CN103134081B - 用于脉冲爆震燃烧器的可变引发位置系统 - Google Patents
用于脉冲爆震燃烧器的可变引发位置系统 Download PDFInfo
- Publication number
- CN103134081B CN103134081B CN201210501257.6A CN201210501257A CN103134081B CN 103134081 B CN103134081 B CN 103134081B CN 201210501257 A CN201210501257 A CN 201210501257A CN 103134081 B CN103134081 B CN 103134081B
- Authority
- CN
- China
- Prior art keywords
- tube
- region
- combustion
- pulse detonation
- initiation
- 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
Links
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
- F23R7/00—Intermittent or explosive combustion chambers
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)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/308,576 US20130139486A1 (en) | 2011-12-01 | 2011-12-01 | Variable initiation location system for pulse detonation combustor |
| US13/308576 | 2011-12-01 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103134081A CN103134081A (zh) | 2013-06-05 |
| CN103134081B true CN103134081B (zh) | 2016-05-11 |
Family
ID=47713762
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210501257.6A Active CN103134081B (zh) | 2011-12-01 | 2012-11-30 | 用于脉冲爆震燃烧器的可变引发位置系统 |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US20130139486A1 (https=) |
| EP (1) | EP2600062A3 (https=) |
| JP (1) | JP6082576B2 (https=) |
| CN (1) | CN103134081B (https=) |
| BR (1) | BR102012030574A2 (https=) |
| CA (1) | CA2796619A1 (https=) |
| IN (1) | IN2012DE03367A (https=) |
Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103438451B (zh) * | 2013-09-11 | 2015-06-17 | 哈尔滨工业大学 | 一种调谐无阀燃气脉动燃烧器 |
| CN103867338B (zh) * | 2014-03-03 | 2016-05-11 | 北京动力机械研究所 | 一种两相高频预爆器 |
| CN110762556B (zh) * | 2019-10-14 | 2020-12-04 | 哈尔滨工程大学 | 气液两相起爆装置 |
| US20240027069A1 (en) * | 2020-03-31 | 2024-01-25 | Mitsubishi Heavy Industries, Ltd. | Combustor for gas turbine and gas turbine |
| US20220252004A1 (en) * | 2021-02-09 | 2022-08-11 | Detonation Space Inc. | Radial pre-detonator |
| CN115218224B (zh) * | 2022-07-29 | 2023-06-20 | 西安热工研究院有限公司 | 一种适用于脉冲爆震燃烧室的冷却结构 |
| CN116147024A (zh) * | 2022-12-15 | 2023-05-23 | 清航空天(北京)科技有限公司 | 一种发动机及其燃烧室结构 |
| US12286952B1 (en) * | 2023-12-18 | 2025-04-29 | Ming Zheng | High-energy remote chamber ignition system |
| CN119063029A (zh) * | 2024-10-18 | 2024-12-03 | 中国航发湖南动力机械研究所 | 一种多管分级爆震燃烧室 |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6662550B2 (en) * | 2002-04-25 | 2003-12-16 | Science Applications International Corporation | Method and apparatus for improving the efficiency of pulsed detonation engines |
| CN101514656A (zh) * | 2009-04-01 | 2009-08-26 | 西北工业大学 | 一种涡轮组合脉冲爆震发动机 |
Family Cites Families (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6062018A (en) * | 1993-04-14 | 2000-05-16 | Adroit Systems, Inc. | Pulse detonation electrical power generation apparatus with water injection |
| 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 |
| US7735311B2 (en) * | 2003-12-09 | 2010-06-15 | Science Applications International Corporation | Pulsed detonation engines manufactured from materials having low thermal stability |
| US20060260291A1 (en) * | 2005-05-20 | 2006-11-23 | General Electric Company | Pulse detonation assembly with cooling enhancements |
| US20090320439A1 (en) * | 2006-01-31 | 2009-12-31 | General Electric Company | Pulsed detonation combustor cleaning device and method of operation |
| US7966803B2 (en) * | 2006-02-03 | 2011-06-28 | General Electric Company | Pulse detonation combustor with folded flow path |
| US7739867B2 (en) * | 2006-02-03 | 2010-06-22 | General Electric Company | Compact, low pressure-drop shock-driven combustor |
