JP6527875B2 - ディーゼル機関の衝突・分流燃焼室 - Google Patents
ディーゼル機関の衝突・分流燃焼室 Download PDFInfo
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- JP6527875B2 JP6527875B2 JP2016549578A JP2016549578A JP6527875B2 JP 6527875 B2 JP6527875 B2 JP 6527875B2 JP 2016549578 A JP2016549578 A JP 2016549578A JP 2016549578 A JP2016549578 A JP 2016549578A JP 6527875 B2 JP6527875 B2 JP 6527875B2
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- 238000002485 combustion reaction Methods 0.000 title claims description 99
- 239000000446 fuel Substances 0.000 claims description 66
- 238000002347 injection Methods 0.000 claims description 21
- 239000007924 injection Substances 0.000 claims description 21
- 238000000889 atomisation Methods 0.000 claims description 9
- 238000010586 diagram Methods 0.000 description 17
- 230000007704 transition Effects 0.000 description 15
- 239000007921 spray Substances 0.000 description 14
- 239000000203 mixture Substances 0.000 description 5
- 239000006229 carbon black Substances 0.000 description 4
- 239000008240 homogeneous mixture Substances 0.000 description 4
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 230000008021 deposition Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000003116 impacting effect Effects 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0618—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion
- F02B23/0624—Swirl flow
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0618—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion
- F02B23/0621—Squish flow
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0645—Details related to the fuel injector or the fuel spray
- F02B23/0648—Means or methods to improve the spray dispersion, evaporation or ignition
- F02B23/0651—Means or methods to improve the spray dispersion, evaporation or ignition the fuel spray impinging on reflecting surfaces or being specially guided throughout the combustion space
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0645—Details related to the fuel injector or the fuel spray
- F02B23/0669—Details related to the fuel injector or the fuel spray having multiple fuel spray jets per injector nozzle
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0696—W-piston bowl, i.e. the combustion space having a central projection pointing towards the cylinder head and the surrounding wall being inclined towards the cylinder wall
-
- 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
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Dispersion Chemistry (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
- Pistons, Piston Rings, And Cylinders (AREA)
Description
2 シリンダライナ
3 ピストン
4 燃焼室
5 燃料噴射装置
6 霧状燃料
7 燃焼室頂面隙間部
8 燃焼室中央部
9 衝突環状帯部
10 上部ガイド凸面
11 衝突傾斜面
12 衝突凸面
13 衝突凹面
14 第1衝突錐面
14a 第1上部衝突傾斜面
14b 第1衝突移行曲面
14c 第1下部衝突傾斜面
15 第2衝突錐面
15a 第2上部衝突傾斜面
15b 第2衝突移行曲面
15c 第2下部衝突凹面
16 衝突曲面
16a 上部衝突凸面
16b 下部衝突凹面
17 上部ガイド平滑面
18 下部ガイド平滑面
19 下部ガイド曲面
20 下部ガイド直角円弧面
21 下部ガイド凹面
22 第1頂面隙間ガイド傾斜面
23 第2頂面隙間ガイド傾斜面
24 第1頂面隙間ガイド面
24a 第1頂面隙間ガイド凹面
24b 第3頂面隙間ガイド傾斜面
25 第2頂面隙間ガイド面
25a 第2頂面隙間ガイド凹面
25b 第4頂面隙間ガイド傾斜面
26 第3頂面隙間ガイド面
26a 頂面隙間ガイド移行面
26b 第5頂面隙間ガイド傾斜面
26c 頂面隙間移行面
26d 第6頂面隙間ガイド傾斜面
27 ω形底面
28 浅皿形底面
Claims (3)
