GB1410543A - Hybrid gas turbine engine - Google Patents

Hybrid gas turbine engine

Info

Publication number
GB1410543A
GB1410543A GB1437673A GB1437673A GB1410543A GB 1410543 A GB1410543 A GB 1410543A GB 1437673 A GB1437673 A GB 1437673A GB 1437673 A GB1437673 A GB 1437673A GB 1410543 A GB1410543 A GB 1410543A
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine
fed
combustion products
combustion
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
GB1437673A
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.)
Nissan Motor Co Ltd
Original Assignee
Nissan Motor Co Ltd
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 Nissan Motor Co Ltd filed Critical Nissan Motor Co Ltd
Publication of GB1410543A publication Critical patent/GB1410543A/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
    • F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F02C3/26—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being solid or pulverulent, e.g. in slurry or suspension
    • 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
    • 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
    • F02C3/32—Inducing air flow by fluid jet, e.g. ejector action
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/60—Fluid transfer
    • F05D2260/601—Fluid transfer using an ejector or a jet pump

Abstract

1410543 Gas turbine plant; combustion chambers NISSAN MOTOR CO Ltd 26 March 1973 [1 April 1972] 14376/73 Headings F1G and F1L A gas turbine engine comprises a combustion chamber 32 to which is fed a solid or semi-solid fuel 34, and high temperature oxygen produced from a hydrogen peroxide source 10 via a catalyst chamber 26, the combustion products being directed to a cooling chamber 46 via a nozzle 44a surrounded by an ejector tube 48 arranged to draw in cooling air which is mixed with the combustion products and directed against the turbine blades 54. The fuel is a solid rod fed by an electric motor 40 and worm gear 38, or be in the form of gelled polyethylene and acryl resins and be fed by gravity. As shown, the turbine rotor 54 drives a main shaft 58 to drive a power transmission 62 and a generator 74 to charge the battery. At starting, the generator 74 may be utilized to drive the turbine. Again, Fig. 2, (not shown), a fan (90) drives cooling air into the ejector tube 48, and oppositely inclined inner and outer swirl vanes (88), (86), respectively, are arranged adjacent the outlet 44a to ensure complete mixing by rotating the combustion products and air in opposite directions. In Fig. 4, (not shown), the turbine 54 is arranged coaxially with the outlet 44a and is provided with guide vanes (96) controlled in accordance with varying operating conditions of the gas turbine engine. The blades may also be used to provide engine braking.
GB1437673A 1972-04-01 1973-03-26 Hybrid gas turbine engine Expired GB1410543A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3280972A JPS4899510A (en) 1972-04-01 1972-04-01

Publications (1)

Publication Number Publication Date
GB1410543A true GB1410543A (en) 1975-10-15

Family

ID=12369147

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1437673A Expired GB1410543A (en) 1972-04-01 1973-03-26 Hybrid gas turbine engine

Country Status (2)

Country Link
JP (1) JPS4899510A (en)
GB (1) GB1410543A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1993007361A1 (en) * 1991-10-11 1993-04-15 Martinez Michele Method of driving a turbine in rotation by means of a jet device
FR2695678A1 (en) * 1992-09-11 1994-03-18 Michele Martinez Control system for high speed turbine - includes venturi effect injector allowing control of mass flow rate of fuel mixture to increase output power
CN105841193A (en) * 2016-05-18 2016-08-10 葛明龙 Two aerospace turbofan engines
CN114278469A (en) * 2021-12-30 2022-04-05 重庆望江摩托车制造有限公司 Hybrid energy motorcycle utilizing methanol cracking to produce hydrogen

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2759748B2 (en) * 1993-11-20 1998-05-28 川崎重工業株式会社 High temperature and high pressure gas generator for turbine drive

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1993007361A1 (en) * 1991-10-11 1993-04-15 Martinez Michele Method of driving a turbine in rotation by means of a jet device
FR2682428A1 (en) * 1991-10-11 1993-04-16 Martinez Michele DEVICE FOR CONTROLLING AND CONTROLLING THE ROTATION OF A PNEUMATIC TURBINE.
US5553995A (en) * 1991-10-11 1996-09-10 Martinez; Mich+E,Gra E+Ee Le Method of driving a turbine in rotation by means of a jet device
FR2695678A1 (en) * 1992-09-11 1994-03-18 Michele Martinez Control system for high speed turbine - includes venturi effect injector allowing control of mass flow rate of fuel mixture to increase output power
CN105841193A (en) * 2016-05-18 2016-08-10 葛明龙 Two aerospace turbofan engines
CN105841193B (en) * 2016-05-18 2018-07-20 葛明龙 Two kinds of aerospace fanjets
US10563619B2 (en) 2016-05-18 2020-02-18 Minglong GE Aerospace turbofan engines
CN114278469A (en) * 2021-12-30 2022-04-05 重庆望江摩托车制造有限公司 Hybrid energy motorcycle utilizing methanol cracking to produce hydrogen
CN114278469B (en) * 2021-12-30 2022-10-21 重庆望江摩托车制造有限公司 Hybrid energy motorcycle utilizing methanol cracking to produce hydrogen

Also Published As

Publication number Publication date
JPS4899510A (en) 1973-12-17

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Legal Events

Date Code Title Description
PS Patent sealed
746 Register noted 'licences of right' (sect. 46/1977)
PCNP Patent ceased through non-payment of renewal fee