JPH0733771B2 - 2-cycle internal combustion engine - Google Patents
2-cycle internal combustion engineInfo
- Publication number
- JPH0733771B2 JPH0733771B2 JP20003588A JP20003588A JPH0733771B2 JP H0733771 B2 JPH0733771 B2 JP H0733771B2 JP 20003588 A JP20003588 A JP 20003588A JP 20003588 A JP20003588 A JP 20003588A JP H0733771 B2 JPH0733771 B2 JP H0733771B2
- Authority
- JP
- Japan
- Prior art keywords
- air supply
- valve
- exhaust
- combustion chamber
- fresh air
- 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.)
- Expired - Fee Related
Links
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
- F02B75/00—Other engines
- F02B75/02—Engines characterised by their cycles, e.g. six-stroke
- F02B2075/022—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
- F02B2075/025—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two
Landscapes
- Combustion Methods Of Internal-Combustion Engines (AREA)
Description
【発明の詳細な説明】 〔産業上の利用分野〕 本発明は2サイクル内燃機関に関する。The present invention relates to a two-cycle internal combustion engine.
〔従来の技術〕 一対の給気弁と一対の排気弁を具備し、シリンダヘッド
内壁面から燃焼室に向けて延びるマスク壁を各排気弁と
吸気弁との間に形成して各マスク壁により給気弁側に位
置する各排気弁周縁部と弁座間の開口を排気弁のリフト
量が小さいときに閉鎖し、一対の給気ポートから夫々流
入する新気の流量が等しくなるように各給気ポートを形
成した2サイクル内燃機関が本出願人により既に提案さ
れている(特願昭62−31559号参照)。この2サイクル
内燃機関では排気弁開弁時においてブローダウンが生じ
た後に排気ポートから燃焼室内に逆流する排気ガスをマ
スク壁により案内し、この逆流排気ガスにより燃焼室内
にシリンダ軸線回りのスワール流を発生せしめるように
している。機関低負荷運転時には給気ポートから流入す
る新気の流速が遅いために新気が逆流排気ガスのスワー
ル流と共に旋回し、その結果新気が燃焼室の下方領域に
拡散せず、燃焼室の上部領域に集まるために燃焼室内は
成層化される。一方、機関高負荷運転時には給気ポート
から流入する新気の流速が速いために新気はピストン頂
面に向かって下降し、次いでピストン頂面において流れ
方向を変え、斯くしてループ掃気が行なわれる。このと
き両給気ポートから流入する新気の流量が異なると、即
ち両給気ポートから流入する新気の強さに差があると弱
い方の新気流は強い方の新気流により横方向に押される
ためにきれいなループ状を描いて流れず、斯くして全体
として良好なループ掃気が得られない。しかしながらこ
の2サイクル内燃機関では両給気ポートから流入する新
気の強さが等しいために両新気流が共にループ状に流
れ、斯くして良好なループ掃気が行なわれる。[Prior Art] A pair of air supply valves and a pair of exhaust valves are provided, and a mask wall extending from the inner wall surface of the cylinder head toward the combustion chamber is formed between each exhaust valve and the intake valve. When the exhaust valve lift amount is small, the opening between the exhaust valve peripheral portion located on the intake valve side and the valve seat is closed, and each intake air is supplied from the pair of intake ports so that the flow rate of fresh air is equal. A two-cycle internal combustion engine having an air port has already been proposed by the present applicant (see Japanese Patent Application No. 62-31559). In this two-cycle internal combustion engine, the exhaust gas that flows back into the combustion chamber from the exhaust port after the blowdown occurs when the exhaust valve is opened is guided by the mask wall, and the swirl flow around the cylinder axis is introduced into the combustion chamber by this backflow exhaust gas. I am trying to generate it. During low engine load operation, the velocity of the fresh air flowing from the air supply port is slow, so the fresh air swirls with the swirl flow of the backflow exhaust gas, and as a result, the fresh air does not diffuse to the lower region of the combustion chamber and The combustion chamber is stratified to gather in the upper region. On the other hand, during high engine load operation, the velocity of the fresh air flowing from the air supply port is high, so the fresh air descends toward the piston top surface, then changes the flow direction at the piston top surface, thus performing loop scavenging. Be done. At this time, if the flow rate of fresh air flowing in from both air supply ports is different, that is, if there is a difference in the strength of fresh air flowing in from both air supply ports, the weaker new air flow will be laterally moved by the stronger new air flow. Since it is pushed, it does not flow in a clean loop shape, and thus good loop scavenging cannot be obtained as a whole. However, in this two-cycle internal combustion engine, since the fresh air flowing from both air supply ports has the same strength, both new air flows in a loop shape, and thus good loop scavenging is performed.
