JPH0460166A - Six-cycle diesel engine - Google Patents

Six-cycle diesel engine

Info

Publication number
JPH0460166A
JPH0460166A JP2170873A JP17087390A JPH0460166A JP H0460166 A JPH0460166 A JP H0460166A JP 2170873 A JP2170873 A JP 2170873A JP 17087390 A JP17087390 A JP 17087390A JP H0460166 A JPH0460166 A JP H0460166A
Authority
JP
Japan
Prior art keywords
chamber
air supply
supply air
supply chamber
air chamber
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
Application number
JP2170873A
Other languages
Japanese (ja)
Inventor
Takeshi Yamakoshi
山越 健史
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
IHI Shibaura Machinery Corp
Original Assignee
IHI Shibaura Machinery Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by IHI Shibaura Machinery Corp filed Critical IHI Shibaura Machinery Corp
Priority to JP2170873A priority Critical patent/JPH0460166A/en
Publication of JPH0460166A publication Critical patent/JPH0460166A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B29/00Engines characterised by provision for charging or scavenging not provided for in groups F02B25/00, F02B27/00 or F02B33/00 - F02B39/00; Details thereof
    • F02B29/04Cooling of air intake supply
    • F02B29/0481Intake air cooling by means others than heat exchangers, e.g. by rotating drum regenerators, cooling by expansion or by electrical means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B3/00Engines characterised by air compression and subsequent fuel addition
    • F02B3/06Engines characterised by air compression and subsequent fuel addition with compression ignition
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01PCOOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P2060/00Cooling circuits using auxiliaries
    • F01P2060/02Intercooler
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01PCOOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P7/00Controlling of coolant flow
    • F01P7/14Controlling of coolant flow the coolant being liquid
    • F01P7/16Controlling of coolant flow the coolant being liquid by thermostatic control
    • F01P7/165Controlling of coolant flow the coolant being liquid by thermostatic control characterised by systems with two or more loops
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B29/00Engines characterised by provision for charging or scavenging not provided for in groups F02B25/00, F02B27/00 or F02B33/00 - F02B39/00; Details thereof
    • F02B29/04Cooling of air intake supply
    • F02B29/045Constructional details of the heat exchangers, e.g. pipes, plates, ribs, insulation, materials, or manufacturing and assembly
    • F02B29/0462Liquid cooled heat exchangers
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Abstract

PURPOSE:To warm a wall surface of a supply air chamber by heat of exhaust gas so as to reduce a cooling loss of heat in compressed air, with which the supply air chamber is charged, by forming an exhaust passage in the vicinity of the supply air chamber while forming the exhaust passage and the supply air chamber in a cylinder head. CONSTITUTION:A subcombustion chamber 9, supply air chamber 10 and a cooling water jacket 11 are formed while forming intake and exhaust passages 7, 8, connected to a main combustion chamber 6 in a cylinder l, in a cylinder head 5. The subcombustion chamber 9 communicates with the main combustion chamber 6 by an injection port 13 formed in an insert 12, and the supply air chamber 10 communicates with the main combustion chamber 6 by a communication port 14. Here, the exhaust passage 8 and the cooling water jacket 11 are formed in a position in the vicinity of the supply air chamber 10 to cause its wall surface to be warmed by heat of combustion gas discharged through the exhaust passage, and activation of an activated premixture, produced in the supply air chamber. is promoted by reducing a cooling loss of heat in compressed air with which the supply air chamber 10 is charged.

Description

【発明の詳細な説明】 産業上の利用分野 本発明は、6サイクルディーゼルエンジンに関する。[Detailed description of the invention] Industrial applications The present invention relates to a six-stroke diesel engine.

従来の技術 従来、燃焼室内に入る空気重量を増加させることにより
出力向上を図った6サイクルディーゼルエンジンが開発
されており、6サイクルディーゼルエンジンのシリンダ
ヘッドには、給気室と吸気通路と排気通路とが形成され
ている。
Conventional technology Six-stroke diesel engines have been developed that aim to improve output by increasing the weight of air entering the combustion chamber.The cylinder head of a six-stroke diesel engine has an air supply chamber, an intake passage, and an exhaust passage. is formed.

