JP6170438B2 - エンジンおよび燃焼システム - Google Patents
エンジンおよび燃焼システム Download PDFInfo
- Publication number
- JP6170438B2 JP6170438B2 JP2013547610A JP2013547610A JP6170438B2 JP 6170438 B2 JP6170438 B2 JP 6170438B2 JP 2013547610 A JP2013547610 A JP 2013547610A JP 2013547610 A JP2013547610 A JP 2013547610A JP 6170438 B2 JP6170438 B2 JP 6170438B2
- Authority
- JP
- Japan
- Prior art keywords
- combustion
- flow
- channel
- engine
- individual
- 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
Links
- 238000002485 combustion reaction Methods 0.000 title claims description 322
- 230000009467 reduction Effects 0.000 claims description 38
- 230000001419 dependent effect Effects 0.000 claims description 27
- 238000005474 detonation Methods 0.000 claims description 18
- 239000012530 fluid Substances 0.000 claims description 14
- 239000000446 fuel Substances 0.000 claims description 5
- 230000007704 transition Effects 0.000 claims description 5
- 238000011144 upstream manufacturing Methods 0.000 claims description 5
- 230000001133 acceleration Effects 0.000 claims description 3
- 238000004891 communication Methods 0.000 claims description 3
- 238000000465 moulding Methods 0.000 claims description 2
- 230000001902 propagating effect Effects 0.000 claims 1
- 230000001052 transient effect Effects 0.000 description 8
- 230000008901 benefit Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 239000007800 oxidant agent Substances 0.000 description 3
- 230000001590 oxidative effect Effects 0.000 description 3
- 230000000750 progressive effect Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 239000000284 extract Substances 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 230000001141 propulsive effect Effects 0.000 description 1
- 230000003252 repetitive effect Effects 0.000 description 1
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
- F23R7/00—Intermittent or explosive combustion chambers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
- F23M9/00—Baffles or deflectors for air or combustion products; Flame shields
- F23M9/06—Baffles or deflectors for air or combustion products; Flame shields in fire-boxes
-
- 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
- F23R3/002—Wall structures
-
- 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
-
- 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
-
- 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
- F23R3/56—Combustion chambers having rotary flame tubes
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 (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US201061427584P | 2010-12-28 | 2010-12-28 | |
| US61/427,584 | 2010-12-28 | ||
| PCT/US2011/067373 WO2012092264A1 (en) | 2010-12-28 | 2011-12-27 | Engine and combustion system |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2014501380A JP2014501380A (ja) | 2014-01-20 |
| JP2014501380A5 JP2014501380A5 (https=) | 2015-02-19 |
| JP6170438B2 true JP6170438B2 (ja) | 2017-07-26 |
Family
ID=46383498
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2013547610A Expired - Fee Related JP6170438B2 (ja) | 2010-12-28 | 2011-12-27 | エンジンおよび燃焼システム |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US9027324B2 (https=) |
| EP (1) | EP2659187B1 (https=) |
| JP (1) | JP6170438B2 (https=) |
| WO (1) | WO2012092264A1 (https=) |
Families Citing this family (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9719678B2 (en) * | 2010-09-22 | 2017-08-01 | The United States Of America, As Represented By The Secretary Of The Navy | Apparatus methods and systems of unidirectional propagation of gaseous detonations |
| EP2971514B1 (en) | 2013-03-15 | 2020-07-22 | Rolls-Royce North American Technologies, Inc. | Continuous detonation combustion engine and system |
| WO2015200346A1 (en) | 2014-06-23 | 2015-12-30 | Air Products And Chemicals, Inc. | Solid fuel burner and method of operating |
| EP3062023A1 (en) | 2015-02-20 | 2016-08-31 | Rolls-Royce North American Technologies, Inc. | Wave rotor with piston assembly |
| US10393383B2 (en) | 2015-03-13 | 2019-08-27 | Rolls-Royce North American Technologies Inc. | Variable port assemblies for wave rotors |
| CN106438014B (zh) * | 2016-08-26 | 2019-06-18 | 南京航空航天大学 | 一种内燃波转子强化燃烧装置 |
| US10520195B2 (en) * | 2017-06-09 | 2019-12-31 | General Electric Company | Effervescent atomizing structure and method of operation for rotating detonation propulsion system |
