JPH04347330A - Piston combustion chamber of direct injection diesel engine - Google Patents
Piston combustion chamber of direct injection diesel engineInfo
- Publication number
- JPH04347330A JPH04347330A JP3146538A JP14653891A JPH04347330A JP H04347330 A JPH04347330 A JP H04347330A JP 3146538 A JP3146538 A JP 3146538A JP 14653891 A JP14653891 A JP 14653891A JP H04347330 A JPH04347330 A JP H04347330A
- Authority
- JP
- Japan
- Prior art keywords
- combustion
- piston
- combustion chamber
- diesel engine
- cavity
- 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 68
- 238000002347 injection Methods 0.000 title claims abstract description 15
- 239000007924 injection Substances 0.000 title claims abstract description 15
- 230000002093 peripheral effect Effects 0.000 abstract 1
- 239000000446 fuel Substances 0.000 description 9
- 230000006835 compression Effects 0.000 description 4
- 238000007906 compression Methods 0.000 description 4
- 239000004071 soot Substances 0.000 description 4
- 238000007796 conventional method Methods 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000007921 spray Substances 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
- F02B23/0618—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
- F02B23/0627—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 having additional bores or grooves machined into the piston for guiding air or charge flow to the piston bowl
-
- 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
- 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)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Abstract
Description
【0001】0001
【産業上の利用分野】この発明は、直接噴射式ディーゼ
ルエンジンのピストン燃焼室に係り、詳しくは中期燃焼
以降の燃焼を改善できる直接噴射式ディーゼルエンジン
のピストン燃焼室に関するものである。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a piston combustion chamber for a direct injection diesel engine, and more particularly to a piston combustion chamber for a direct injection diesel engine that can improve combustion after mid-term combustion.
【0002】0002
【従来の技術】直接噴射式ディーゼルエンジンのピスト
ン燃焼室における燃料の燃焼改善についての従来技術に
は次のようなものがある。
(a)シリンダヘッドに設けられている吸気ポートの形
状及び構造を改善することにより、シリンダ内への吸入
空気の導入の際に、ピストン燃焼室に適切な渦流及び乱
れを生成するようにする。
(b)ピストン燃焼室の形状を改善することにより、燃
料噴射前にピストン燃焼室内に適切な渦流及び縦流れ等
を生成し、ピストン燃焼室内のガス流の乱れの場へ燃料
を高圧噴射し、燃料と空気とのミキシングを最適化する
。2. Description of the Related Art Conventional techniques for improving fuel combustion in the piston combustion chamber of a direct injection diesel engine include the following. (a) Improving the shape and structure of the intake port provided in the cylinder head to create appropriate swirl and turbulence in the piston combustion chamber during the introduction of intake air into the cylinder. (b) By improving the shape of the piston combustion chamber, appropriate vortices, vertical flows, etc. are generated within the piston combustion chamber before fuel injection, and fuel is injected at high pressure into the turbulent gas flow within the piston combustion chamber. Optimize the mixing of fuel and air.
【0003】0003
【発明が解決しようとする課題】このような従来の改善
技術はいずれも初期燃焼におけるガス流動の最適化に係
り、中期燃焼以降の燃料の燃焼改善には寄与していない
。[Problems to be Solved by the Invention] All of these conventional improvement techniques relate to optimizing gas flow during initial combustion, but do not contribute to improving fuel combustion after mid-stage combustion.
【0004】この発明の目的は、中期燃焼以降における
ガス流動を最適化することにより燃焼改善を図ることが
できる直接噴射式ディーゼルエンジンのピストン燃焼室
を提供することである。An object of the present invention is to provide a piston combustion chamber for a direct injection diesel engine that can improve combustion by optimizing gas flow after mid-term combustion.
【0005】[0005]
【課題を解決するための手段】この直接噴射式ディーゼ
ルエンジンのピストン燃焼室は次の(a)〜(d)の構
成要素を有してなる。
(a)ピストンの頂面に開口するようにピストンに形成
される燃焼空間
(b)この燃焼空間の底部において隆起する隆起部(c
)この隆起部内に形成される空洞
(d)隆起部の周辺部に開口し燃焼空間と空洞とを相互
に連通する複数個の連通路とを有してなる。[Means for Solving the Problems] The piston combustion chamber of this direct injection diesel engine has the following components (a) to (d). (a) A combustion space formed in the piston so as to open at the top surface of the piston (b) A raised portion raised at the bottom of this combustion space (c
) A cavity formed within the raised portion; and (d) a plurality of communicating passages that open at the periphery of the raised portion and communicate the combustion space and the cavity with each other.