ここで、給気室に臨ませて副噴射ノズルを設け、第一の
圧縮行程において給気室内に充填された圧縮空気に燃料
を噴射して活性化予混合気を生成することにより、−回
の燃焼で消費される燃料を増加させてエンジンの出力向
上を図り、また、始動性を向上させ、さらに、スモーク
やCo、HCの有害な排ガス成分の減少を図るようにし
た6サイクルディーゼルエンジンが特願平2−2583
0号において提案されている。
Here, a sub-injection nozzle is provided facing the air supply chamber, and fuel is injected into the compressed air filled in the air supply chamber in the first compression stroke to generate an activated premixture. The 6-cycle diesel engine is designed to increase the amount of fuel consumed during combustion to improve engine output, improve startability, and reduce harmful exhaust gas components such as smoke, Co, and HC. Patent application Hei 2-2583
It is proposed in No. 0.

なお、給気室で生成される活性化予混合気の活性化を促
進させる手段としては、給気室内の圧力、給気室の容積
、形状、給気室を囲む壁厚等を変えることが一般に考え
られる。
In addition, as a means to promote the activation of the activated premixture generated in the air supply chamber, it is possible to change the pressure inside the air supply chamber, the volume and shape of the air supply chamber, the thickness of the wall surrounding the air supply chamber, etc. Generally considered.

発明が解決しようとする課題 しかし、給気室は容積が大きいとともに表面積が大きい
ため、給気室内での熱の冷却損失が大きく、活性化予混
合気の活性化を十分に行えず、このため、出力向上や始
動性の向上、及び、スモークやCo、HCの有害な排ガ
ス成分の減少に関して十分な効果が得られない場合があ
る。
Problems to be Solved by the Invention However, since the air supply chamber has a large volume and a large surface area, there is a large cooling loss of heat within the air supply chamber, and the activated premixture cannot be activated sufficiently. In some cases, sufficient effects cannot be obtained in terms of improving output, improving startability, and reducing harmful exhaust gas components such as smoke, Co, and HC.

課題を解決するための手段 連通口を介して主燃焼室に連通された給気室と吸気通路
と排気通路とをシリンダヘッドに形成するとともに第一
の吸気行程と第一の圧縮行程と第二の吸気行程と第二の
圧縮行程と膨張行程と排気行程との6行程で運転される
6サイクルディーゼルエンジンにおいて、前記給気室に
臨ませて燃料を噴射する副噴射ノズルを設けるとともに
、前記排気通路を前記給気室に近接させて形成した。
Means for Solving the Problem An air supply chamber, an intake passage, and an exhaust passage, which are communicated with the main combustion chamber through a communication port, are formed in the cylinder head, and a first intake stroke, a first compression stroke, and a second In a 6-stroke diesel engine that is operated in 6 strokes including an intake stroke, a second compression stroke, an expansion stroke, and an exhaust stroke, a sub-injection nozzle is provided that faces the air supply chamber and injects fuel, and the exhaust A passageway was formed close to the air supply chamber.

作用 排気通路を通って排気される燃焼ガスの熱により給気室
の壁面が暖められ、給気室に充填された圧縮空気におけ
る熱の冷却損失が低減されることにより、給気室におい
て生成される活性化予混合気の活性化が促進される。
The heat of the combustion gas exhausted through the exhaust passage warms the wall surface of the air supply chamber, and the cooling loss of the compressed air filled in the air supply chamber is reduced. Activation of the activated premixture is promoted.

実施例 本発明の一実施例を図面に基づいて説明する。Example An embodiment of the present invention will be described based on the drawings.

シリンダ1内にはピストン2が摺動自在に設けられてお
り、ピストン2はコネクティングロッド3を介してクラ
ンクシャフト(図示せず)に連結されている。また、シ
リンダ1の先端部にはへラドガスケット4を介装したシ
リンダヘッド5がヘッドボルト(図示せず)により締付
けられている。
A piston 2 is slidably provided within the cylinder 1, and the piston 2 is connected to a crankshaft (not shown) via a connecting rod 3. Further, a cylinder head 5 having a helad gasket 4 interposed therein is fastened to the tip of the cylinder 1 with a head bolt (not shown).

