JP6465208B2 - エンジン後部構造 - Google Patents
エンジン後部構造 Download PDFInfo
- Publication number
- JP6465208B2 JP6465208B2 JP2017524175A JP2017524175A JP6465208B2 JP 6465208 B2 JP6465208 B2 JP 6465208B2 JP 2017524175 A JP2017524175 A JP 2017524175A JP 2017524175 A JP2017524175 A JP 2017524175A JP 6465208 B2 JP6465208 B2 JP 6465208B2
- Authority
- JP
- Japan
- Prior art keywords
- angle
- rear structure
- axis
- cone
- duct
- 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.)
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Classifications
-
- 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
- F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
- F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/78—Other construction of jet pipes
-
- 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
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Radar Systems Or Details Thereof (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Nozzles (AREA)
Description
Claims (3)
- 軸を有するジェットエンジンの後部構造であって、
前記軸の周りにダクトを囲み、軸方向に前方および後方に開口したケーシングと、
前記軸に対して第1の角度を成して後方に先細り、尖った後端を有するコーンと、
それぞれ前記コーンから前記ケーシングへ径方向に延び、前記軸を含む面に対して第2の角度を成す正圧面を備えた、一以上のガイドベーンと、
それぞれ前記ダクト内において径方向に延び、それぞれ前記軸を含む面に対して第3の角度を成して後方に向いた一以上の背面を備えた、一以上のスプレイバーと、
それぞれ前記ダクト内において径方向に延び、それぞれ前記軸を含む面に対して第4の角度を成して後方に向いた一以上の内面を備えた、一以上のフレイムホルダと、
を備えた後部構造であって、
前記第1ないし第4の角度は、いずれも0度を超えて45度未満であり、
前記第1ないし第4の角度は同一である、後部構造。 - 請求項1の後部構造であって、前記軸方向に後方から見て、前記スプレイバーは前記背面のみが露出しており、前記フレイムホルダは前記内面のみが露出している、後部構造。
- 請求項1の後部構造であって、前記軸方向に後方から見て、前記コーン、前記ガイドベーン、前記スプレイバー、および前記フレイムホルダが露出する面積は、前記ダクトの断面積の50%を超えている、後部構造。
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/JP2015/067280 WO2016203540A1 (ja) | 2015-06-16 | 2015-06-16 | エンジン後部構造 |
Publications (2)
Publication Number | Publication Date |
---|---|
JPWO2016203540A1 JPWO2016203540A1 (ja) | 2017-11-30 |
JP6465208B2 true JP6465208B2 (ja) | 2019-02-06 |
Family
ID=57545153
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2017524175A Active JP6465208B2 (ja) | 2015-06-16 | 2015-06-16 | エンジン後部構造 |
Country Status (5)
Country | Link |
---|---|
US (1) | US10830180B2 (ja) |
EP (1) | EP3244054B1 (ja) |
JP (1) | JP6465208B2 (ja) |
CA (1) | CA2988555C (ja) |
WO (1) | WO2016203540A1 (ja) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114234231B (zh) * | 2021-12-27 | 2022-11-22 | 中国航发沈阳发动机研究所 | 一种兼顾雷达隐身外形的火焰稳定器 |
EP4345003A1 (en) * | 2022-09-29 | 2024-04-03 | HENSOLDT Sensors GmbH | Propulsion system for an aerial vehicle |
CN115653782B (zh) * | 2022-10-13 | 2024-05-03 | 中国航发四川燃气涡轮研究院 | 基于涡扇发动机双腔体结构的隐身喷管结构 |
CN116293820B (zh) * | 2023-04-17 | 2024-06-11 | 中国航发沈阳发动机研究所 | 一种航空发动机加力燃烧室红外辐射信号抑制增强结构 |
Family Cites Families (28)
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FR1063453A (fr) * | 1952-09-18 | 1954-05-04 | Snecma | Perfectionnement aux dispositifs de réglage de la section d'une tuyère, notamment d'une tuyère de réacteur |
GB870268A (en) * | 1957-08-14 | 1961-06-14 | Garrett Corp | Compound gas turbine engine |
US3176465A (en) * | 1962-08-27 | 1965-04-06 | Gen Electric | Vapor fuel injector flameholder |
US5233827A (en) * | 1970-06-08 | 1993-08-10 | General Motors Corporation | Radiation supression |
US3747345A (en) * | 1972-07-24 | 1973-07-24 | United Aircraft Corp | Shortened afterburner construction for turbine engine |