しかしながらこの2サイクル内燃機関では排気弁のリフ
トが大きくなると排気弁と弁座間の開口が排気弁の全周
に亘って燃焼室内に開口し、その結果給気ポートから流
入した新気の一部がシリンダヘッド内壁面に沿って流
れ、次いでマスク壁を越えて排気ポート内に流出するた
めに新気の吹き抜けが生じる。ところがこのように新気
の一部が排気ポート内に吹き抜けるとこの新気はループ
掃気に寄与しないことになるので強力なループ掃気を行
なうことができないという問題がある。However, in this two-cycle internal combustion engine, when the lift of the exhaust valve increases, the opening between the exhaust valve and the valve seat opens in the combustion chamber over the entire circumference of the exhaust valve, and as a result, a part of the fresh air flowing from the intake port Fresh air blows through because it flows along the inner wall surface of the cylinder head and then flows over the mask wall into the exhaust port. However, if a part of the fresh air blows into the exhaust port in this way, this fresh air does not contribute to the loop scavenging, so that there is a problem that strong loop scavenging cannot be performed.
上記問題点を解決するために本発明によれば一対の給気
弁および一対の給気ポートをシリンダ軸線を含む平面に
関して夫々対称に配置すると共に各給気弁の形状および
各給気ポートの形状を夫々実質的に同一の形状に形成
し、シリンダヘッド内壁面から燃焼室に向けて延びるマ
スク壁を各給気弁と排気弁との間に形成して各マスク壁
により排気弁側に位置する各給気弁周縁部と弁座間の開
口を給気弁の全開弁期間に亘って閉鎖し、各マスク壁を
上述シリンダ軸線を含む平面に関して対称に配置すると
共に各マスク壁の形状を実質的に同一の形状に形成して
いる。According to the present invention, in order to solve the above-mentioned problems, a pair of air supply valves and a pair of air supply ports are arranged symmetrically with respect to a plane including a cylinder axis, and the shape of each air supply valve and the shape of each air supply port. Are formed in substantially the same shape, a mask wall extending from the inner wall surface of the cylinder head toward the combustion chamber is formed between each air supply valve and the exhaust valve, and each mask wall is positioned on the exhaust valve side. The opening between the periphery of each air supply valve and the valve seat is closed for the full opening period of the air supply valve, each mask wall is arranged symmetrically with respect to the plane including the cylinder axis, and the shape of each mask wall is substantially They are formed in the same shape.
排気弁側に位置する各給気弁周縁部と弁座間の開口を給
気弁の全開弁期間に亘ってマスク壁により閉鎖すること
によって給気ポートから流入する新気は排気ポート内に
吹き抜けることなくピストン頂面に向かい、しかも両給
気ポートから流入する新気が共にきれいなループ状をな
して流れる。By closing the opening between the periphery of each intake valve located on the exhaust valve side and the valve seat with the mask wall for the full opening period of the intake valve, the fresh air flowing in from the intake port is blown into the exhaust port. Instead, the fresh air flowing from both air supply ports flows toward the top of the piston in a clean loop.
第1図から第3図を参照すると、1はシリンダブロッ
ク、2はシリンダブロック1内で往復動するピストン、
3はシリンダブロック1上に固定されたシリンダヘッ
ド、4はシリンダヘッド3の内壁面3aとピストン2の頂
面間に形成された燃焼室を夫々示す。シリンダヘッド3
の内壁面3a上には燃焼室4に向けて突出しかつシリンダ
ヘッド3の内壁面3aの直径に沿いその直径の全体に亙っ
て延びる隆起部5が形成される。第1図に示すようにこ
の隆起部5はその下端部に尾根5aを有する三角形状断面
を有しており、この隆起部5の根元部が第1図から第3
図において5bで示される。隆起部5の一側には一対の給
気弁6が配置され、隆起部5の他側には一対の排気弁7
が配置される。Referring to FIGS. 1 to 3, 1 is a cylinder block, 2 is a piston reciprocating in the cylinder block 1,
Reference numeral 3 denotes a cylinder head fixed on the cylinder block 1, and 4 denotes a combustion chamber formed between the inner wall surface 3a of the cylinder head 3 and the top surface of the piston 2. Cylinder head 3
A ridge 5 is formed on the inner wall surface 3a of the cylinder 3, which projects toward the combustion chamber 4 and extends along the diameter of the inner wall surface 3a of the cylinder head 3 and extends over the entire diameter. As shown in FIG. 1, this raised portion 5 has a triangular cross section having a ridge 5a at its lower end, and the root portion of this raised portion 5 is shown in FIGS.
It is shown at 5b in the figure. A pair of air supply valves 6 are arranged on one side of the raised portion 5, and a pair of exhaust valves 7 are arranged on the other side of the raised portion 5.
Are placed.