前記シリンダヘッド5には、前記シリンダl内の主燃焼
室6に連通された吸気通路7と排気通路8とが形成され
ており、さらに、副燃焼室9と給気室10と冷却水ジャ
ケット11とが形成されている。なお、前記副燃焼室9
はインサート12をシリンダブロック5に組付けること
により形成されており、このインサート12には副燃焼
室9と主燃焼室6とを連通ずる噴口13が形成されてい
る。また、前記給気室10と前記主燃焼室6とは連通口
14により連通されている。ここで、前記排気通路8と
前記冷却水ジャケット11とは前記給気室10に近接し
た位置に形成されている。
The cylinder head 5 is formed with an intake passage 7 and an exhaust passage 8 that communicate with the main combustion chamber 6 in the cylinder 1, and further includes an auxiliary combustion chamber 9, an air supply chamber 10, and a cooling water jacket 11. is formed. Note that the sub-combustion chamber 9
is formed by assembling an insert 12 to the cylinder block 5, and this insert 12 is formed with a nozzle port 13 that communicates the auxiliary combustion chamber 9 and the main combustion chamber 6. Further, the air supply chamber 10 and the main combustion chamber 6 are communicated with each other through a communication port 14 . Here, the exhaust passage 8 and the cooling water jacket 11 are formed in a position close to the air supply chamber 10.

また、前記シリンダヘッド5には、前記吸気通路7の前
記主燃焼室6に開口するボート部を開閉する吸気弁15
と、前記排気通路8の前記主燃焼室6に開口するボート
部を開閉する排気弁16と、前記連通口14の前記主燃
焼室6に開口するボート部を開閉する副バルブ17とが
摺動自在に取付けられている。さらに、前記シリンダヘ
ッド5には、前記副燃焼室9に臨んだ主噴射ノズル18
とグロープラグ19、及び、前記給気室10に臨んだ副
噴射ノズル20が固定的に取付けられている。
The cylinder head 5 also includes an intake valve 15 that opens and closes a boat portion of the intake passage 7 that opens into the main combustion chamber 6.
An exhaust valve 16 that opens and closes a boat portion of the exhaust passage 8 that opens into the main combustion chamber 6 and a sub valve 17 that opens and closes a boat portion of the communication port 14 that opens into the main combustion chamber 6 slide. It can be installed freely. Furthermore, the cylinder head 5 has a main injection nozzle 18 facing the sub-combustion chamber 9.
A glow plug 19 and a sub-injection nozzle 20 facing the air supply chamber 10 are fixedly attached.

つぎに、前記シリンダヘッド5にはスタットボルト21
とキャップナツト22とによりロッカーカバー23が締
付けられている。そして、このロッカーカバー23内に
は、前記スタットボルト21とナツト24とにより締付
けられた半割構造の軸受25,26と、これらの軸受2
5,26により軸支されたカムシャト27と、吸気用ロ
ッカーアーム(図示せず)と、排気用ロッカーアーム2
8と、副バルブ用ロッカーアーム29と、前記カムシャ
フト27に固定された副バルブカム30や排気カムC図
示せず)等が設けられている。
Next, a stud bolt 21 is attached to the cylinder head 5.
The rocker cover 23 is tightened by the cap nut 22 and the cap nut 22. Inside this rocker cover 23 are half-split bearings 25 and 26 that are tightened by the stud bolts 21 and nuts 24, and these bearings 2.
5 and 26, an intake rocker arm (not shown), and an exhaust rocker arm 2.
8, a sub-valve rocker arm 29, a sub-valve cam 30 fixed to the camshaft 27, an exhaust cam C (not shown), etc. are provided.

ここで、前記排気弁16はリテーナ31とコツタ32と
を介してスプリング33により閉弁方向へ付勢されてお
り、前記排気用ロッカーアーム28の一端は排気弁16
のステムエンドに当接され、排気用ロッカーアーム28
の他端は支点34に回動自在に当接されている。なお、
排気用ロッカーアーム28の略中央部にはシャフト35
が固定され、このシャフト35に回動自在に取付けられ
たローラ36が前記排気カムの外周面に当接されている
。また、前記支点34は、前記ローラ36と前記排気カ
ムの外周面との隙間を適正値に調整した後、ナツト37
によりロックされている。
Here, the exhaust valve 16 is urged in the valve closing direction by a spring 33 via a retainer 31 and a stopper 32, and one end of the exhaust rocker arm 28 is connected to the exhaust valve 16.
The exhaust rocker arm 28 is in contact with the stem end of the exhaust rocker arm 28.
The other end is rotatably abutted on a fulcrum 34. In addition,
A shaft 35 is located approximately at the center of the exhaust rocker arm 28.
is fixed, and a roller 36 rotatably attached to the shaft 35 is in contact with the outer peripheral surface of the exhaust cam. Further, the fulcrum 34 is connected to the nut 37 after adjusting the gap between the roller 36 and the outer peripheral surface of the exhaust cam to an appropriate value.
is locked by.

