JPS59141717A - Piston for use in internal-combustion engine - Google Patents
Piston for use in internal-combustion engineInfo
- Publication number
- JPS59141717A JPS59141717A JP58014918A JP1491883A JPS59141717A JP S59141717 A JPS59141717 A JP S59141717A JP 58014918 A JP58014918 A JP 58014918A JP 1491883 A JP1491883 A JP 1491883A JP S59141717 A JPS59141717 A JP S59141717A
- Authority
- JP
- Japan
- Prior art keywords
- combustion chamber
- piston
- flame
- cavities
- 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.)
- Pending
Links
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 46
- 239000000446 fuel Substances 0.000 claims abstract description 14
- 238000002347 injection Methods 0.000 claims abstract description 8
- 239000007924 injection Substances 0.000 claims abstract description 8
- 238000011144 upstream manufacturing Methods 0.000 claims abstract description 5
- 238000010791 quenching Methods 0.000 abstract description 4
- 230000000171 quenching effect Effects 0.000 abstract description 4
- 239000000779 smoke Substances 0.000 description 3
- 238000004880 explosion Methods 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
Classifications
-
- 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
- F02B23/0645—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
- F02B23/0672—Omega-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 center axis
-
- 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
-
- 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
- F02B2275/00—Other engines, components or details, not provided for in other groups of this subclass
- F02B2275/14—Direct injection into combustion chamber
-
- 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
- F02B3/00—Engines characterised by air compression and subsequent fuel addition
- F02B3/06—Engines characterised by air compression and subsequent fuel addition with compression ignition
-
- 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
Landscapes
- 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)
Abstract
Description
【発明の詳細な説明】
本発明は内燃機関用ビス1〜ンに係り、とくに16部に
オーブンチャンバ型燃焼室を設(」て成るピストンに関
する。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a piston for an internal combustion engine, and more particularly to a piston having an oven chamber type combustion chamber in 16 parts.
直噴型ディーゼルエンジンにおいては、ピストンの頂部
に形成された燃焼室に向けて燃料噴射ノズルから燃料を
噴射して、この燃焼室内において燃焼爆発を起こさ往る
ことによって出力を得るようにしている。すなわち例え
ば第1図に示すようにピストン1の頂部にオープンチャ
ンバ型燃焼室2を形成し、この燃焼室2の内表面に燃料
を@射することによって燃焼爆発を起こさせるようにし
ている。ところが燃焼室2内において生じた火炎は、第
1図において矢印3で示すように燃焼室2の表面に沿つ
C1:方へ移動し、そしてこの燃焼室2からピストン1
の頂部側へ流れる。そしてピストン1のl711?;部
側の温度の低い部分においてクエンチされるために、こ
こで火炎が消滅することになり、この結果不完全燃焼を
起こすことになる。In a direct-injection diesel engine, fuel is injected from a fuel injection nozzle toward a combustion chamber formed at the top of a piston, and combustion explosion occurs within the combustion chamber to obtain output. That is, for example, as shown in FIG. 1, an open chamber type combustion chamber 2 is formed at the top of a piston 1, and fuel is injected onto the inner surface of this combustion chamber 2 to cause a combustion explosion. However, the flame generated in the combustion chamber 2 moves in the direction C1 along the surface of the combustion chamber 2 as shown by the arrow 3 in FIG.
Flows toward the top side. And piston 1 l711? ; Since the flame is quenched in the lower temperature part, the flame is extinguished here, resulting in incomplete combustion.
すなわち第1図に示すにうなオープンチャンバ型の燃1
2室2を備えたピストン1を用いるようにすると、排気
ガス中に炭素分が多くなり、これによって黒煙が11出
されることになる。In other words, an open chamber type fuel 1 as shown in FIG.
If a piston 1 with two chambers 2 is used, the carbon content in the exhaust gas will increase, resulting in black smoke 11 being emitted.
このようなオープンチャンバ型燃焼室の欠点を防lにす
るために、第2図に示すようなりエンドラント型燃焼室
、4を備えたビスI〜ン1が用いられるようになってい
る。この燃焼室4は、その開口縁部にスキッシュリップ
5を形成することによって、ピストン1の頂部に噴出さ
れる火炎の量を少なくし、これにJ:って火炎がビスI
・ン1の外周側の低渇によってり1ンチされないJ、う
にし/、: ’(>のである。ところが燃焼室4の開口
縁部を形成するスキッシュリップ5(よ、その先端の肉
11〕がi9りなっており、しかも^い熱負荷を受ける
ために亀裂を起こし易く、これによって信頼性が低下J
ることになる。In order to avoid such drawbacks of the open chamber type combustion chamber, a screw engine 1 equipped with an end runt type combustion chamber 4 as shown in FIG. 2 has been used. By forming a squish lip 5 on the opening edge of the combustion chamber 4, the amount of flame ejected to the top of the piston 1 is reduced.