また、隆起部5の中央部5cは排気弁7側に湾曲せしめら
れており、この湾曲中央部5cの給気弁6側に点火栓8が
配置される。従って点火栓8はほぼシリンダ軸線上に位
置し、しかも隆起部5に対して給気弁6側に配置されて
いる。隆起部5上には排気弁7側に位置する給気弁6周
縁部と弁座9間の開口を覆うために各給気弁6に対して
夫々マスク壁10が形成されている。これらのマスク壁10
は対応する給気弁6の周縁部に極めて近接配置されかつ
給気弁6の周縁部に沿って延びる断面円弧状をなしてお
り、更にこれらのマスク壁10は第1図において鎖線で示
す最大リフト位置にある給気弁6よりも下方まて燃焼室
4に向けて延びている。従って排気弁7側に位置する給
気弁6周縁部と弁座9間の開口は給気弁6の開弁期間全
体に亙ってマスク壁10により閉鎖されることになる。一
方、排気弁7の周縁部と隆起部5の根元部5bとの間には
一定の間隔が設けられており従って給気弁6側に位置す
る排気弁7周縁部と弁座11間の開口は隆起部5によって
閉鎖されることがない。従って排気弁7が開弁すると排
気弁7と弁座11間に形成される開口はその全体が燃焼室
4内に開口することになる。Further, the central portion 5c of the raised portion 5 is curved toward the exhaust valve 7 side, and the spark plug 8 is arranged on the air supply valve 6 side of the curved central portion 5c. Therefore, the spark plug 8 is located substantially on the cylinder axis and is arranged on the air supply valve 6 side with respect to the raised portion 5. A mask wall 10 is formed on the raised portion 5 for each air supply valve 6 so as to cover the opening between the periphery of the air supply valve 6 located on the exhaust valve 7 side and the valve seat 9. These mask walls 10
Are arranged very close to the peripheral edge of the corresponding air supply valve 6 and have an arcuate cross-section extending along the peripheral edge of the air supply valve 6, and these mask walls 10 are the maximum indicated by the chain line in FIG. It extends toward the combustion chamber 4 below the air supply valve 6 at the lift position. Therefore, the opening between the periphery of the air supply valve 6 located on the exhaust valve 7 side and the valve seat 9 is closed by the mask wall 10 during the entire opening period of the air supply valve 6. On the other hand, a constant space is provided between the peripheral portion of the exhaust valve 7 and the root portion 5b of the raised portion 5, and therefore the opening between the peripheral portion of the exhaust valve 7 located on the intake valve 6 side and the valve seat 11 is formed. Is not closed by the ridge 5. Therefore, when the exhaust valve 7 opens, the entire opening formed between the exhaust valve 7 and the valve seat 11 opens into the combustion chamber 4.
シリンダヘッド3内には給気弁6に対して給気ポート12
が形成され、排気弁7に対して排気ポート13が形成され
る。各給気ポート12は例えば機関によって駆動される機
械式過給機14および給気ダクト15を介して図示しないエ
アクリーナに接続されており、給気ダクト15内にはスロ
ットル弁16が配置される。各給気ポート12の上壁面には
燃料噴射弁17が配置され、各燃料噴射弁17からは広がり
角の小さい剛体状の燃料が給気弁6の第3図においてハ
ッチングで示す領域18に向けて噴射される。この領域18
は給気ポート12軸線に関して点火栓8側に位置し、かつ
両給気弁6の弁ステムを結ぶ線に対して点火栓8と反対
側に位置する。In the cylinder head 3, there is an air supply port 12 for the air supply valve 6.
Is formed, and the exhaust port 13 is formed for the exhaust valve 7. Each air supply port 12 is connected to an air cleaner (not shown) via a mechanical supercharger 14 driven by an engine and an air supply duct 15, and a throttle valve 16 is arranged in the air supply duct 15. A fuel injection valve 17 is disposed on the upper wall surface of each air supply port 12, and a rigid fuel having a small divergence angle is directed from each fuel injection valve 17 toward a region 18 of the air supply valve 6 shown by hatching in FIG. Is jetted. This area 18
Is located on the spark plug 8 side with respect to the axis of the air supply port 12 and on the side opposite to the spark plug 8 with respect to the line connecting the valve stems of both air supply valves 6.
第2図からわかるように一対の給気弁6はシリンダ軸線
を含む平面a−aに関して対称に配置されており、一対
の給気ポート12も平面a−aに関して対称に配置されて
いる。また、各給気弁6の形状は実質的に同一であり、
各給気ポート12の形状も実質的に同一である。また、各
給気弁6の弁リフト曲線は実質的に同一であり、従って
給気弁8が開弁したときに各給気ポート12から流入する
新気の量は実質的に同一となる。また、隆起部5は平面
a−aに関して対称的な形状を有し、各マスク壁10も平
面a−aに関して対称的に配置されている。更に各マス
ク壁10は実質的に同一の形状を有する。また、各排気弁
7も平面a−aに関して対称的に配置されており、各排
気弁7は実質的に同一の形状を有する。As can be seen from FIG. 2, the pair of air supply valves 6 are arranged symmetrically with respect to the plane aa including the cylinder axis, and the pair of air supply ports 12 are also arranged symmetrically with respect to the plane aa. Further, the shape of each air supply valve 6 is substantially the same,
The shape of each air supply port 12 is also substantially the same. Further, the valve lift curves of the air supply valves 6 are substantially the same, and therefore, when the air supply valve 8 is opened, the amount of fresh air flowing in from each air supply port 12 is substantially the same. The raised portion 5 has a shape symmetrical with respect to the plane aa, and the mask walls 10 are also arranged symmetrically with respect to the plane aa. Further, each mask wall 10 has substantially the same shape. The exhaust valves 7 are also arranged symmetrically with respect to the plane aa, and the exhaust valves 7 have substantially the same shape.
第4図は各給気弁6および各排気弁7の開弁期間の一
例、および燃料噴射期間の一例を示している。第4図に
示す例においては給気弁6よりも排気弁7が先に開弁
し、給気弁6よりも排気弁7が先に閉弁する。更に燃料
噴射期間は給気弁6の開弁後、下死点BDC前までの間に
設定されている。FIG. 4 shows an example of a valve opening period of each air supply valve 6 and each exhaust valve 7, and an example of a fuel injection period. In the example shown in FIG. 4, the exhaust valve 7 opens earlier than the intake valve 6, and the exhaust valve 7 closes earlier than the intake valve 6. Further, the fuel injection period is set after the air supply valve 6 is opened and before the bottom dead center BDC.
第5図は給気弁6および排気弁7の弁リフトおよび排気
ポート13内の圧力変化P1,P2,Q1,Q2を示している。これ
らの圧力変化P1,P2,Q1,Q2については後述する。FIG. 5 shows valve lifts of the intake valve 6 and the exhaust valve 7 and pressure changes P 1 , P 2 , Q 1 , Q 2 in the exhaust port 13. These pressure changes P 1 , P 2 , Q 1 , Q 2 will be described later.
次に第6図および第7図を参照して掃気作用および成層
化作用について説明する。第6図は低負荷運転時を示し
ており、第7図は高負荷運転時を示している。また、第
6図(A)および第7図(A)は給気弁6が開弁した直
後を示しており、第6図(B)および第7図(B)はピ
ストン2がほぼ下死点にあるときを示している。Next, the scavenging action and the stratification action will be described with reference to FIGS. 6 and 7. FIG. 6 shows a low load operation, and FIG. 7 shows a high load operation. Further, FIGS. 6 (A) and 7 (A) show immediately after the air supply valve 6 is opened, and FIGS. 6 (B) and 7 (B) show that the piston 2 is almost dead. It shows when there is a point.
まず初めに第6図を参照して機関低負荷運転時について
説明する。First, the engine low load operation will be described with reference to FIG.
ピストン2が下降して排気弁7が開弁すると燃焼室4内
の高圧燃焼ガスが排気ポート13内に流出し、その結果第
5図においてP1で示すように排気ポート13内の圧力は一
時的に正圧となる。この正圧P1は排気通路内を下流に向
けて伝播し、各気筒の排気通路の集合部において反射
し、今度は負圧となって再び排気ポート13内に伝播して
くる。従って給気弁6が開弁すると第5図においてP2で
示されるように排気ポート13内には負圧が発生する。こ
の負圧の発生する時期は排気通路の長さに依存してい
る。機関低負荷運転時は燃焼圧が低く、従って排気ポー
ト13内に発生する正圧P1、負圧P2は比較的小さい。When the piston 2 descends and the exhaust valve 7 opens, the high-pressure combustion gas in the combustion chamber 4 flows into the exhaust port 13, and as a result, the pressure in the exhaust port 13 temporarily changes as indicated by P 1 in FIG. Positive pressure. This positive pressure P 1 propagates in the exhaust passage toward the downstream side, is reflected at the gathering portion of the exhaust passages of the cylinders, becomes negative pressure this time, and propagates again into the exhaust port 13. Therefore, when the air supply valve 6 is opened, a negative pressure is generated in the exhaust port 13 as shown by P 2 in FIG. The time when this negative pressure is generated depends on the length of the exhaust passage. The combustion pressure is low during engine low load operation, so the positive pressure P 1 and the negative pressure P 2 generated in the exhaust port 13 are relatively small.
給気弁6が開弁すると給気ポート12から燃焼室4内に燃
料を含んだ新気が流入するが給気弁6の開口に対してマ
スク壁10が設けられているために新気および燃料は主に
マスク壁10と反対側の給気弁6の開口部から燃焼室4内
に流入する。一方、給気弁6が開弁すると第5図におい
てP2で示されるように排気ポート13内には負圧が発生す
るので燃焼室4の上方部の既燃ガスがこの負圧によって
排気ポート13内に吸い出される。この既燃ガスの移動に
よって新気および燃料は第6図(A)において矢印R1で
示すように排気弁7に向けて引っぱられ、斯くして燃料
が点火栓8(第2図)の周りに導びかれる。次いで第6
図(B)に示すようにピストン2が下降すると燃料を含
んだ新気はR2で示されるように給気弁6下方のシリンダ
内壁面に沿って下方に向かう。しかしながら機関低負荷
運転時は燃焼室4内に流入する新気量が少なくしかも流
入速度が遅いために新気はピストン2の頂面まで達せ
ず、燃焼室4の上方部に滞留している。従ってピストン
2が上昇すると燃焼室4の上方部には混合気が集まり、
燃焼室4の下方部には残留既燃ガスが集まるために燃焼
室4内は成層化されることになる。斯くして混合気が点
火栓8によって確実に着火せしめられることになる。When the air supply valve 6 is opened, fresh air containing fuel flows into the combustion chamber 4 from the air supply port 12, but since the mask wall 10 is provided to the opening of the air supply valve 6, The fuel mainly flows into the combustion chamber 4 through the opening of the air supply valve 6 on the side opposite to the mask wall 10. On the other hand, when the intake valve 6 is opened, a negative pressure is generated in the exhaust port 13 as indicated by P 2 in FIG. 5, so that the burnt gas in the upper portion of the combustion chamber 4 is exhausted by this negative pressure. It is sucked into 13. Due to the movement of the burnt gas, the fresh air and the fuel are pulled toward the exhaust valve 7 as shown by an arrow R 1 in FIG. 6 (A), so that the fuel is around the spark plug 8 (FIG. 2). Be guided to. Then the sixth
As shown in FIG. 3B, when the piston 2 descends, the fresh air containing fuel moves downward along the cylinder inner wall surface below the air supply valve 6 as indicated by R 2 . However, during engine low load operation, the amount of fresh air flowing into the combustion chamber 4 is small and the inflow speed is slow, so the fresh air does not reach the top surface of the piston 2 and remains in the upper portion of the combustion chamber 4. Therefore, when the piston 2 rises, the air-fuel mixture gathers in the upper part of the combustion chamber 4,
Since the residual burned gas collects in the lower portion of the combustion chamber 4, the inside of the combustion chamber 4 is stratified. Thus, the air-fuel mixture is surely ignited by the spark plug 8.
一方、機関高負荷運転時には燃焼圧が高くなるために第
5図においてQ1で示されるように排気ポート13内に発生
する正圧が高くなり、またこの正圧Q1の反射波である負
圧Q2も大きくなる。また、負圧Q2のピークは負圧P2のピ
ークよりも若干遅れて発生する。On the other hand, since the combustion pressure becomes high during engine high load operation, the positive pressure generated in the exhaust port 13 becomes high as indicated by Q 1 in FIG. 5, and the negative pressure which is a reflected wave of this positive pressure Q 1 The pressure Q 2 also increases. Further, the peak of the negative pressure Q 2 occurs slightly later than the peak of the negative pressure P 2 .
機関高負荷運転時には燃焼室4内に流入する新気の量が
多く、しかも流入速度が速くなる。従って排気弁6が開
弁すると多量の新気が高速度で燃焼室4内に流入する。
次いで排気ポート13内に発生する負圧Q2によって燃焼室
4の上方部の既燃ガスが排気ポート13内に吸い出される
と第7図(A)において矢印S1,S2で示されるように新
気は燃焼室4の中心部の方に向きを変える。次いで更に
ピストン2が下降すると第7図(B)においてS3で示さ
れるように新気は給気弁6下方のシリンダ内壁面に沿っ
て下方に向かい、ピストン2の頂面に達する。従って燃
焼室4内の既燃ガスは第7図(B)において矢印Tで示
すように新気により徐々に追いやられて排気ポート13内
に排出され、斯くして燃焼室4内ではループ掃気が行な
われることになる。During engine high load operation, the amount of fresh air flowing into the combustion chamber 4 is large, and the inflow speed is high. Therefore, when the exhaust valve 6 opens, a large amount of fresh air flows into the combustion chamber 4 at high speed.
Next, when the burned gas in the upper portion of the combustion chamber 4 is sucked into the exhaust port 13 by the negative pressure Q 2 generated in the exhaust port 13, as shown by arrows S 1 and S 2 in FIG. 7 (A). The fresh air turns toward the center of the combustion chamber 4. Next, when the piston 2 further descends, the fresh air moves downward along the cylinder inner wall surface below the air supply valve 6 and reaches the top surface of the piston 2 as indicated by S 3 in FIG. 7 (B). Therefore, the burned gas in the combustion chamber 4 is gradually driven by fresh air and discharged into the exhaust port 13 as indicated by an arrow T in FIG. 7 (B). Will be done.
ところで前述したように第1図から第3図に示す実施例
では各給気弁6、各マスク壁10および各給気ポート12は
夫々平面a−aに関して対称に配置されており、夫々実
質的に同一の形状を有する。従って各給気ポート12から
流入する新気の強さは実質的に等しく、しかも燃焼室4
内の形状が平面a−aに関して対称的な形状となってい
るので各給気ポート12から燃焼室4内に流入した新気は
平面a−aに関して対称的なループ状の流れを生ずる。
その結果、新気はきれいなループ状をなして燃焼室4内
を流れることになり、斯くして機関高負荷運転時には強
力なループ掃気が得られることになる。By the way, as described above, in the embodiment shown in FIGS. 1 to 3, the air supply valves 6, the mask walls 10 and the air supply ports 12 are arranged symmetrically with respect to the plane aa, respectively. Have the same shape. Therefore, the strength of the fresh air flowing from each air supply port 12 is substantially equal, and the combustion chamber 4
Since the inner shape is symmetrical with respect to the plane aa, the fresh air flowing into the combustion chamber 4 from each air supply port 12 produces a symmetrical loop-shaped flow with respect to the plane aa.
As a result, the fresh air flows in the combustion chamber 4 in a clean loop shape, and thus a strong loop scavenging can be obtained during engine high load operation.