| US7841167B2 (en) * | 2006-11-17 | 2010-11-30 | General Electric Company | Pulse detonation engine bypass and cooling flow with downstream mixing volume |
| US20090102203A1 (en) * | 2007-10-23 | 2009-04-23 | Lu Frank K | System and method for power production using a hybrid helical detonation device |
| US20110047962A1 (en) * | 2009-08-28 | 2011-03-03 | General Electric Company | Pulse detonation combustor configuration for deflagration to detonation transition enhancement |
| US20130081376A1 (en) * | 2011-10-03 | 2013-04-04 | Paul Reynolds | Pulse Detonation Engine with Variable Control Piezoelectric Fuel Injector |
-
2011
- 2011-12-01 US US13/308,576 patent/US20130139486A1/en not_active Abandoned
-
2012
- 2012-11-01 IN IN3367DE2012 patent/IN2012DE03367A/en unknown
- 2012-11-22 CA CA2796619A patent/CA2796619A1/en not_active Abandoned
- 2012-11-26 EP EP12194309.6A patent/EP2600062A3/en not_active Withdrawn
- 2012-11-29 JP JP2012260439A patent/JP6082576B2/ja not_active Expired - Fee Related
- 2012-11-30 CN CN201210501257.6A patent/CN103134081B/zh active Active
- 2012-11-30 BR BR102012030574A patent/BR102012030574A2/pt not_active IP Right Cessation
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6662550B2 (en) * | 2002-04-25 | 2003-12-16 | Science Applications International Corporation | Method and apparatus for improving the efficiency of pulsed detonation engines |
| CN101514656A (zh) * | 2009-04-01 | 2009-08-26 | 西北工业大学 | 一种涡轮组合脉冲爆震发动机 |
Also Published As
| Publication number | Publication date |
|---|---|
| EP2600062A2 (en) | 2013-06-05 |
| BR102012030574A2 (pt) | 2015-11-03 |
| CA2796619A1 (en) | 2013-06-01 |
| JP6082576B2 (ja) | 2017-02-15 |
| EP2600062A3 (en) | 2017-11-15 |
| CN103134081A (zh) | 2013-06-05 |
| US20130139486A1 (en) | 2013-06-06 |
| IN2012DE03367A (https=) | 2015-06-19 |
| JP2013117370A (ja) | 2013-06-13 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103134082B (zh) | 用于在脉冲爆震燃烧器操作期间定位爆震转变的方法 | |
| CN103134081B (zh) | 用于脉冲爆震燃烧器的可变引发位置系统 | |
| US8650856B2 (en) | Fluidic deflagration-to-detonation initiation obstacles | |
| Yang et al. | Experimental research on initiation characteristics of a rotating detonation engine | |
| US8683780B2 (en) | Gas turbine engine and pulse detonation combustion system | |
| US8539752B2 (en) | Integrated deflagration-to-detonation obstacles and cooling fluid flow | |
| US7966803B2 (en) | Pulse detonation combustor with folded flow path | |
| US7669405B2 (en) | Shaped walls for enhancement of deflagration-to-detonation transition | |
| JP5121540B2 (ja) | 電気力学的スワラ、燃焼装置 | |
| JP6238997B2 (ja) | 圧力ゲイン燃焼装置及び方法 | |
| US5513489A (en) | Rotary valve multiple combustor pulse detonation engine | |
| EP2559939A2 (en) | Pulse detonation combustor with plenum | |
| JP2011047638A (ja) | デフラグレーションからデトネーションへの遷移を向上させるためのパルスデトネーション燃焼器構成 | |
| US10221763B2 (en) | Combustor for rotating detonation engine and method of operating same | |
| US7669406B2 (en) | Compact, low pressure-drop shock-driven combustor and rocket booster, pulse detonation based supersonic propulsion system employing the same | |
| US20120102916A1 (en) | Pulse Detonation Combustor Including Combustion Chamber Cooling Assembly | |
| US7980056B2 (en) | Methods and apparatus for controlling air flow within a pulse detonation engine | |
| US7634904B2 (en) | Methods and apparatus to facilitate generating power from a turbine engine | |
| Assiz et al. | Design, Analysis and Qualification of Hydrogen-Oxygen Based Gaseous Igniter | |
| WO2011131493A2 (en) | Air breathing reaction propulsion engine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |