JP4705727B2 - 複合サイクル・パルスデトネーション・タービンエンジン - Google Patents

複合サイクル・パルスデトネーション・タービンエンジン Download PDF

Info

Publication number
JP4705727B2
JP4705727B2 JP2001097814A JP2001097814A JP4705727B2 JP 4705727 B2 JP4705727 B2 JP 4705727B2 JP 2001097814 A JP2001097814 A JP 2001097814A JP 2001097814 A JP2001097814 A JP 2001097814A JP 4705727 B2 JP4705727 B2 JP 4705727B2
Authority
JP
Japan
Prior art keywords
pulse detonation
augmentor
engine
turbofan engine
assembly
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 - Fee Related
Application number
JP2001097814A
Other languages
English (en)
Japanese (ja)
Other versions
JP2001355515A (ja
JP2001355515A5 (enExample
Inventor
ジェームズ・エドワード・ジョンソン
ローレンス・ウェイン・ダンバー
ローレンス・バトラー
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of JP2001355515A publication Critical patent/JP2001355515A/ja
Publication of JP2001355515A5 publication Critical patent/JP2001355515A5/ja
Application granted granted Critical
Publication of JP4705727B2 publication Critical patent/JP4705727B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

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
    • F02K7/06—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 with combustion chambers having valves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/075—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type controlling flow ratio between flows

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)
JP2001097814A 2000-03-31 2001-03-30 複合サイクル・パルスデトネーション・タービンエンジン Expired - Fee Related JP4705727B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/540566 2000-03-31
US09/540,566 US6442930B1 (en) 2000-03-31 2000-03-31 Combined cycle pulse detonation turbine engine

Publications (3)

Publication Number Publication Date
JP2001355515A JP2001355515A (ja) 2001-12-26
JP2001355515A5 JP2001355515A5 (enExample) 2008-05-08
JP4705727B2 true JP4705727B2 (ja) 2011-06-22

Family

ID=24155993

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2001097814A Expired - Fee Related JP4705727B2 (ja) 2000-03-31 2001-03-30 複合サイクル・パルスデトネーション・タービンエンジン

Country Status (3)

Country Link
US (2) US6442930B1 (enExample)
EP (1) EP1138922A1 (enExample)
JP (1) JP4705727B2 (enExample)