給気弁6および排気弁7を具えた2サイクル内燃機関で
はこのようなループ掃気が最も掃気効率がよい。また2
サイクル内燃機関では残留既燃ガス量が多く、このよう
に残留既燃ガスが多い場合においても良好な着火燃焼を
確保するためには点火栓8の周りに混合気を集めておく
こと、即ち良好な成層化を行なうことが必要となる。第
1図から第3図に示す実施例ではマスク壁10を設けるこ
とによって新気および混合気がシリンダヘッド3の内壁
面3aに沿って排気ポート13内に流出することがなく、そ
れによって良好なループ掃気を確保できるばかりでな
く、良好な成層化も確保することができる。In a two-cycle internal combustion engine equipped with the air supply valve 6 and the exhaust valve 7, such loop scavenging has the highest scavenging efficiency. Again 2
In a cycle internal combustion engine, the amount of residual burned gas is large, and even when there is a large amount of residual burned gas, it is necessary to collect the air-fuel mixture around the spark plug 8 in order to ensure good ignition combustion. It is necessary to perform proper stratification. In the embodiment shown in FIGS. 1 to 3, the provision of the mask wall 10 prevents the fresh air and the air-fuel mixture from flowing out into the exhaust port 13 along the inner wall surface 3a of the cylinder head 3, which is favorable. Not only can loop scavenging be secured, but good stratification can also be secured.
また、点火栓8を隆起部5に対して給気弁6側に配置す
ることによって点火栓8の周りに混合気が集まりやすく
なり、従って点火栓8による混合気の良好な着火を確保
することができる。特に隆起部5の湾曲中央部5cにより
包囲された領域には混合気が滞留しやすく、この領域内
に点火栓8が配置されているので着火性が向上せしめら
れる。Further, by disposing the spark plug 8 on the side of the air supply valve 6 with respect to the raised portion 5, it becomes easier for the air-fuel mixture to gather around the spark plug 8, so that good ignition of the air-fuel mixture by the spark plug 8 is ensured. You can In particular, the air-fuel mixture is likely to stay in the region surrounded by the curved center portion 5c of the raised portion 5, and the ignition plug 8 is arranged in this region, so that the ignitability is improved.
また、燃焼噴射弁17から噴射された燃料は給気弁6のか
さ部背面に衝突して霧化した後にただちに燃焼室4内に
供給されるので燃焼が給気ポート12の内壁面上に付着す
ることがない。Further, since the fuel injected from the combustion injection valve 17 collides with the rear surface of the bulk portion of the air supply valve 6 and is atomized and immediately supplied into the combustion chamber 4, combustion adheres to the inner wall surface of the air supply port 12. There is nothing to do.
第8図および第9図は更に良好なループ掃気を確保でき
るようにした2サイクル内燃機関の別の実施例を示す。
この実施例ではシリンダヘッド内壁面3a上に凹溝20が形
成され、この凹溝20の底壁面をなすシリンダヘッド内壁
面部分3b上に給気弁6が配置される。一方、凹溝20を除
くシリンダヘッド内壁面部分3cはほぼ平坦をなし、この
シリンダヘッド内壁面部分3c上に排気弁7が配置され
る。シリンダヘッド内壁面部分3bとシリンダヘッド内壁
面部分3cは凹溝20の周壁21を介して互いに接続されてい
る。この凹溝周壁21は給気弁6の周縁部に極めて近接配
置されかつ給気弁6の周縁部に沿って円弧状に延びるマ
スク壁21aと、給気弁6間に位置する新気ガイド壁21b
と、シリンダヘッド内壁面3aの周壁と給気弁6間に位置
する新気ガイド壁21cとにより構成される。各マスク壁2
1aは最大リフト位置にある給気弁6よりも下方まで燃焼
室4に向けて延びており、従って排気弁7側に位置する
給気弁6周縁部と弁座9間の開口は給気弁6の開弁期間
全体に亙ってマスク壁21aにより閉鎖されることにな
る。また、各新気ガイド壁21b,21cはほぼ同一平面内に
位置しており、更にこれらの新気ガイド壁21b,21cは両
給気弁6の中心を結ぶ線に対してほぼ平行に延びてい
る。点火栓8はシリンダヘッド内壁面3aの中心に位置す
るようにシリンダヘッド内壁面部分3c上に配置されてい
る。FIG. 8 and FIG. 9 show another embodiment of the two-cycle internal combustion engine which can ensure better loop scavenging.
