JP6268529B2 - 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

Info

Publication number
JP6268529B2
JP6268529B2 JP2014070205A JP2014070205A JP6268529B2 JP 6268529 B2 JP6268529 B2 JP 6268529B2 JP 2014070205 A JP2014070205 A JP 2014070205A JP 2014070205 A JP2014070205 A JP 2014070205A JP 6268529 B2 JP6268529 B2 JP 6268529B2
Authority
JP
Japan
Prior art keywords
jet engine
flame
flame holder
combustor
fuel
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
JP2014070205A
Other languages
English (en)
Japanese (ja)
Other versions
JP2015190740A (ja
JP2015190740A5 (enExample
Inventor
祥彦 上野
祥彦 上野
正二郎 古谷
正二郎 古谷
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries 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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP2014070205A priority Critical patent/JP6268529B2/ja
Priority to EP15769123.9A priority patent/EP3098429B1/en
Priority to US15/120,867 priority patent/US10274199B2/en
Priority to PCT/JP2015/054301 priority patent/WO2015146375A1/ja
Publication of JP2015190740A publication Critical patent/JP2015190740A/ja
Publication of JP2015190740A5 publication Critical patent/JP2015190740A5/ja
Application granted granted Critical
Publication of JP6268529B2 publication Critical patent/JP6268529B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/22—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants movable, e.g. to an inoperative position; adjustable, e.g. self-adjusting
    • 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
    • F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
    • 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
    • F02K7/18—Composite ram-jet/rocket engines
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60—Support structures; Attaching or mounting means
    • 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
    • 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
    • F05D2260/00—Function
    • F05D2260/99—Ignition, e.g. ignition by warming up of fuel or oxidizer in a resonant acoustic cavity
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00015—Trapped vortex combustion chambers
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00017—Assembling combustion chamber liners or subparts
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Testing Of Engines (AREA)
JP2014070205A 2014-03-28 2014-03-28 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 JP6268529B2 (ja)

Priority Applications (4)

Application Number Priority Date Filing Date Title
JP2014070205A JP6268529B2 (ja) 2014-03-28 2014-03-28 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
EP15769123.9A EP3098429B1 (en) 2014-03-28 2015-02-17 Jet engine, flying body, and method for operating jet engine
US15/120,867 US10274199B2 (en) 2014-03-28 2015-02-17 Jet engine, flying object, and method of operating jet engine
PCT/JP2015/054301 WO2015146375A1 (ja) 2014-03-28 2015-02-17 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

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2014070205A JP6268529B2 (ja) 2014-03-28 2014-03-28 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
JP2015190740A JP2015190740A (ja) 2015-11-02
JP2015190740A5 JP2015190740A5 (enExample) 2017-02-16
JP6268529B2 true JP6268529B2 (ja) 2018-01-31

Family

ID=54194911

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2014070205A Active JP6268529B2 (ja) 2014-03-28 2014-03-28 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

Country Status (4)

Country Link
US (1) US10274199B2 (enExample)
EP (1) EP3098429B1 (enExample)
JP (1) JP6268529B2 (enExample)
WO (1) WO2015146375A1 (enExample)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6719933B2 (ja) * 2016-03-16 2020-07-08 三菱重工業株式会社 ジェットエンジン、飛しょう体、および、ジェットエンジンの動作方法
JP2017166409A (ja) * 2016-03-16 2017-09-21 三菱重工業株式会社 ジェットエンジン、および、飛しょう体
JP6628246B2 (ja) * 2016-03-28 2020-01-08 三菱重工業株式会社 スクラムジェットエンジン、飛しょう体
CN106121825B (zh) * 2016-07-28 2018-03-13 西安航天动力试验技术研究所 发动机进气道堵盖及其开闭系统
US11415080B2 (en) * 2018-05-14 2022-08-16 General Electric Company Engine for an aircraft
CN113006967B (zh) * 2021-02-08 2022-04-19 中国人民解放军国防科技大学 一种火箭与前缘突扩凹腔组合的rbcc内流道
CN113720611B (zh) * 2021-06-25 2022-07-26 蓝箭航天空间科技股份有限公司 运载火箭起飞推力模拟加载装置
CN114440259B (zh) * 2021-12-14 2023-01-17 西安航天动力研究所 一种多路供油的拼接式火焰稳定装置

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2989922A (en) * 1953-02-17 1961-06-27 Marvin H Greenwood Ramjet propulsion device
US3074668A (en) * 1958-12-10 1963-01-22 Snecma Burner for hot fuel
US3667233A (en) * 1969-11-14 1972-06-06 Us Air Force Dual mode supersonic combustion ramjet engine
US4628688A (en) * 1983-08-29 1986-12-16 The United States Of America As Represented By The Secretary Of The Navy Solid fuel ramjet flow control device
FR2661454B1 (fr) * 1985-07-12 1994-02-11 Onera Perfectionnements apportes aux propulseurs de type statoreacteur.
US5174524A (en) * 1991-10-10 1992-12-29 General Electric Company Cooling system for high speed aircraft
JP3032377B2 (ja) * 1992-06-05 2000-04-17 ダイセル化学工業株式会社 ラムジェットエンジンの点火手段
JPH09250395A (ja) 1996-03-18 1997-09-22 Ishikawajima Harima Heavy Ind Co Ltd ジェットエンジンの可変式フレームホルダ
US6293091B1 (en) * 1999-04-22 2001-09-25 Trw Inc. Axisymmetrical annular plug propulsion system for integrated rocket/ramjet or rocket/scramjet
US6739121B2 (en) * 2002-01-22 2004-05-25 Environmental Areoscience Corp. Flame holder for a hybrid rocket motor
JP5791323B2 (ja) * 2011-03-29 2015-10-07 三菱重工業株式会社 スクラムジェットエンジン
JP5758163B2 (ja) * 2011-03-30 2015-08-05 三菱重工業株式会社 スクラムジェットエンジン

Also Published As

Publication number Publication date
JP2015190740A (ja) 2015-11-02
WO2015146375A1 (ja) 2015-10-01
EP3098429B1 (en) 2018-12-12
EP3098429A1 (en) 2016-11-30
US10274199B2 (en) 2019-04-30
US20160363318A1 (en) 2016-12-15
EP3098429A4 (en) 2017-03-22

Similar Documents

Publication Publication Date Title
JP6268529B2 (ja) 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
JP6719933B2 (ja) ジェットエンジン、飛しょう体、および、ジェットエンジンの動作方法
WO2009142674A1 (en) Rocket nozzles for unconventional vehicles
JP6310292B2 (ja) 燃焼器、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
EP3098515B1 (en) Jet engine, flying body, and method for operating a jet engine
JP5791323B2 (ja) スクラムジェットエンジン
JP6204250B2 (ja) 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
WO2015151621A1 (ja) 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
JP6310293B2 (ja) 燃焼器、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
JP6037818B2 (ja) ジェットエンジン
WO2017158856A1 (ja) ジェットエンジン、および飛しょう体
JP6016616B2 (ja) ジェットエンジン
AU2012277568A1 (en) A bomb for deployment from an air vehicle
JP5777294B2 (ja) 飛しょう体

Legal Events

Date Code Title Description
A521 Written amendment

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20170111

A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20170111

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20171129

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20171213

R150 Certificate of patent or registration of utility model

Ref document number: 6268529

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150