GB1605457A (en) * | 1977-03-05 | 2008-07-16 | Rolls Royce | Improvements in or relating to reheat system for gas turbine engines |
US5203796A (en) * | 1990-08-28 | 1993-04-20 | General Electric Company | Two stage v-gutter fuel injection mixer |
FR2706588B1 (fr) * | 1993-06-16 | 1995-07-21 | Snecma | Système d'injection de carburant pour chambre de combustion. |
JP3387227B2 (ja) | 1994-08-15 | 2003-03-17 | 石川島播磨重工業株式会社 | ターボエンジン |
JPH09256906A (ja) | 1996-03-21 | 1997-09-30 | Ishikawajima Harima Heavy Ind Co Ltd | ジェットエンジンの再熱装置 |
JPH09268947A (ja) * | 1996-04-01 | 1997-10-14 | Ishikawajima Harima Heavy Ind Co Ltd | ジェットエンジンの保炎器 |
JPH11121972A (ja) | 1997-10-09 | 1999-04-30 | Yokohama Rubber Co Ltd:The | 反射電波散乱構造 |
JP4164742B2 (ja) | 2002-10-17 | 2008-10-15 | 株式会社Ihi | マイクロ波反射制御装置 |
US6983601B2 (en) * | 2004-05-28 | 2006-01-10 | General Electric Company | Method and apparatus for gas turbine engines |
JP4546770B2 (ja) | 2004-06-16 | 2010-09-15 | ゼネラル・エレクトリック・カンパニイ | 赤外線を抑制する二次元変向可能単一拡大斜面ノズル |
FR2873411B1 (fr) * | 2004-07-21 | 2009-08-21 | Snecma Moteurs Sa | Turboreacteur avec des moyens de protection pour un dispositif d'injection de carburant, dispositif d'injection et tole de protection pour le turboreacteur |
US7437876B2 (en) * | 2005-03-25 | 2008-10-21 | General Electric Company | Augmenter swirler pilot |
US7596950B2 (en) * | 2005-09-16 | 2009-10-06 | General Electric Company | Augmentor radial fuel spray bar with counterswirling heat shield |
JP2007168491A (ja) | 2005-12-19 | 2007-07-05 | Ishikawajima Harima Heavy Ind Co Ltd | 航空機用インテークダクト |
US7467518B1 (en) * | 2006-01-12 | 2008-12-23 | General Electric Company | Externally fueled trapped vortex cavity augmentor |
US7712315B2 (en) * | 2006-04-20 | 2010-05-11 | United Technologies Corporation | Augmentor variable vane flame stabilization |
FR2928202A1 (fr) * | 2008-02-29 | 2009-09-04 | Snecma Sa | Accroche flamme pour canal de rechauffe d'un turboreacteur avec une semelle d'ecartement, canal de rechauffe et turboreacteur comprenant un canal de rechauffe. |
US9181899B2 (en) | 2008-08-27 | 2015-11-10 | General Electric Company | Variable slope exhaust nozzle |
JP2010112298A (ja) | 2008-11-07 | 2010-05-20 | Ihi Corp | ターボファンエンジン |
JP2010180756A (ja) | 2009-02-04 | 2010-08-19 | Ihi Corp | ジェットエンジン |
JP5573656B2 (ja) * | 2010-12-22 | 2014-08-20 | 株式会社Ihi | アフタバーナ及び航空機エンジン |
JP2013181473A (ja) | 2012-03-02 | 2013-09-12 | Ihi Corp | アフタバーナ及び航空機エンジン |
JP2014070548A (ja) * | 2012-09-28 | 2014-04-21 | Ihi Corp | 再熱装置 |
-
2015
- 2015-06-16 CA CA2988555A patent/CA2988555C/en active Active
- 2015-06-16 WO PCT/JP2015/067280 patent/WO2016203540A1/ja active Application Filing
- 2015-06-16 JP JP2017524175A patent/JP6465208B2/ja active Active
- 2015-06-16 EP EP15895561.7A patent/EP3244054B1/en active Active
-
2017
- 2017-08-08 US US15/671,788 patent/US10830180B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US20170370327A1 (en) | 2017-12-28 |
CA2988555A1 (en) | 2016-12-22 |
CA2988555C (en) | 2019-03-26 |
EP3244054A1 (en) | 2017-11-15 |
EP3244054B1 (en) | 2019-08-21 |
US10830180B2 (en) | 2020-11-10 |
WO2016203540A1 (ja) | 2016-12-22 |
EP3244054A4 (en) | 2018-08-15 |
JPWO2016203540A1 (ja) | 2017-11-30 |
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