In this embodiment, the concave groove 20 is formed on the cylinder head inner wall surface 3a, and the air supply valve 6 is arranged on the cylinder head inner wall surface portion 3b forming the bottom wall surface of the concave groove 20. On the other hand, the cylinder head inner wall surface portion 3c excluding the concave groove 20 is substantially flat, and the exhaust valve 7 is arranged on the cylinder head inner wall surface portion 3c. The cylinder head inner wall surface portion 3b and the cylinder head inner wall surface portion 3c are connected to each other via the peripheral wall 21 of the concave groove 20. The concave groove peripheral wall 21 is arranged very close to the peripheral edge of the air supply valve 6 and extends in an arc shape along the peripheral edge of the air supply valve 6, and a fresh air guide wall located between the air supply valve 6. 21b
And a fresh air guide wall 21c located between the peripheral wall of the cylinder head inner wall surface 3a and the air supply valve 6. Each mask wall 2
1a extends toward the combustion chamber 4 below the intake valve 6 at the maximum lift position, and therefore the opening between the peripheral edge of the intake valve 6 located on the exhaust valve 7 side and the valve seat 9 is an intake valve. It will be closed by the mask wall 21a over the entire 6 valve opening period. Further, the fresh air guide walls 21b and 21c are located substantially in the same plane, and these fresh air guide walls 21b and 21c extend substantially parallel to the line connecting the centers of both air supply valves 6. There is. The spark plug 8 is arranged on the cylinder head inner wall surface portion 3c so as to be located at the center of the cylinder head inner wall surface 3a.
第9図からわかるようにこの実施例においても一対の給
気弁6はシリンダ軸線を含む平面a−aに関して対称に
配置されており、一対の給気ポート12も平面a−aに関
して対称に配置されている。また、各給気弁6の形状は
実質的に同一であり、各給気ポート12の形状も実質的に
同一である。また、各給気弁6の弁リフト曲線は実質的
に同一であり、従って給気弁6が開弁したときに各給気
ポート12から流入する新気の量は実質的に同一となる。
また、各マスク壁21aは平面a−aに関して対称的な形
状を有し、新気ガイド壁21bおよび各新気ガイド壁21cも
夫々平面a−aに関して対称的に配置されている。更に
各マスク壁21aおよび各新気ガイド壁21cは夫々実質的に
同一の形状を有する。また、各排気弁7および各排気ポ
ート13も夫々平面a−aに関して対称的に配置されてお
り、各排気弁7および各排気ポート13は夫々実質的に同
一の形状を有する。As can be seen from FIG. 9, also in this embodiment, the pair of air supply valves 6 are arranged symmetrically with respect to the plane aa including the cylinder axis, and the pair of air supply ports 12 are also arranged symmetrically with respect to the plane aa. Has been done. Further, the shape of each air supply valve 6 is substantially the same, and the shape of each air supply port 12 is also substantially the same. Further, the valve lift curves of the air supply valves 6 are substantially the same, and therefore, when the air supply valves 6 are opened, the amounts of fresh air flowing in from the air supply ports 12 are substantially the same.
Further, each mask wall 21a has a symmetrical shape with respect to the plane aa, and the fresh air guide wall 21b and each fresh air guide wall 21c are also arranged symmetrically with respect to the plane aa. Further, each mask wall 21a and each fresh air guide wall 21c have substantially the same shape. The exhaust valves 7 and the exhaust ports 13 are also arranged symmetrically with respect to the plane aa, and the exhaust valves 7 and the exhaust ports 13 have substantially the same shape.
この実施例では第1図から第3図に示す実施例に比べて
円弧状に延びるマスク壁21aの長さが長く、給気弁6と
その弁座9間に形成される開口のうちで排気弁7側に位
置するほぼ1/3の開口がマスク壁21aにより閉鎖され、排
気弁7と反対側に位置するほぼ2/3の開口から新気が供
給される。更にこの実施例では給気弁6から流入した新
気は新気ガイド壁21b,21cによりシリンダ内壁面に沿っ
て下方に向かうように案内される。従ってこの実施例で
は排気弁6が開弁したときには第10図において矢印Uで
示すように大部分の新気がシリンダ内壁面に沿ってピス
トン2の頂面に向かい、斯くして良好なループ掃気が行
なわれることになる。In this embodiment, the length of the mask wall 21a extending in an arc shape is longer than that in the embodiment shown in FIGS. 1 to 3, and the exhaust gas is exhausted from the opening formed between the air supply valve 6 and its valve seat 9. The mask wall 21a closes the approximately 1/3 opening located on the valve 7 side, and fresh air is supplied from the approximately 2/3 opening located on the opposite side of the exhaust valve 7. Further, in this embodiment, the fresh air flowing from the air supply valve 6 is guided downward by the fresh air guide walls 21b and 21c along the inner wall surface of the cylinder. Therefore, in this embodiment, when the exhaust valve 6 is opened, most of the fresh air flows toward the top surface of the piston 2 along the inner wall surface of the cylinder as indicated by an arrow U in FIG. Will be performed.
ところで第9図および第10図に示す実施例においても各
給気弁6、各給気ポート12、各マスク壁21aおよび各新
気ガイド壁21cは夫々平面a−aに関して対称に配置さ
れており、夫々実質的に同一の形状を有する。従って各
給気ポート12から流入する新気の強さは実質的に等し
く、しかも燃焼室4内の形状が平面a−aに関して対称
的な形状となっているので各給気ポート12から燃焼室4
内に流入した新気は平面a−aに関して対称的なループ
状の流れを生ずる。その結果、この実施例においても新
気はきれいなループ状をなして燃焼室4内を流れること
になり、斯くして機関高負荷運転時には強力なループ掃
気が得られることになる。By the way, also in the embodiment shown in FIGS. 9 and 10, each air supply valve 6, each air supply port 12, each mask wall 21a and each fresh air guide wall 21c are arranged symmetrically with respect to the plane aa. , And each has substantially the same shape. Therefore, the strength of the fresh air flowing in from each air supply port 12 is substantially equal, and the shape of the combustion chamber 4 is symmetrical with respect to the plane aa, so that the air from each air supply port 12 to the combustion chamber Four
The fresh air that has flowed in produces a symmetrical loop-shaped flow with respect to the plane aa. As a result, in this embodiment as well, fresh air flows in the combustion chamber 4 in a clean loop shape, so that strong loop scavenging is obtained during engine high load operation.
