GB2526611B - Hybrid Electric Ramjet Engine - Google Patents

Hybrid Electric Ramjet Engine

Info

Publication number
GB2526611B
GB2526611B GB1409600.2A GB201409600A GB2526611B GB 2526611 B GB2526611 B GB 2526611B GB 201409600 A GB201409600 A GB 201409600A GB 2526611 B GB2526611 B GB 2526611B
Authority
GB
United Kingdom
Prior art keywords
hybrid electric
ramjet engine
ramjet
engine
hybrid
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.)
Active
Application number
GB1409600.2A
Other versions
GB2526611A (en
GB201409600D0 (en
Inventor
William Lefley Paul
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 GB1409600.2A priority Critical patent/GB2526611B/en
Publication of GB201409600D0 publication Critical patent/GB201409600D0/en
Priority to SE1600350A priority patent/SE542641C2/en
Priority to PCT/GB2015/000148 priority patent/WO2015181512A1/en
Publication of GB2526611A publication Critical patent/GB2526611A/en
Application granted granted Critical
Publication of GB2526611B publication Critical patent/GB2526611B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/02—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/16—Composite ram-jet/turbo-jet engines
    • 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
    • F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/12—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the combustion chambers having inlet or outlet valves, e.g. Holzwarth gas-turbine plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K5/00—Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan
    • F02K5/02—Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan the engine being of the reciprocating-piston type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/12—Injection-induction jet engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/18—Composite ram-jet/rocket engines
    • 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
    • F05D2220/00—Application
    • F05D2220/10—Application in ram-jet engines or ram-jet driven vehicles
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
GB1409600.2A 2014-05-30 2014-05-30 Hybrid Electric Ramjet Engine Active GB2526611B (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB1409600.2A GB2526611B (en) 2014-05-30 2014-05-30 Hybrid Electric Ramjet Engine
SE1600350A SE542641C2 (en) 2014-05-30 2015-05-22 Ramjet Engine, Hybrid
PCT/GB2015/000148 WO2015181512A1 (en) 2014-05-30 2015-05-22 A new ramjet engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1409600.2A GB2526611B (en) 2014-05-30 2014-05-30 Hybrid Electric Ramjet Engine

Publications (3)

Publication Number Publication Date
GB201409600D0 GB201409600D0 (en) 2014-07-16
GB2526611A GB2526611A (en) 2015-12-02
GB2526611B true GB2526611B (en) 2017-09-20

Family

ID=51214454

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1409600.2A Active GB2526611B (en) 2014-05-30 2014-05-30 Hybrid Electric Ramjet Engine

Country Status (3)

Country Link
GB (1) GB2526611B (en)
SE (1) SE542641C2 (en)
WO (1) WO2015181512A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20220341374A1 (en) * 2020-09-22 2022-10-27 Taiwan Innovative Space, Inc. Motor And Fuel-Powered Hybrid System for a Rocket Thruster

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3044714B1 (en) * 2015-12-08 2020-08-28 Airbus Group Sas HYBRID POWER OR PUSH GENERATOR AND VEHICLE CONTAINING SUCH A GENERATOR
CN106884739A (en) * 2017-05-05 2017-06-23 中国科学院力学研究所 A kind of punching engine that thrust is lifted based on liquid fuel mixing energetic material powder
US10762726B2 (en) 2017-06-13 2020-09-01 General Electric Company Hybrid-electric propulsion system for an aircraft
WO2020180368A2 (en) 2019-03-01 2020-09-10 United Technologies Advanced Projects, Inc. Aircraft having hybrid-electric propulsion system with electric storage located in fuselage
EP3798130B1 (en) 2019-09-30 2023-03-01 Hamilton Sundstrand Corporation Systems and methods for battery ventilation
US11879415B2 (en) 2020-07-13 2024-01-23 Rafael Mártinez-Vilanova Piñó Jet engine for aircraft
EP3985241B1 (en) * 2020-10-14 2023-11-29 Taiwan Innovative Space, Inc. Motor and fuel-powered hybrid system for a rocket thruster
WO2022175739A1 (en) * 2021-11-23 2022-08-25 Nejati Mohammadamin Ramjet or scrum jet aircraft engine with the capability of mounting two fans behind the aircraft's nozzle

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1031192A (en) * 1963-02-15 1966-06-02 Kershaw H A Improvements in thermal engines; for example, jet propulsion units and gas turbine engines
US3719428A (en) * 1969-03-14 1973-03-06 W Dettmering Jet engine for hypersonic intake velocities
US3812672A (en) * 1972-02-10 1974-05-28 Cci Aerospace Corp Supercharged ejector ramjet aircraft engine
US4368620A (en) * 1980-06-20 1983-01-18 Giles Jr Harry L Windmills for ramjet engine
GB2230820A (en) * 1989-02-07 1990-10-31 Kershaw H A Ram jet device
WO2004072451A1 (en) * 2003-02-12 2004-08-26 Ishikawajima-Harima Heavy Industries Co., Ltd. Pulse detonation engine system for driving turbine
JP2009162097A (en) * 2007-12-28 2009-07-23 Koichi Yokozeki Improved pulse jet engine "fan pulse jet engine"

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1031192A (en) * 1963-02-15 1966-06-02 Kershaw H A Improvements in thermal engines; for example, jet propulsion units and gas turbine engines
US3719428A (en) * 1969-03-14 1973-03-06 W Dettmering Jet engine for hypersonic intake velocities
US3812672A (en) * 1972-02-10 1974-05-28 Cci Aerospace Corp Supercharged ejector ramjet aircraft engine
US4368620A (en) * 1980-06-20 1983-01-18 Giles Jr Harry L Windmills for ramjet engine
GB2230820A (en) * 1989-02-07 1990-10-31 Kershaw H A Ram jet device
WO2004072451A1 (en) * 2003-02-12 2004-08-26 Ishikawajima-Harima Heavy Industries Co., Ltd. Pulse detonation engine system for driving turbine
JP2009162097A (en) * 2007-12-28 2009-07-23 Koichi Yokozeki Improved pulse jet engine "fan pulse jet engine"

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20220341374A1 (en) * 2020-09-22 2022-10-27 Taiwan Innovative Space, Inc. Motor And Fuel-Powered Hybrid System for a Rocket Thruster
US11598288B2 (en) * 2020-09-22 2023-03-07 Taiwan Innovative Space, Inc. Motor and fuel-powered hybrid system for a rocket thruster

Also Published As

Publication number Publication date
GB2526611A (en) 2015-12-02
SE542641C2 (en) 2020-06-23
SE1600350A1 (en) 2016-12-22
GB201409600D0 (en) 2014-07-16
WO2015181512A1 (en) 2015-12-03
WO2015181512A4 (en) 2015-12-23

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