同様に、前記副バルブ17はリテーナ38とコツタ39
とを介してスプリング40により閉弁方向へ付勢されて
おり、前記副バルブ用ロッカーアーム29の一端は副バ
ルブ17のステムエンドに当接され、副バルブ用ロッカ
ーアーム29の他端は支点41に回動自在に当接されて
いる。なお、副バルブ用ロッカーアーム29の略中央部
にはシャフト42が固定され、このシャフト42に回動
自在に取付けられたローラ43が前記副バルブカム30
の外周面に当接されている。また、前記支点41は、前
記ローラ43と前記副バルブカム30の外周面との隙間
を適正値に調整した後、ナツト44によりロックされて
いる。
Similarly, the auxiliary valve 17 has a retainer 38 and a socket 39.
One end of the auxiliary valve rocker arm 29 is brought into contact with the stem end of the auxiliary valve 17, and the other end of the auxiliary valve rocker arm 29 is pressed against the fulcrum 41. It is rotatably abutted on. A shaft 42 is fixed to a substantially central portion of the sub-valve rocker arm 29, and a roller 43 rotatably attached to the shaft 42 is attached to the sub-valve cam 30.
is in contact with the outer peripheral surface of the Further, the fulcrum 41 is locked by a nut 44 after adjusting the gap between the roller 43 and the outer peripheral surface of the sub-valve cam 30 to an appropriate value.

このような構成において、まず、6サイクルデイーセ゛
ルエンシンの動作を第3図及び第4図に基づいて説明す
る。第3図(a)は、第一の吸気行程を示す。吸気弁1
5が開弁されており、ピストン2が下方へ摺動するとと
もに空気が吸気通路7を通って主燃焼室6内に吸入され
る。
In such a configuration, the operation of the six-cycle diesel engine will first be described with reference to FIGS. 3 and 4. FIG. 3(a) shows the first intake stroke. Intake valve 1
5 is open, and as the piston 2 slides downward, air is drawn into the main combustion chamber 6 through the intake passage 7.

第3図(b)は、第一の圧縮行程を示す。第一の吸気行
程において主燃焼室6内に吸入された空気がピストン2
の上昇に伴って圧縮される。なお、副バルブ17が開弁
しており、圧縮空気は副燃焼室9内に充填されるととも
に給気室10内にも充填される。
FIG. 3(b) shows the first compression stroke. The air sucked into the main combustion chamber 6 during the first intake stroke is transferred to the piston 2.
is compressed as the value increases. Note that the auxiliary valve 17 is open, and the compressed air is filled into the auxiliary combustion chamber 9 and also into the air supply chamber 10.

第3図(c)は、第一の圧縮行程の最終段階を示す。ピ
ストン2が路上死点に達するタイミングで副バルブ17
が閉弁されるとともに副噴射ノズル20から給気室10
内に燃料が噴射される。この燃料は、給気室10内の渦
流空気と混合され、活性化予混合気が生成される。なお
、このときの燃料噴射においては、給気室10内の圧縮
比及び温度が低いために燃料の着火には至らない。
FIG. 3(c) shows the final stage of the first compression stroke. At the timing when the piston 2 reaches the road dead center, the auxiliary valve 17
is closed and the air supply chamber 10 is discharged from the sub-injection nozzle 20.
Fuel is injected inside. This fuel is mixed with the swirling air in the air supply chamber 10 to generate an activated premixture. In addition, in the fuel injection at this time, the compression ratio and temperature in the air supply chamber 10 are low, so that the fuel does not ignite.

第3図(d)は、第二の吸気行程を示す。ピストン2が
クランク角度で約90” 下降すると主燃焼室6内の圧
力が外部に対して負圧状態となり、このタイミングで吸
気弁15を開弁させると空気が吸気通路7を通って主燃
焼室6内に吸入される。
FIG. 3(d) shows the second intake stroke. When the piston 2 descends by about 90" at the crank angle, the pressure inside the main combustion chamber 6 becomes negative relative to the outside. When the intake valve 15 is opened at this timing, air passes through the intake passage 7 and enters the main combustion chamber. Inhaled within 6 days.