・The squish lip 5 that forms the opening edge of the combustion chamber 4 (the flesh 11 at its tip) Since it is exposed to high heat loads, it is prone to cracking, which reduces reliability.
That will happen.
本発明はこのような問題点に鑑みてなされたものであっ
て、火炎のクエンチを防+L L、しかも信頼性の高い
ピストンを112供づることを目的と覆るものである
以下本発明を図示の一実施例につき説明する。The present invention has been made in view of these problems, and aims to provide a highly reliable piston that prevents flame quenching. An example will be explained.
第3図および第4図は本実施例に係るピストン10を示
すものであって、このビス1−ン10の頂部11のほぼ
中央部には、円形を成ザ凹部からなる燃焼室12が形成
されている。この燃焼室12は、基本的にはオーブンチ
ャンバ型になっている。そしてこの燃焼室12の内表面
には、燃131 @lノズル13の噴口と対応するよう
に、噴口と同数の四部14が形成されている。この四部
′14の高さ方向の断面形状は、第5図に示すようにそ
の上端の方が深くなってJ3す、ボケッ1−22を構成
している。これに対して下仝i:側はゆるかな曲線によ
って構成され、燃焼室12の一重部とほぼ連続している
。3 and 4 show a piston 10 according to this embodiment, and a combustion chamber 12 consisting of a circular recess is formed approximately at the center of the top 11 of the piston 10. has been done. This combustion chamber 12 is basically an oven chamber type. On the inner surface of this combustion chamber 12, four parts 14 are formed, the same number of which corresponds to the nozzles of the combustion nozzle 13. As shown in FIG. 5, the cross-sectional shape of the four portions 14 in the height direction is deeper at the upper end to form a bulge 1-22. On the other hand, the lower side is formed by a gentle curve and is almost continuous with the single part of the combustion chamber 12.
そしてこの四部14の上端(J、スワール15の下流側
の方が一1流側よりも低くなっている。また四部14の
円周方向の断面形状は、第6図に示すように円周方向に
対して非対称になっている。すなわf−)スワール15
の上流側が深くなっており、この部分がポケット16を
構成している。またこのピストン10の頂部には、四部
17.1Bによって、一対のバルブを逃げる逃げが形成
されている。The upper end of the fourth part 14 (J) is lower on the downstream side of the swirl 15 than on the eleventh stream side. Also, the cross-sectional shape of the fourth part 14 in the circumferential direction is as shown in FIG. It is asymmetrical with respect to f-) swirl 15
The upstream side of the pocket is deeper, and this portion constitutes the pocket 16. Further, at the top of this piston 10, a relief is formed by a fourth part 17.1B to escape a pair of valves.
以上のようイf構成において、ピストン10の燃焼室1
2のほぼ中火部と対応でる位置に配された燃料噴射ノズ
ル13の噴口から噴射された燃料は、第3図にa3いて
矢印19で示すように燃焼室12の凹部14に°向けて
噴射されることになる。そしてこの燃焼室12内の高温
によって着火されて燃焼を起こず。そしてこの燃焼の際
の火炎は第5図において矢印20で示すように凹部14
の壁面に沿って上昇することになる。四部14の壁面は
、その上端側がボI)ツト22によって深くむ・)でい
るために、この四部14の壁面形状によって火炎20を
燃焼室12の内ハ11に再び>9 < J、・)に1′
る。In the above-described configuration, the combustion chamber 1 of the piston 10
The fuel injected from the nozzle of the fuel injection nozzle 13, which is arranged at a position that corresponds approximately to the medium flame part 2, is injected toward the recess 14 of the combustion chamber 12, as shown by the arrow 19 at a3 in FIG. will be done. Then, due to the high temperature in the combustion chamber 12, it is ignited and combustion does not occur. The flame during this combustion is transmitted to the recess 14 as shown by the arrow 20 in FIG.
It will rise along the wall. Since the upper end of the wall surface of the fourth part 14 is deeply recessed by the bore 22, the shape of the wall surface of the fourth part 14 allows the flame 20 to be directed back to the inner part 11 of the combustion chamber 12. 1′
Ru.