Families Citing this family (71)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6666018B2 (en) * 2000-03-31 2003-12-23 General Electric Company Combined cycle pulse detonation turbine engine
US6868665B2 (en) * 2001-12-21 2005-03-22 General Electric Company Methods and apparatus for operating gas turbine engines
US6877310B2 (en) 2002-03-27 2005-04-12 General Electric Company Shock wave reflector and detonation chamber
US6725646B2 (en) 2002-04-10 2004-04-27 Caterpillar Inc Rotary pulse detonation engine
US6813878B2 (en) * 2002-12-11 2004-11-09 General Electric Company Methods and apparatus for operating gas turbine engines
US6883302B2 (en) * 2002-12-20 2005-04-26 General Electric Company Methods and apparatus for generating gas turbine engine thrust with a pulse detonation thrust augmenter
US6901738B2 (en) * 2003-06-26 2005-06-07 United Technologies Corporation Pulsed combustion turbine engine
US7047724B2 (en) * 2002-12-30 2006-05-23 United Technologies Corporation Combustion ignition
US6857261B2 (en) * 2003-01-07 2005-02-22 Board Of Regents, The University Of Texas System Multi-mode pulsed detonation propulsion system
US7200538B2 (en) * 2003-01-15 2007-04-03 General Electric Company Methods and apparatus for modeling gas turbine engines
WO2004072451A1 (en) 2003-02-12 2004-08-26 Ishikawajima-Harima Heavy Industries Co., Ltd. Pulse detonation engine system for driving turbine
US6928804B2 (en) * 2003-03-06 2005-08-16 General Electric Company Pulse detonation system for a gas turbine engine
RU2311555C2 (ru) * 2003-04-28 2007-11-27 Владимир Николаевич Костюков Пульсирующий газотурбинный двигатель
US7055308B2 (en) 2003-05-30 2006-06-06 General Electric Company Detonation damper for pulse detonation engines
US6983586B2 (en) * 2003-12-08 2006-01-10 General Electric Company Two-stage pulse detonation system
JP3952202B2 (ja) 2004-02-19 2007-08-01 独立行政法人 宇宙航空研究開発機構 パルスデトネーションエンジン
US6983601B2 (en) * 2004-05-28 2006-01-10 General Electric Company Method and apparatus for gas turbine engines
US7200987B2 (en) * 2004-06-18 2007-04-10 General Electric Company Off-axis pulse detonation configuration for gas turbine engine
JP4256820B2 (ja) * 2004-06-29 2009-04-22 三菱重工業株式会社 デトネーションエンジンおよびこれを備えた飛行体
US7228683B2 (en) * 2004-07-21 2007-06-12 General Electric Company Methods and apparatus for generating gas turbine engine thrust using a pulse detonator
US7174704B2 (en) * 2004-07-23 2007-02-13 General Electric Company Split shroud exhaust nozzle
US7100377B2 (en) * 2004-08-30 2006-09-05 General Electric Company Methods for operating gas turbine engines
US7093446B2 (en) * 2004-09-15 2006-08-22 General Electric Company Gas turbine engine having improved core system
US7096674B2 (en) * 2004-09-15 2006-08-29 General Electric Company High thrust gas turbine engine with improved core system
US20060053801A1 (en) * 2004-09-15 2006-03-16 Orlando Robert J Cooling system for gas turbine engine having improved core system
US7140174B2 (en) * 2004-09-30 2006-11-28 General Electric Company Methods and apparatus for assembling a gas turbine engine
US7188467B2 (en) * 2004-09-30 2007-03-13 General Electric Company Methods and apparatus for assembling a gas turbine engine
US7818956B2 (en) * 2005-05-13 2010-10-26 General Electric Company Pulse detonation assembly and hybrid engine
US7828546B2 (en) * 2005-06-30 2010-11-09 General Electric Company Naturally aspirated fluidic control for diverting strong pressure waves
WO2007008112A1 (fr) * 2005-07-13 2007-01-18 Kostioukov Vladimir Nikolaevic Moteur a turbine a gaz pulse
RU2362033C2 (ru) * 2005-07-13 2009-07-20 Владимир Николаевич Костюков Пульсирующий газотурбинный эжекторный двигатель (варианты)
RU2362034C2 (ru) * 2006-03-06 2009-07-20 Владимир Николаевич Костюков Пульсирующий газотурбинный двигатель (варианты)
US7526912B2 (en) 2005-10-31 2009-05-05 General Electric Company Pulse detonation engines and components thereof
US7966803B2 (en) * 2006-02-03 2011-06-28 General Electric Company Pulse detonation combustor with folded flow path
US7784265B2 (en) 2006-02-07 2010-08-31 General Electric Company Multiple tube pulse detonation engine turbine apparatus and system