なお、ピストン2が下死点に達した際には、第一の吸気
行程の場合と同量の空気が主燃焼室6内に吸入される。
Note that when the piston 2 reaches the bottom dead center, the same amount of air is sucked into the main combustion chamber 6 as in the first intake stroke.

第3図(e)は、第二の吸気行程の終了直前の状態を示
す。吸気弁15が閉弁されるとともに副バルブ17が開
弁され、給気室lo内の活性化予混合気が主燃焼室6内
に噴出し、主燃焼室6内の空気量は第一の吸気行程終了
時における主燃焼室6内の空気量の約1.5倍となる。
FIG. 3(e) shows the state immediately before the end of the second intake stroke. The intake valve 15 is closed and the auxiliary valve 17 is opened, and the activated premixture in the air supply chamber lo is injected into the main combustion chamber 6, and the amount of air in the main combustion chamber 6 is reduced to the first level. This is approximately 1.5 times the amount of air in the main combustion chamber 6 at the end of the intake stroke.

第3図(f)は、第二の圧縮行程を示す。FIG. 3(f) shows the second compression stroke.

第3図(g)は、第二の圧縮行程の最終段階を示す。活
性化予混合気が混合された圧縮空気は着火可能な温度に
上昇し、ピストン2が略り死点に達したタイミングで主
噴射ノズル18から副燃焼室9内に燃料が噴射され、着
火が起こる。
FIG. 3(g) shows the final stage of the second compression stroke. The compressed air mixed with the activated premixture rises to a temperature that can be ignited, and when the piston 2 reaches its dead center, fuel is injected from the main injection nozzle 18 into the sub-combustion chamber 9, causing ignition. happen.

第3図(h)は、膨張行程を示す。燃焼ガスが副燃焼室
9から主燃焼室6内に噴出し、主燃焼室6内での燃焼が
行われるとともにピストン2が下方へ押し下げられ、ク
ランクシャフトに動力が伝達される。
FIG. 3(h) shows the expansion stroke. Combustion gas is ejected from the sub-combustion chamber 9 into the main combustion chamber 6, combustion occurs within the main combustion chamber 6, and the piston 2 is pushed downward, thereby transmitting power to the crankshaft.

第3図(i)は、排気行程を示す。排気弁16が開弁さ
れるとともにピストン2が上昇し、主燃焼室6内の燃焼
ガスが排気通路8を通して排出される。
FIG. 3(i) shows the exhaust stroke. When the exhaust valve 16 is opened, the piston 2 rises, and the combustion gas in the main combustion chamber 6 is discharged through the exhaust passage 8.

ここで、給気室10内の活性化予混合気は第3図(C)
に示した第一の圧縮行程の最終段階において生成される
が、給気室10に近接して排気通路8が形成されている
ため、この排気通路8を通って排気される燃焼ガスの熱
により給気室10の壁面が暖められている。従って、給
気室IO内に圧縮空気を充填した際における熱の冷却損
失が低減され、給気室10において生成される活性化予
混合気の活性化が促進される。一方、給気室10に近接
して冷却水ジャケット11が形成されているため、冷却
水ジャケット1】内を流れる冷却水によって給気室10
の壁面が冷却され、給気室10内の温度が高くなり過ぎ
て活性化予混合気を生成する段階で着火が起こるという
ことが防止される。なお、給気室10に対する排気通路
8と冷却水ジャケット11との形成位置を変更すること
により、給気室1o壁面の温度調節を行える。
Here, the activated premixture in the air supply chamber 10 is shown in FIG. 3(C).
However, since the exhaust passage 8 is formed close to the air supply chamber 10, the heat of the combustion gas exhausted through the exhaust passage 8 The wall surface of the air supply chamber 10 is heated. Therefore, cooling loss of heat when compressed air is filled into the air supply chamber IO is reduced, and activation of the activated premixture generated in the air supply chamber 10 is promoted. On the other hand, since the cooling water jacket 11 is formed close to the air supply chamber 10, the cooling water flowing inside the cooling water jacket 1
The wall surface of the air supply chamber 10 is cooled, and ignition is prevented from occurring at a stage when the temperature inside the air supply chamber 10 becomes too high and an activated premixture is generated. Note that by changing the formation positions of the exhaust passage 8 and the cooling water jacket 11 with respect to the air supply chamber 10, the temperature of the wall surface of the air supply chamber 1o can be adjusted.