従ってこの四部14によってピストン10の上部側へ出
る火炎の1j1が少なくなるu従ってピストン10の頂
部11の外周側tこおいてクコーンチされる燃filも
減少され、J:り完全に燃料を燃焼煩光さUることが可
能となり、排気ガス中における黒煙の徂を低鷲すること
が可t1トとbる。また第5図において矢印20で示す
火炎は、燃焼室12の内表面を円周方向に流れるスワー
ル15と干渉されるために、これによって吸気との混合
割合が高められてさらに燃焼が(1進されることに仕る
。Therefore, due to these four parts 14, the amount of flame 1j1 emitted to the upper side of the piston 10 is reduced. Therefore, the amount of fuel that is quenched on the outer circumferential side t of the top 11 of the piston 10 is also reduced. This makes it possible to reduce the amount of black smoke in the exhaust gas. Furthermore, the flame indicated by the arrow 20 in FIG. 5 is interfered with by the swirl 15 flowing in the circumferential direction on the inner surface of the combustion chamber 12, so that the mixing ratio with the intake air is increased and the combustion is further accelerated. Serve what is done to you.
また本7′施例に係るビス1〜ン10によれば、燃焼室
12の内表面に形成されている凹部141ま、7スワー
ル15の流れに対してその上流側に深いポケット16を
有している1こめに、第6図に承りようにこの四部]4
内においてマイクロスワール21を生ずることが可能と
なる。従−)てこのマイクロスワール21によって、霧
状の燃料と空気とのffa含l〜(11進されることに
なり、これよってもより完全41燃焼を達成することが
できるようになる。Further, according to the screws 1 to 10 according to the seventh embodiment, the recess 141 formed on the inner surface of the combustion chamber 12 has a deep pocket 16 on the upstream side with respect to the flow of the seven swirls 15. Please refer to Figure 6 for this four part] 4
It becomes possible to generate micro-swirls 21 within. The lever microswirl 21 causes the ffa content of the atomized fuel and air to be decimalized, thereby making it possible to achieve more complete combustion.
しかしこのマイク[1スワール21は、ポケット16を
スCノール15のにンQ側(こIQ Gするようにして
いるために、J、り効果的に発生されることになる。However, this microphone [1 swirl 21] is generated more effectively because the pocket 16 is placed on the Q side (IQ G) of the scanner 15.
以にに述べたにうに本実施例に係るビス1−ンにJ、れ
ば、燃焼室12の内表面に四部14を設け!こことによ
って、火炎20がこの凹部14の壁面に拾−)で流れ、
るとともに、スワール15と交差することににって燃焼
が促進され、またピストン1゜の頂部11の上を半径方
向外方へ流れることを防+L、することによって、クエ
ンチングを阻止することが11能とt3る。従ってJl
l気ガス中の黒煙を低減することが可能となる。しかも
四部14にはポケッ1〜16がiQ G、Jられており
、このポケット16の存f[ににって効果的にマイクロ
スワール21が発生されるために、このマイクロスワー
ル21によ・)で燃料と吸気との混合がさらに促進され
、にり埋μ:的む燃焼を行なうことが可能になる。しか
もこの燃焼v12は基本的に1.東オーブンチャンバ型
に構成されてi15つ、開口縁部にスキフシ1リツプが
形成されていないために、信頼性の高いピストン10を
得ることが可能になる。As described above, if the screw 1 according to this embodiment is used, the four parts 14 are provided on the inner surface of the combustion chamber 12. Due to this, the flame 20 flows onto the wall surface of this recess 14,
At the same time, combustion is promoted by intersecting the swirl 15, and quenching is prevented by preventing the flow from flowing radially outward over the top 11 of the piston 1°. 11th ability and t3. Therefore Jl
It becomes possible to reduce black smoke in the 1-air gas. Moreover, pockets 1 to 16 are arranged in the fourth part 14, and the existence of this pocket 16 is due to this micro-swirl 21 in order to effectively generate the micro-swirl 21. This further promotes the mixing of fuel and intake air, making it possible to perform targeted combustion. Moreover, this combustion v12 is basically 1. Since it is configured in an east oven chamber type and no skiff lip is formed on the opening edge, it is possible to obtain a highly reliable piston 10.