【0006】[0006]
【作用】圧縮行程では、高圧ガスは、燃焼空間から連通
路を経て空洞内へ導入され、空洞において貯留される。
膨張行程において中期燃焼以降に達すると、空洞内のガ
ス圧が燃焼空間のガス圧より増大し、空洞に貯留されて
いた高圧ガスが、連通路を経て逆流し、隆起部の周辺部
より燃焼空間へ導出される。これにより、燃焼空間には
、縦流れが生成される。[Operation] During the compression stroke, high-pressure gas is introduced from the combustion space into the cavity through the communication path and is stored in the cavity. When the expansion stroke reaches mid-stage combustion or later, the gas pressure inside the cavity increases compared to the gas pressure in the combustion space, and the high-pressure gas stored in the cavity flows back through the communication path and flows into the combustion space from the periphery of the bulge. is derived. As a result, a longitudinal flow is generated in the combustion space.
【0007】[0007]
【実施例】以下、この発明を図面の実施例について説明
する。図2及び図3は直接噴射式ディーゼルエンジンの
ピストン12の縦断面図及び平面図である。ピストン燃
焼室10はピストン12の頂部に設けられる。Aは燃焼
空間14における渦流の流れ方向を示し、Iはインジェ
クションノズル(図示せず)の噴孔から噴射された燃料
噴霧を示している。DESCRIPTION OF THE PREFERRED EMBODIMENTS The present invention will be described below with reference to the drawings. 2 and 3 are a longitudinal sectional view and a plan view of the piston 12 of a direct injection diesel engine. A piston combustion chamber 10 is provided at the top of the piston 12. A indicates the flow direction of the vortex in the combustion space 14, and I indicates the fuel spray injected from the nozzle hole of the injection nozzle (not shown).
【0008】図1はピストン燃焼室10の詳細図である
。
燃焼空間14は、ピストン12の頂面に開口するように
、ピストン12に形成され、ほぼハート形の縦断面を有
している。隆起部16は、燃焼空間14の底面を画定し
、ピストン12の頂面に達しない高さまで隆起している
。空洞18は隆起部16内に形成される。複数個の連通
路20は、図3に示されるように、周方向へ等角度間隔
で配列され、ピストン12の上方から見て放射方向へ延
び、隆起部16の周辺部において燃焼空間14へ開口し
、燃焼空間14と空洞18とを相互に連通している。連
通路20は、ピストン12の頂面に対して平行な平面に
対してθ(ただし、0°<θ<45°)の角度で燃焼空
間14側の開口個所へ向かって斜めに上昇している。連
通路20は、円形ではなく、角形の横断面を有している
。隆起部16内における空洞18及び連通路20の形成
には消型中子が利用される。図1において、B1,C1
はそれぞれ圧縮行程時の縦流れ及び連通路20内のガス
流を示し、B2,C2はそれぞれ膨張行程の中期燃焼以
降の縦流れ及び連通路20内のガス流を示している。FIG. 1 is a detailed view of the piston combustion chamber 10. The combustion space 14 is formed in the piston 12 so as to open at the top surface of the piston 12, and has a substantially heart-shaped longitudinal section. The raised portion 16 defines the bottom surface of the combustion space 14 and is raised to a height that does not reach the top surface of the piston 12. A cavity 18 is formed within the ridge 16. As shown in FIG. 3, the plurality of communication passages 20 are arranged at equal angular intervals in the circumferential direction, extend in the radial direction when viewed from above the piston 12, and open to the combustion space 14 at the periphery of the raised portion 16. The combustion space 14 and the cavity 18 are communicated with each other. The communication passage 20 rises obliquely toward the opening on the combustion space 14 side at an angle of θ (0°<θ<45°) with respect to a plane parallel to the top surface of the piston 12. . The communication path 20 has a rectangular cross section rather than a circular cross section. A demolition core is used to form the cavity 18 and the communication path 20 within the raised portion 16. In FIG. 1, B1, C1
B2 and C2 respectively indicate the longitudinal flow and the gas flow in the communication passage 20 during the compression stroke, and B2 and C2 respectively indicate the longitudinal flow and the gas flow in the communication passage 20 after the middle combustion of the expansion stroke.
【0009】図4はクランク角度と筒内圧との関係を示
している。インジェクションノズルからの燃料噴射は、
TDCの少し手前で行なわれ、TDCの直後に燃焼が開
始され、筒内圧のピークはTDCより少し後になる。初
期燃焼は燃焼開始から筒内圧ピークまでであり、中期燃
焼は筒内圧がピークから所定値まで下降するまでであり
、後期燃焼は中期燃焼以降となる。FIG. 4 shows the relationship between crank angle and cylinder pressure. Fuel injection from the injection nozzle is
Combustion is carried out a little before TDC, combustion starts immediately after TDC, and the peak of the in-cylinder pressure is a little after TDC. Initial combustion is from the start of combustion to the peak of the cylinder pressure, middle combustion is from the peak until the cylinder pressure falls to a predetermined value, and late combustion is after the middle combustion.
【0010】実施例の作用について述べる。圧縮行程で
は、高圧ガスは、図1のB1のように、縦流れが生成さ
れるとともに、さらに、C1のように、燃焼空間14か
ら連通路20を経て空洞18内へ導入され、空洞18に
おいて貯留される。膨張行程において中期燃焼以降に達
すると、空洞18内のガス圧が燃焼空間14のガス圧よ
り増大し、空洞18に貯留されていた高圧ガスが、図1
のC2のように、連通路20を経て逆流し、隆起部の周
辺部より燃焼空間14へ導出され、燃焼空間14におい
てB2のような縦流れを生成する。この縦流れは、中期
燃焼以降の燃料の燃焼の改善に寄与する。[0010] The operation of the embodiment will be described. In the compression stroke, high-pressure gas is generated into a vertical flow as shown in B1 in FIG. stored. When the expansion stroke reaches mid-term combustion or later, the gas pressure in the cavity 18 increases compared to the gas pressure in the combustion space 14, and the high-pressure gas stored in the cavity 18 is released as shown in FIG.
As shown in C2, the fuel flows backward through the communication path 20 and is led out from the periphery of the protuberance into the combustion space 14, producing a vertical flow as shown in B2 in the combustion space 14. This vertical flow contributes to improving the combustion of the fuel after mid-term combustion.
【0011】一方、連通路20には煤が付着するが、連
通路20は、ドリルによる穿孔のような円形横断面では
なく、角形の横断面となっているので、煤が付着し難く
、また、空洞18から燃焼空間14への高圧ガスの吹き
出し際に吹き飛ばされ、煤に因る連通路20の詰まりが
防止される。On the other hand, soot adheres to the communication passage 20, but since the communication passage 20 has a rectangular cross section rather than a circular cross section as in the case of drilling, it is difficult for soot to adhere to it. When the high-pressure gas is blown out from the cavity 18 to the combustion space 14, the soot is blown off and the communication passage 20 is prevented from being clogged with soot.
【0012】0012
【発明の効果】この発明では、空洞が、燃焼空間の底部
の隆起部内に形成されるとともに、隆起部の周辺部に開
口する複数個の連通路を経て燃焼空間へ連通している。
したがって、圧縮行程時に連通路を介して空洞へ導入し
た高圧ガスを、膨張行程時の中期燃焼以降に連通路を経
て燃焼空間内へ吹き出して、燃焼空間内に縦流れを生成
することができる。こうして、良好な縦流れにより中期
燃焼以降の燃焼を改善することができる。According to the present invention, the cavity is formed within the protuberance at the bottom of the combustion space, and communicates with the combustion space through a plurality of communicating passages that open at the periphery of the protuberance. Therefore, the high-pressure gas introduced into the cavity through the communication passage during the compression stroke can be blown out into the combustion space through the communication passage after mid-term combustion during the expansion stroke, thereby generating a vertical flow within the combustion space. In this way, combustion after the middle stage combustion can be improved due to good longitudinal flow.