発明の効果 本発明は、上述のようにシリンダヘッドに排気通路と給
気室とを形成するとともに排気通路を給気室に近接させ
て形成したことにより、排気通路を通って排気される燃
焼ガスの熱によって給気室の壁面を暖めることができ、
従って、給気室に充填された圧縮空気における熱の冷却
損失を低減させ、給気室内の圧縮空気に副噴射ノズルか
ら燃料を噴射することにより生成される活性化予混合気
の活性化を促進させることができ、このため、6サイク
ルディーゼルエンジンの出力向上や始動性向上、及び、
スモークやC○、HCの有害な排ガス成分の減少をより
一層確実に達成することができる等の効果を有する。
Effects of the Invention The present invention has an exhaust passage and an air supply chamber formed in the cylinder head as described above, and the exhaust passage is formed close to the air supply chamber, so that the combustion gas exhausted through the exhaust passage is reduced. The heat can warm the walls of the air supply room,
Therefore, the cooling loss of heat in the compressed air filled in the air supply chamber is reduced, and the activation of the activated premixture generated by injecting fuel from the sub-injection nozzle into the compressed air in the air supply chamber is promoted. Therefore, it is possible to improve the output and startability of a 6-stroke diesel engine, and
It has the effect of more reliably achieving a reduction in harmful exhaust gas components such as smoke, CO, and HC.

【図面の簡単な説明】[Brief explanation of drawings]

図面は本発明の〜実施例を示すもので、第1図は縦断正
面図、第2図は第1図におけるA−A線断面図、第3図
は6サイクルディーゼルエンジンの動作を説明する説明
図、第4図は弁の開閉と燃料噴射とのタイミングを説明
するタイミングチャートである。 5・・・シリンダヘッド、7・・・吸気通路、8・・・
排気通路、9・・・副燃焼室、10・・・給気室lZ図
The drawings show embodiments of the present invention; FIG. 1 is a longitudinal sectional front view, FIG. 2 is a sectional view taken along line A-A in FIG. 1, and FIG. 3 is an explanation explaining the operation of a 6-cycle diesel engine. 4 are timing charts illustrating the timing of opening and closing of the valve and the timing of fuel injection. 5... Cylinder head, 7... Intake passage, 8...
Exhaust passage, 9... Sub-combustion chamber, 10... Air supply chamber lZ diagram

Claims (1)

【特許請求の範囲】[Claims]  連通口を介して主燃焼室に連通された給気室と吸気通
路と排気通路とをシリンダヘッドに形成するとともに第
一の吸気行程と第一の圧縮行程と第二の吸気行程と第二
の圧縮行程と膨張行程と排気行程との6行程で運転され
る6サイクルディーゼルエンジンにおいて、前記給気室
に臨ませて燃料を噴射する副噴射ノズルを設けるととも
に、前記排気通路を前記給気室に近接させて形成したこ
とを特徴とする6サイクルディーゼルエンジン。
An air supply chamber, an intake passage, and an exhaust passage, which are communicated with the main combustion chamber through a communication port, are formed in the cylinder head, and a first intake stroke, a first compression stroke, a second intake stroke, and a second In a 6-cycle diesel engine that is operated in six strokes including a compression stroke, an expansion stroke, and an exhaust stroke, a sub-injection nozzle is provided that faces the air supply chamber and injects fuel, and the exhaust passage is connected to the air supply chamber. A 6-stroke diesel engine characterized by being formed close to each other.
JP2170873A 1990-06-28 1990-06-28 Six-cycle diesel engine Pending JPH0460166A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2170873A JPH0460166A (en) 1990-06-28 1990-06-28 Six-cycle diesel engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2170873A JPH0460166A (en) 1990-06-28 1990-06-28 Six-cycle diesel engine

Publications (1)

Publication Number Publication Date
JPH0460166A true JPH0460166A (en) 1992-02-26

Family

ID=15912899

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2170873A Pending JPH0460166A (en) 1990-06-28 1990-06-28 Six-cycle diesel engine

Country Status (1)

Country Link
JP (1) JPH0460166A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7765785B2 (en) 2005-08-29 2010-08-03 Kashmerick Gerald E Combustion engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7765785B2 (en) 2005-08-29 2010-08-03 Kashmerick Gerald E Combustion engine

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