以上に)ホべたように本発明は、燃焼室の内表面であっ
て燃料噴射ノズルの噴[1と対応する位置にそれぞれ四
部を形成するとともに、この四部の円周方向のス1ノー
ルの上流側にボケツ1〜を設置゛JるJ、うにしたもの
である。従って本発明によれば、ポケットを右Jる凹部
によってマイクロスワールが生じ、燃料と吸気との混合
がより促進されるとともに、四部に沿った火炎の流れに
J、−)てりTンブングを防止することが可11;にな
る。またスキッシュリップを設しJる必要が’J <
!’Cるkめに、信頼性の高いビス1〜ンを促供するこ
とが可能になる。As mentioned above, the present invention forms four parts on the inner surface of the combustion chamber at positions corresponding to the injection nozzle [1], and upstream of the nozzles in the circumferential direction of these four parts. It is designed with a pocket 1~ installed on the side. Therefore, according to the present invention, a micro-swirl is generated by the concave portion of the pocket, which further promotes the mixing of the fuel and the intake air, and prevents the flame flow along the four parts from occurring. It is possible to do 11; It is also necessary to set up a squish lip.
! This makes it possible to provide highly reliable services for customers.
第1図は従来のオーアンチ11ンバQljの燃焼室を備
えたピストンの縦断面図、第2図1,1従米のり]ンI
・ランI−型の燃焼室をIIえたピストンの縦断面図、
第3図は本発明の一実施例1こ係るビス1〜ンの平面図
、第4図は第3図における■〜■線断面図、第5図は第
3図におけるV〜V線断面図、第6図は第5図にd−3
けるV1〜V[線断面図である。
l鵞お秋1面に用いた符号において、
10・・・ビス1−ン
11・・・頂部
12・・・燃焼寮
13・・・燃II llFmノズル
14・・・四部
15・・・スワール
16・・・ボケッ1−
である。Figure 1 is a vertical cross-sectional view of a piston with a combustion chamber of a conventional engine 11 chamber Qlj, Figure 2 is a longitudinal sectional view of a piston equipped with a combustion chamber of a conventional engine
・Longitudinal cross-sectional view of a piston with a run I-type combustion chamber II,
FIG. 3 is a plan view of the screws 1 to 1 according to an embodiment of the present invention, FIG. 4 is a sectional view taken along the line ■ to ■ in FIG. 3, and FIG. 5 is a sectional view taken along the line V to V in FIG. 3. , Figure 6 is d-3 in Figure 5.
This is a cross-sectional view taken along lines V1 to V. In the codes used on page 1 of the 1st page, 10...Bis 1-11...Top 12...Combustion dormitory 13...Moon II llFm nozzle 14...Four parts 15...Swirl 16 ...It's blurry.
Claims (1)
ストンにおいて、前記燃焼室の内表面であって燃f11
11A射ノズルの噴口ど対応する荀Wにイれぞれ凹部を
形成するとともに、この凹部の円周方向のスワールの上
流側にポケットを設(プるようにしたことを特徴とする
内燃機関用ピストン。I! has an oven chamber type combustion chamber on the top! 9( ), the inner surface of the combustion chamber has a fuel f11
For an internal combustion engine, a recess is formed in each hole W corresponding to the nozzle of the 11A injection nozzle, and a pocket is provided on the upstream side of the swirl in the circumferential direction of the recess. piston.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP58014918A JPS59141717A (en) | 1983-01-31 | 1983-01-31 | Piston for use in internal-combustion engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP58014918A JPS59141717A (en) | 1983-01-31 | 1983-01-31 | Piston for use in internal-combustion engine |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS59141717A true JPS59141717A (en) | 1984-08-14 |
Family
ID=11874340
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP58014918A Pending JPS59141717A (en) | 1983-01-31 | 1983-01-31 | Piston for use in internal-combustion engine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS59141717A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105308285A (en) * | 2013-06-20 | 2016-02-03 | 丰田自动车株式会社 | Compression ignition internal combustion engine |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS4734448U (en) * | 1971-05-14 | 1972-12-16 | ||
JPS572536A (en) * | 1980-06-06 | 1982-01-07 | Seiko Epson Corp | Semiconductor device |
-
1983
- 1983-01-31 JP JP58014918A patent/JPS59141717A/en active Pending
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS4734448U (en) * | 1971-05-14 | 1972-12-16 | ||
JPS572536A (en) * | 1980-06-06 | 1982-01-07 | Seiko Epson Corp | Semiconductor device |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105308285A (en) * | 2013-06-20 | 2016-02-03 | 丰田自动车株式会社 | Compression ignition internal combustion engine |
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