US7752835B2 (en) 2006-06-01 2010-07-13 United Technologies Corporation Pulsed combustion engine
US7797943B2 (en) * 2006-10-18 2010-09-21 Aerojet-General Corporation Core burning for scramjet engines
US7841167B2 (en) * 2006-11-17 2010-11-30 General Electric Company Pulse detonation engine bypass and cooling flow with downstream mixing volume
US8082725B2 (en) * 2007-04-12 2011-12-27 General Electric Company Electro-dynamic swirler, combustion apparatus and methods using the same
US20080310984A1 (en) * 2007-06-12 2008-12-18 General Electric Company Positive displacement capture device
US20080310981A1 (en) * 2007-06-12 2008-12-18 General Electric Company Positive displacement flow separator
US8146371B2 (en) * 2007-12-21 2012-04-03 United Technologies Corporation Direct induction combustor/generator
US8205433B2 (en) * 2008-08-21 2012-06-26 Lockheed Martin Corporation Pulse detonation/deflagration apparatus and related methods for enhancing DDT wave production
US8157503B2 (en) * 2008-09-22 2012-04-17 Rolls Royce Corporation Thermal management system
US8302377B2 (en) * 2009-01-30 2012-11-06 General Electric Company Ground-based simple cycle pulse detonation combustor based hybrid engine for power generation
US8429893B2 (en) * 2009-08-11 2013-04-30 Northrop Grumman Corporation Airflow modulation for dual mode combined cycle propulsion systems
JP5764131B2 (ja) 2009-09-23 2015-08-12 エアロジェット ロケットダイン オブ ディーイー，インコーポレイテッド 一過性プラズマを用いて連続爆轟波を維持するための燃焼システムおよびその方法
DE202009013789U1 (de) 2009-10-09 2010-03-04 Kostiukov, Vladimir Nikolaevich Pulsierender Motor
US8978387B2 (en) 2010-12-21 2015-03-17 General Electric Company Hot gas path component cooling for hybrid pulse detonation combustion systems
FR2975434B1 (fr) * 2011-05-16 2015-08-14 Mbda France Turbomachine a chambre de detonation et engin volant pourvu d'une telle turbomachine
DE202012013035U1 (de) 2011-12-14 2014-08-01 Vladimir Nikolaevich Kostyukov Turbo-Rotor-Triebwerk
RU2553589C2 (ru) * 2012-08-28 2015-06-20 Открытое акционерное общество "Научно-производственное объединение "Сатурн" Способ функционирования сверхзвукового пульсирующего детонационного прямоточного воздушно-реактивного двигателя
US10371090B2 (en) 2014-01-13 2019-08-06 United Technologies Corporation Variable area exhaust mixer for a gas turbine engine
US10030606B2 (en) 2014-01-27 2018-07-24 United Technologies Corporation Variable exhaust mixer and cooler for a three-stream gas turbine engine
CN104110326B (zh) * 2014-07-02 2016-06-29 北京航空航天大学 一种新概念高速飞行器推进系统布局方法
WO2016157224A1 (en) * 2015-04-03 2016-10-06 MAUTONE BARROS, Jose Eduardo Engine for hypersonic aircrafts with supersonic combustor
CH714304A1 (de) * 2017-11-06 2019-05-15 Explotechnik AG Pulsantrieb.
RU2693948C1 (ru) * 2018-02-27 2019-07-08 Виталий Иванович Коминов Газотурбинный двигатель
US11236908B2 (en) 2018-10-24 2022-02-01 General Electric Company Fuel staging for rotating detonation combustor
US11371711B2 (en) 2018-11-28 2022-06-28 General Electric Company Rotating detonation combustor with offset inlet
US11105511B2 (en) 2018-12-14 2021-08-31 General Electric Company Rotating detonation propulsion system
CN110131074B (zh) * 2019-05-24 2020-06-30 西安航天动力研究所 一种双组元空气涡轮火箭推进系统
US11572840B2 (en) * 2019-12-03 2023-02-07 General Electric Company Multi-mode combustion control for a rotating detonation combustion system
CN111271192A (zh) * 2020-02-02 2020-06-12 西北工业大学 一种基于脉冲爆震的空气涡轮火箭发动机
CN111305972A (zh) * 2020-03-28 2020-06-19 西北工业大学 一种脉冲爆震燃烧室及基于脉冲爆震的空气涡轮火箭发动机
CN112240568B (zh) * 2020-09-11 2022-10-28 北京动力机械研究所 一种用于加热器稳定燃烧的水冷筒形整流器
CN112901344B (zh) * 2021-01-26 2022-04-01 厦门大学 级间旋转爆震变循环涡轴发动机
US12078357B2 (en) 2022-12-09 2024-09-03 General Electric Company Rotating detonation-enabled augmentor systems
CN116220943B (zh) * 2022-12-26 2025-10-10 清航空天(北京)科技有限公司 组合发动机系统、航空航天飞行器及飞行控制方法、装置
US12065965B1 (en) 2023-08-15 2024-08-20 Rolls-Royce North American Technologies Inc. Rotating detonation augmentors with adjustable throats for gas turbine engines
US12352224B2 (en) 2023-10-05 2025-07-08 General Electric Company Serial rotating detonation combustor systems