【図1】ピストン燃焼室の詳細図である。FIG. 1 is a detailed view of the piston combustion chamber.
【図2】直接噴射式ディーゼルエンジンのピストンの縦
断面図である。FIG. 2 is a longitudinal cross-sectional view of a piston of a direct injection diesel engine.
【図3】直接噴射式ディーゼルエンジンのピストンの縦
断面図である。FIG. 3 is a longitudinal cross-sectional view of a piston of a direct injection diesel engine.
【図4】クランク角度と筒内圧との関係を示すグラフで
ある。FIG. 4 is a graph showing the relationship between crank angle and cylinder pressure.
10 ピストン燃焼室 12 ピストン 14 燃焼空間 16 隆起部 18 空洞 20 連通路 10 Piston combustion chamber 12 Piston 14 Combustion space 16 Raised part 18 Hollow 20 Communication path
Claims (1)
ピストンに形成される燃焼空間と、この燃焼空間の底部
において隆起する隆起部と、この隆起部内に形成される
空洞と、前記隆起部の周辺部に開口し前記燃焼空間と前
記空洞とを相互に連通する複数個の連通路とを有してな
ることを特徴とする直接噴射式ディーゼルエンジンのピ
ストン燃焼室。1. A combustion space formed in the piston so as to open at the top surface of the piston, a raised part raised at the bottom of the combustion space, a cavity formed in the raised part, and a cavity formed in the raised part. A piston combustion chamber for a direct injection diesel engine, characterized in that it has a plurality of communicating passages that are open to the periphery and communicate the combustion space and the cavity with each other.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3146538A JPH04347330A (en) | 1991-05-23 | 1991-05-23 | Piston combustion chamber of direct injection diesel engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3146538A JPH04347330A (en) | 1991-05-23 | 1991-05-23 | Piston combustion chamber of direct injection diesel engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH04347330A true JPH04347330A (en) | 1992-12-02 |
Family
ID=15409919
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP3146538A Pending JPH04347330A (en) | 1991-05-23 | 1991-05-23 | Piston combustion chamber of direct injection diesel engine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH04347330A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114607522A (en) * | 2022-03-18 | 2022-06-10 | 潍柴动力股份有限公司 | Combustion system and engine |
-
1991
- 1991-05-23 JP JP3146538A patent/JPH04347330A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114607522A (en) * | 2022-03-18 | 2022-06-10 | 潍柴动力股份有限公司 | Combustion system and engine |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JPH11190217A (en) | Direct injection diesel engine | |
| JPH04347330A (en) | Piston combustion chamber of direct injection diesel engine | |
| JPH09303149A (en) | Combustion chamber of direct injection diesel engine | |
| JPS6032929A (en) | Combustion chamber of direct-injection type internal- combustion engine | |
| JP3116612B2 (en) | In-cylinder direct injection diesel engine | |
| JPH0913971A (en) | Structure for nozzle hole of combustion chamber of swirl chamber type diesel engine | |
| US4532898A (en) | Fuel injection type internal combustion engine | |
| JPH036824Y2 (en) | ||
| JPH11117747A (en) | Direct injection diesel engine | |
| JPH06173687A (en) | Combustion chamber of internal combustion engine having sub chamber | |
| JPS5840255Y2 (en) | Diesel engine combustion chamber | |
| JPS6023463Y2 (en) | Diesel engine fuel injection nozzle device | |
| JPS6115217Y2 (en) | ||
| JPS5926772B2 (en) | Pre-chamber internal combustion engine | |
| JPH0134657Y2 (en) | ||
| JPS6224760Y2 (en) | ||
| JPS5851129B2 (en) | 4-stroke internal combustion engine | |
| JPH0619804Y2 (en) | Diesel engine piston | |
| JPS63198720A (en) | Combustion chamber of direct injection type diesel engine | |
| JPH074241A (en) | Sub-chamber engine | |
| JPH06317159A (en) | Auxiliary chamber type engine | |
| JPH05141244A (en) | Direct injection diesel engine | |
| JPS6019913A (en) | Direct injection type diesel-engine | |
| JPH0719051A (en) | Combustion chamber for internal combustion engine | |
| JPH06248953A (en) | Piston for reciprocating internal combustion engine |