- 燃料噴射装置(5)はマルチポイント式で高圧燃料を霧状でシリンダヘッド(1)とシリンダライナ(2)とピストン(3)とから成る燃焼室(4)内に噴射し、前記燃焼室(4)に衝突環状帯部(9)を設け、前記燃焼室(4)を燃焼室頂面隙間部(7)と燃焼室中央部(8)という2つの領域に分け、前記燃焼室頂面隙間部(7)の直径D2が気筒直径とし;前記燃料噴射装置(5)から噴出した霧状燃料(6)を衝突環状帯部(9)上に噴射し、一部の燃料が反発されて二次霧化を行い、一部の燃料が前記衝突環状帯部(9)に沿って各々前記燃焼室頂面隙間部(7)及び前記燃焼室中央部(8)に流れ、油気のより一層均一な混合を実現するディーゼル機関の衝突・分流燃焼室であって、前記衝突環状帯部(9)は衝突面と衝突上部ガイド面と衝突下部ガイド面とを含み;前記衝突面は、衝突傾斜面(11)を用い、前記衝突傾斜面(11)に応じて前記燃焼室頂面隙間部(7)及び前記燃焼室中央部(8)の燃料分布比率が決定され;前記衝突上部ガイド面は、上部ガイド凸面(10)を用い;前記上部ガイド凸面(10)がピストン頂面隙間面より高い構成であって、前記ピストン頂面隙間面は、前記衝突上部ガイド面から外周に向かって漸次低く傾斜する傾斜面であり、前記衝突下部ガイド面は、下部ガイド平滑面(18)、下部ガイド曲面(19)、下部ガイド直角円弧面(20)或いは下部ガイド凹面(21)を用い、
前記衝突環状帯部(9)の頂部は前記ピストン頂面隙間面よりも突出し、前記衝突環状帯部(9)の直径が前記衝突環状帯部(9)の頂部で囲まれた領域である喉部の直径D1よりも大きいことを特徴とするディーゼル機関の衝突・分流燃焼室。 - 燃料噴射装置(5)はマルチポイント式で高圧燃料を霧状でシリンダヘッド(1)とシリンダライナ(2)とピストン(3)とから成る燃焼室(4)内に噴射し、前記燃焼室(4)に衝突環状帯部(9)を設け、前記燃焼室(4)を燃焼室頂面隙間部(7)と燃焼室中央部(8)という2つの領域に分け、前記燃焼室頂面隙間部(7)の直径D2が気筒直径とし;前記燃料噴射装置(5)から噴出した霧状燃料(6)を衝突環状帯部(9)上に噴射し、一部の燃料が反発されて二次霧化を行い、一部の燃料が前記衝突環状帯部(9)に沿って各々前記燃焼室頂面隙間部(7)及び前記燃焼室中央部(8)に流れ、油気のより一層均一な混合を実現するディーゼル機関の衝突・分流燃焼室であって、前記衝突環状帯部(9)は衝突面と衝突上部ガイド面と衝突下部ガイド面とを含み;前記衝突面は、第2衝突錐面(15)を用い、第2衝突錐面(15)に応じて前記燃焼室頂面隙間部(7)及び前記燃焼室中央部(8)の燃料分布比率が決定され;前記第2衝突錐面(15)の構造が第2上部衝突傾斜面(15a)と第2衝突移行曲面(15b)と第2下部衝突凹面(15c)とを含み;前記衝突上部ガイド面は、上部ガイド凸面(10)を用い;前記上部ガイド凸面(10)がピストン頂面隙間面より高い構成であって、前記ピストン頂面隙間面は、前記衝突上部ガイド面から外周に向かって漸次低く傾斜する傾斜面であり、前記衝突下部ガイド面は、下部ガイド平滑面(18)、下部ガイド曲面(19)、下部ガイド直角円弧面(20)或いは下部ガイド凹面(21)を用い、
前記衝突環状帯部(9)の頂部は前記ピストン頂面隙間面よりも突出し、前記衝突環状帯部(9)の直径が前記衝突環状帯部(9)の頂部で囲まれた領域である喉部の直径D1よりも大きいことを特徴とするディーゼル機関の衝突・分流燃焼室。 - 燃料噴射装置(5)はマルチポイント式で高圧燃料を霧状でシリンダヘッド(1)とシリンダライナ(2)とピストン(3)とから成る燃焼室(4)内に噴射し、前記燃焼室(4)に衝突環状帯部(9)を設け、前記燃焼室(4)を燃焼室頂面隙間部(7)と燃焼室中央部(8)という2つの領域に分け、前記燃焼室頂面隙間部(7)の直径D2が気筒直径とし;前記燃料噴射装置(5)から噴出した霧状燃料(6)を衝突環状帯部(9)上に噴射し、一部の燃料が反発されて二次霧化を行い、一部の燃料が前記衝突環状帯部(9)に沿って各々前記燃焼室頂面隙間部(7)及び前記燃焼室中央部(8)に流れ、油気のより一層均一な混合を実現するディーゼル機関の衝突・分流燃焼室であって、前記衝突環状帯部(9)は衝突面と衝突上部ガイド面と衝突下部ガイド面とを含み;前記衝突面は、衝突凹面(13)を用い、前記衝突凹面(13)に応じて前記燃焼室頂面隙間部(7)及び前記燃焼室中央部(8)の燃料分布比率が決定され;前記衝突上部ガイド面は、上部ガイド凸面(10)を用い;前記上部ガイド凸面(10)がピストン頂面隙間面より高い構成であって、前記ピストン頂面隙間面は、前記衝突上部ガイド面から外周に向かって漸次低く傾斜する傾斜面であり、前記衝突下部ガイド面は、下部ガイド平滑面(18)、下部ガイド曲面(19)、下部ガイド直角円弧面(20)或いは下部ガイド凹面(21)を用い、
前記衝突環状帯部(9)の頂部は前記ピストン頂面隙間面よりも突出し、前記衝突環状帯部(9)の直径が前記衝突環状帯部(9)の頂部で囲まれた領域である喉部の直径D1よりも大きいことを特徴とするディーゼル機関の衝突・分流燃焼室。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
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CN201410061414.5A CN103835803B (zh) | 2014-02-24 | 2014-02-24 | 柴油机碰撞分流燃烧室 |
CN201410061414.5 | 2014-02-24 | ||
PCT/CN2015/000103 WO2015124038A1 (zh) | 2014-02-24 | 2015-02-16 | 柴油机碰撞分流燃烧室 |
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JP2017512273A JP2017512273A (ja) | 2017-05-18 |
JP6527875B2 true JP6527875B2 (ja) | 2019-06-05 |
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US (1) | US20160363042A1 (ja) |
JP (1) | JP6527875B2 (ja) |
CN (1) | CN103835803B (ja) |
WO (1) | WO2015124038A1 (ja) |
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JP6197750B2 (ja) * | 2014-06-09 | 2017-09-20 | マツダ株式会社 | ディーゼルエンジンの燃焼室構造 |
JP6160564B2 (ja) * | 2014-06-09 | 2017-07-12 | マツダ株式会社 | ディーゼルエンジン |
-
2014
- 2014-02-24 CN CN201410061414.5A patent/CN103835803B/zh active Active
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2015
- 2015-02-16 JP JP2016549578A patent/JP6527875B2/ja active Active
- 2015-02-16 WO PCT/CN2015/000103 patent/WO2015124038A1/zh active Application Filing
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2016
- 2016-08-24 US US15/245,215 patent/US20160363042A1/en not_active Abandoned
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US20160363042A1 (en) | 2016-12-15 |
CN103835803A (zh) | 2014-06-04 |
JP2017512273A (ja) | 2017-05-18 |
CN103835803B (zh) | 2016-02-24 |
WO2015124038A1 (zh) | 2015-08-27 |
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