter and ignition means for turbojet engines
EP0300979A1 (en) Motor with turning ram jets
GB669945A (en) Improvements in or relating to marine propulsion power plant
JPS5686005A (en) Electric car motor with conical spiral rotary blades powered by air generation due to electromagnetic force
GB1467681A (en) Aircraft power plant including auxiliary engine for driving aircraft auxiliary components and an air-conditioning unit
JPS55114847A (en) Gas turbine

Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee