JP6310302B2 - ジェットエンジン、飛しょう体及びジェットエンジンの動作方法 - Google Patents

ジェットエンジン、飛しょう体及びジェットエンジンの動作方法 Download PDF

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Publication number
JP6310302B2
JP6310302B2 JP2014074491A JP2014074491A JP6310302B2 JP 6310302 B2 JP6310302 B2 JP 6310302B2 JP 2014074491 A JP2014074491 A JP 2014074491A JP 2014074491 A JP2014074491 A JP 2014074491A JP 6310302 B2 JP6310302 B2 JP 6310302B2
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fuel
jet engine
sectional area
flow path
speed
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JP2014074491A
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Japanese (ja)
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JP2015197058A (ja
JP2015197058A5 (enExample
Inventor
祥彦 上野
祥彦 上野
正二郎 古谷
正二郎 古谷
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Mitsubishi Heavy Industries Ltd
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Mitsubishi Heavy Industries Ltd
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Priority to JP2014074491A priority Critical patent/JP6310302B2/ja
Priority to US15/121,187 priority patent/US11203984B2/en
Priority to PCT/JP2015/054476 priority patent/WO2015151621A1/ja
Priority to EP15773405.4A priority patent/EP3098420B1/en
Publication of JP2015197058A publication Critical patent/JP2015197058A/ja
Publication of JP2015197058A5 publication Critical patent/JP2015197058A5/ja
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    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/32—Control of fuel supply characterised by throttling of fuel
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • F02C7/222—Fuel flow conduits, e.g. manifolds
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • F02C7/232—Fuel valves; Draining valves or systems
    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/44—Control of fuel supply responsive to the speed of aircraft, e.g. Mach number control, optimisation of fuel consumption
    • 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
    • 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
    • F02K7/14—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 with external combustion, e.g. scram-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
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N1/00—Regulating fuel supply
    • F23N1/002—Regulating fuel supply using electronic means
    • 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
    • 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
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet 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
    • F05D2220/80—Application in supersonic vehicles excluding hypersonic vehicles or ram, scram or rocket propulsion
    • 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
    • F05D2240/00—Components
    • F05D2240/35—Combustors or associated equipment
    • 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
    • F05D2250/00—Geometry
    • F05D2250/90—Variable geometry
    • 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
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/306—Mass flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N2237/00—Controlling
    • F23N2237/02—Controlling two or more burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N2237/00—Controlling
    • F23N2237/10—High or low fire
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N2241/00—Applications
    • F23N2241/20—Gas turbines

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Nozzles (AREA)
  • Fuel-Injection Apparatus (AREA)
JP2014074491A 2014-03-31 2014-03-31 ジェットエンジン、飛しょう体及びジェットエンジンの動作方法 Active JP6310302B2 (ja)

Priority Applications (4)

Application Number Priority Date Filing Date Title
JP2014074491A JP6310302B2 (ja) 2014-03-31 2014-03-31 ジェットエンジン、飛しょう体及びジェットエンジンの動作方法
US15/121,187 US11203984B2 (en) 2014-03-31 2015-02-18 Jet engine, flying object, and method of operating a jet engine
PCT/JP2015/054476 WO2015151621A1 (ja) 2014-03-31 2015-02-18 ジェットエンジン、飛しょう体及びジェットエンジンの動作方法
EP15773405.4A EP3098420B1 (en) 2014-03-31 2015-02-18 Jet engine, flying vehicle, and method for operating jet engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2014074491A JP6310302B2 (ja) 2014-03-31 2014-03-31 ジェットエンジン、飛しょう体及びジェットエンジンの動作方法

Publications (3)

Publication Number Publication Date
JP2015197058A JP2015197058A (ja) 2015-11-09
JP2015197058A5 JP2015197058A5 (enExample) 2017-02-16
JP6310302B2 true JP6310302B2 (ja) 2018-04-11

Family

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JP2014074491A Active JP6310302B2 (ja) 2014-03-31 2014-03-31 ジェットエンジン、飛しょう体及びジェットエンジンの動作方法

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Country Link
US (1) US11203984B2 (enExample)
EP (1) EP3098420B1 (enExample)
JP (1) JP6310302B2 (enExample)
WO (1) WO2015151621A1 (enExample)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107084071B (zh) * 2017-04-20 2018-06-05 中国人民解放军国防科学技术大学 一种基于爆震燃烧的超燃冲压发动机
US10973600B2 (en) 2017-09-29 2021-04-13 Ethicon Llc Power axle wrist for robotic surgical tool
JP6975658B2 (ja) * 2018-02-23 2021-12-01 三菱重工業株式会社 整流構造体及び飛しょう体
US11473780B2 (en) 2018-02-26 2022-10-18 General Electric Company Engine with rotating detonation combustion system
CN113123898B (zh) * 2021-04-19 2022-06-07 中国人民解放军国防科技大学 一种基于分隔板后缘射流扰动的超声速流混合装置
CN119178170B (zh) * 2024-10-09 2025-09-12 南京航空航天大学 超燃冲压-斜爆震组合发动机燃烧室中的可分离支板结构
CN121875835B (zh) * 2026-03-20 2026-05-26 中国空气动力研究与发展中心计算空气动力研究所 用于进气道启动增强的微型超声速喷管阵列装置及发动机

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FR1217843A (fr) * 1958-12-10 1960-05-05 Snecma Brûleur de combustion ou de post-combustion pour combustible chaud
US3448947A (en) * 1967-01-30 1969-06-10 Us Navy Fuel throttling computer
DE1800611A1 (de) * 1968-10-02 1970-05-27 Hertel Dr Ing Heinrich Anordnung zum Einspritzen von Kraftstoff in einen an einer Einspritzduese mit UEberschallgeschwindigkeit vorbeistroemenden Luftstrom
US3667233A (en) * 1969-11-14 1972-06-06 Us Air Force Dual mode supersonic combustion ramjet engine
US4327886A (en) * 1972-11-30 1982-05-04 The United States Of America As Represented By The Secretary Of The Navy Integral rocket ramjet missile
US4381642A (en) * 1980-06-20 1983-05-03 The Boeing Company Ramjet engine
JPH08219408A (ja) 1995-02-08 1996-08-30 Ishikawajima Harima Heavy Ind Co Ltd 超音速燃焼器
GB0027288D0 (en) * 2000-11-08 2000-12-27 Rolls Royce Plc Overthrust protection system and method
JP5529650B2 (ja) * 2010-07-01 2014-06-25 三菱重工業株式会社 超音速燃焼器
JP5762003B2 (ja) * 2011-01-06 2015-08-12 三菱重工業株式会社 スクラムジェットエンジンの燃料噴射制御装置
US9726115B1 (en) * 2011-02-15 2017-08-08 Aerojet Rocketdyne, Inc. Selectable ramjet propulsion system
JP5758160B2 (ja) * 2011-03-23 2015-08-05 三菱重工業株式会社 スクラムジェットエンジン
JP5701187B2 (ja) * 2011-09-13 2015-04-15 三菱重工業株式会社 超音速燃焼器

Also Published As

Publication number Publication date
US20170009665A1 (en) 2017-01-12
EP3098420B1 (en) 2020-04-22
WO2015151621A1 (ja) 2015-10-08
JP2015197058A (ja) 2015-11-09
EP3098420A4 (en) 2017-03-22
EP3098420A1 (en) 2016-11-30
US11203984B2 (en) 2021-12-21

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