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB586572A (en) * 1943-08-11 1947-03-24 David Macleish Smith Improvements in internal combustion turbine plant for propulsion by jet action, at least in part
BE462134A (enExample) * 1944-03-16
US2635420A (en) * 1947-05-14 1953-04-21 Shell Dev Jet propulsion engine with auxiliary pulse jet engine
DE2046079B1 (de) * 1970-09-18 1971-12-23 Messerschmitt Bolkow Blohm GmbH, 8000 München Luftatmendes strahlrohr
WO1987006976A1 (fr) 1986-05-14 1987-11-19 Daniel Buchser Statoreacteur
US4947641A (en) * 1988-06-23 1990-08-14 Sundstrand Corporation Pulse accelerating turbine
US5694768A (en) 1990-02-23 1997-12-09 General Electric Company Variable cycle turbofan-ramjet engine
US5345758A (en) 1993-04-14 1994-09-13 Adroit Systems, Inc. Rotary valve multiple combustor pulse detonation engine
US5873240A (en) 1993-04-14 1999-02-23 Adroit Systems, Inc. Pulsed detonation rocket engine

Also Published As

Publication number Publication date
JP2001355515A (ja) 2001-12-26
US6550235B2 (en) 2003-04-22
US20030029160A1 (en) 2003-02-13
EP1138922A1 (en) 2001-10-04
US6442930B1 (en) 2002-09-03

Similar Documents

Publication Publication Date Title
JP4705727B2 (ja) 複合サイクル・パルスデトネーション・タービンエンジン
US6666018B2 (en) Combined cycle pulse detonation turbine engine
JP4471644B2 (ja) ガスタービンエンジン推力を発生するための方法及び装置
CN100404839C (zh) 尾部flade发动机
CN109028142B (zh) 推进系统及操作其的方法
US5694768A (en) Variable cycle turbofan-ramjet engine
US10641169B2 (en) Hybrid combustor assembly and method of operation
US7475545B2 (en) Fladed supersonic missile turbojet
JP5220400B2 (ja) ダクト燃焼式混成流ターボファン
US7509797B2 (en) Thrust vectoring missile turbojet
CN114746700B (zh) 旋转爆震燃烧和热交换器系统
JPH0367026A (ja) ターボロケットエンジンとラムジェットエンジンとを組合わせた再燃焼形推進機
US20210140641A1 (en) Method and system for rotating detonation combustion
US20180356099A1 (en) Bulk swirl rotating detonation propulsion system
US6889505B2 (en) Pulse detonation system for a gas turbine engine
US6868665B2 (en) Methods and apparatus for operating gas turbine engines
CA2520471C (en) Methods and apparatus for assembling a gas turbine engine
US20220389884A1 (en) Variable cycle jet engine
JP5000101B2 (ja) ガスタービンエンジン推力を発生させるための方法及び装置
US6904750B2 (en) Integral pulse detonation system for a gas turbine engine
RU173530U1 (ru) Силовая установка гиперзвукового летательного аппарата
RU174498U1 (ru) Силовая установка гиперзвукового летательного аппарата

Legal Events

Date Code Title Description
A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20080326

A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20080326

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20100525

A601 Written request for extension of time

Free format text: JAPANESE INTERMEDIATE CODE: A601

Effective date: 20100820

RD02 Notification of acceptance of power of attorney

Free format text: JAPANESE INTERMEDIATE CODE: A7422

Effective date: 20100820

RD04 Notification of resignation of power of attorney

Free format text: JAPANESE INTERMEDIATE CODE: A7424

Effective date: 20100820

A602 Written permission of extension of time

Free format text: JAPANESE INTERMEDIATE CODE: A602

Effective date: 20100825

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20101124

A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20110215

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20110314

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

LAPS Cancellation because of no payment of annual fees