| US10969107B2 (en) | 2017-09-15 | 2021-04-06 | General Electric Company | Turbine engine assembly including a rotating detonation combustor |
| US11149954B2 (en) | 2017-10-27 | 2021-10-19 | General Electric Company | Multi-can annular rotating detonation combustor |
| US11473780B2 (en) | 2018-02-26 | 2022-10-18 | General Electric Company | Engine with rotating detonation combustion system |
| US11320147B2 (en) | 2018-02-26 | 2022-05-03 | General Electric Company | Engine with rotating detonation combustion system |
| US11619172B1 (en) * | 2022-03-01 | 2023-04-04 | General Electric Company | Detonation combustion systems |
| US12037962B1 (en) | 2023-03-07 | 2024-07-16 | General Electric Company | Airbreathing propulsion engines including rotating detonation and bluff body systems |
| US12510249B2 (en) | 2023-06-20 | 2025-12-30 | Pratt & Whitney Canada Corp. | Auxiliary power unit with pulse detonation combustion |
| 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 |
Family Cites Families (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3315468A (en) * | 1965-10-01 | 1967-04-25 | Gen Electric | Cooled flameholder assembly |
| US5203796A (en) | 1990-08-28 | 1993-04-20 | General Electric Company | Two stage v-gutter fuel injection mixer |
| JPH06280679A (ja) * | 1993-03-26 | 1994-10-04 | Ishikawajima Harima Heavy Ind Co Ltd | 燃焼器とその保炎方法 |
| DE9306924U1 (de) * | 1993-05-07 | 1993-12-16 | Grace Gmbh, 22844 Norderstedt | Vorrichtung zum Verbrennen oxidierbarer Bestandteile in einem zu reinigenden Trägergas |
| US5494438A (en) | 1994-02-08 | 1996-02-27 | National Science Council | Sudden expansion combustion chamber with slotted inlet port |
| US5512250A (en) * | 1994-03-02 | 1996-04-30 | Catalytica, Inc. | Catalyst structure employing integral heat exchange |
| US6877310B2 (en) * | 2002-03-27 | 2005-04-12 | General Electric Company | Shock wave reflector and detonation chamber |
| US7137243B2 (en) * | 2002-07-03 | 2006-11-21 | Rolls-Royce North American Technologies, Inc. | Constant volume combustor |
| US7637096B2 (en) | 2004-11-25 | 2009-12-29 | Rolls-Royce Plc | Pulse jet engine having pressure sensor means for controlling fuel delivery into a combustion chamber |
| JP4729947B2 (ja) * | 2005-03-08 | 2011-07-20 | タマティーエルオー株式会社 | デトネータ |
| US7500348B2 (en) * | 2005-03-24 | 2009-03-10 | United Technologies Corporation | Pulse combustion device |
| US7520123B2 (en) | 2005-05-12 | 2009-04-21 | Lockheed Martin Corporation | Mixing-enhancement inserts for pulse detonation chambers |
| US7828546B2 (en) * | 2005-06-30 | 2010-11-09 | General Electric Company | Naturally aspirated fluidic control for diverting strong pressure waves |
| US7669405B2 (en) * | 2005-12-22 | 2010-03-02 | General Electric Company | Shaped walls for enhancement of deflagration-to-detonation transition |
| US7966803B2 (en) | 2006-02-03 | 2011-06-28 | General Electric Company | Pulse detonation combustor with folded flow path |
| US7669406B2 (en) | 2006-02-03 | 2010-03-02 | General Electric Company | Compact, low pressure-drop shock-driven combustor and rocket booster, pulse detonation based supersonic propulsion system employing the same |
| US7784265B2 (en) | 2006-02-07 | 2010-08-31 | General Electric Company | Multiple tube pulse detonation engine turbine apparatus and system |
| US7758334B2 (en) | 2006-03-28 | 2010-07-20 | Purdue Research Foundation | Valveless pulsed detonation combustor |
| US8881500B2 (en) * | 2010-08-31 | 2014-11-11 | General Electric Company | Duplex tab obstacles for enhancement of deflagration-to-detonation transition |
-
2011
- 2011-12-24 US US13/337,083 patent/US9027324B2/en active Active
- 2011-12-27 JP JP2013547610A patent/JP6170438B2/ja not_active Expired - Fee Related
- 2011-12-27 EP EP11852405.7A patent/EP2659187B1/en not_active Not-in-force
- 2011-12-27 WO PCT/US2011/067373 patent/WO2012092264A1/en not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| WO2012092264A1 (en) | 2012-07-05 |
| EP2659187A4 (en) | 2015-11-11 |
| EP2659187B1 (en) | 2019-05-15 |
| JP2014501380A (ja) | 2014-01-20 |
| US9027324B2 (en) | 2015-05-12 |
| EP2659187A1 (en) | 2013-11-06 |
| US20120216504A1 (en) | 2012-08-30 |
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