なお、これまで本発明を2サイクルガソリン機関に適用
した場合について説明してきたが本発明を2サイクルデ
ィーゼル機関に適用しうることは云うまでもない。Although the present invention has been described so far as applied to a two-cycle gasoline engine, it goes without saying that the present invention can be applied to a two-cycle diesel engine.
排気弁側に位置する給気弁周縁部と弁座間の開口を給気
弁の全開弁期間に亙ってマスク壁により閉鎖しかつ各給
気ポートから実質的に同じ強さで新気を燃焼室内に流入
させ、流入した新気をシリンダ軸線を含む平面に関し対
称的にループ状に流すことによって強力なループ掃気を
確保することができる。The opening between the periphery of the intake valve located on the exhaust valve side and the valve seat is closed by the mask wall for the full opening period of the intake valve, and fresh air is burned with substantially the same strength from each intake port. A strong loop scavenging can be ensured by allowing the fresh air that has flowed into the chamber to flow in a loop shape symmetrically with respect to the plane including the cylinder axis.
第1図は2サイクル内燃機関の側面断面図、第2図はシ
リンダヘッド内壁面を示す図、第3図はシリンダヘッド
の平面断面図、第4図は給排気弁の開弁期間を示す線
図、第5図は給排気弁の弁リフトおよび排気ポート内の
圧力変化を示す図、第6図は低負荷運転時の作動を説明
するための図、第7図は高負荷運転時の作動を説明する
ための図、第8図は別の実施例を示す2サイクル内燃機
関の側面断面図、第9図は第8図のシリンダヘッド内壁
面を示す図、第10図は作動を説明するための図である。 3……シリンダヘッド、4……燃焼室、 5……隆起部、6……給気弁、 7……排気弁、8……点火栓、 10,21a……マスク壁、12……給気ポート。FIG. 1 is a side sectional view of a two-cycle internal combustion engine, FIG. 2 is a view showing an inner wall surface of a cylinder head, FIG. 3 is a plan sectional view of a cylinder head, and FIG. 4 is a line showing an opening period of a supply / exhaust valve. 5 and 5 are views showing the valve lift of the air supply / exhaust valve and changes in pressure in the exhaust port, FIG. 6 is a diagram for explaining the operation during low load operation, and FIG. 7 is the operation during high load operation. FIG. 8 is a side sectional view of a two-cycle internal combustion engine showing another embodiment, FIG. 9 is a view showing the inner wall surface of the cylinder head of FIG. 8, and FIG. 10 is a view for explaining the operation. FIG. 3 ... Cylinder head, 4 ... Combustion chamber, 5 ... Raised part, 6 ... Air supply valve, 7 ... Exhaust valve, 8 ... Spark plug, 10,21a ... Mask wall, 12 ... Air supply port.
Claims (1)
リンダ軸線を含む平面に関して夫々対称に配置すると共
に各給気弁の形状および各給気ポートの形状を夫々実質
的に同一の形状に形成し、シリンダヘッド内壁面から燃
焼室に向けて延びるマスク壁を各給気弁と排気弁との間
に形成して各マスク壁により排気弁側に位置する各給気
弁周縁部と弁座間の開口を給気弁の全開弁期間に亘って
閉鎖し、各マスク壁を上記シリンダ軸線を含む平面に関
して対称に配置すると共に各マスク壁の形状を実質的に
同一の形状に形成した2サイクル内燃機関。1. A pair of air supply valves and a pair of air supply ports are arranged symmetrically with respect to a plane including a cylinder axis, and the shape of each air supply valve and the shape of each air supply port are substantially the same. And a mask wall extending from the inner wall surface of the cylinder head toward the combustion chamber is formed between each air supply valve and the exhaust valve, and each mask wall surrounds each air supply valve peripheral portion and valve located on the exhaust valve side. Two cycles in which the openings of the seats are closed for the full opening period of the air supply valve, the mask walls are arranged symmetrically with respect to the plane including the cylinder axis, and the shapes of the mask walls are formed to be substantially the same. Internal combustion engine.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP20003588A JPH0733771B2 (en) | 1988-08-12 | 1988-08-12 | 2-cycle internal combustion engine |
| US07/391,786 US4945867A (en) | 1988-08-12 | 1989-08-09 | Two-stroke engine |
| DE3926631A DE3926631C2 (en) | 1988-08-12 | 1989-08-11 | Two-stroke engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP20003588A JPH0733771B2 (en) | 1988-08-12 | 1988-08-12 | 2-cycle internal combustion engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH0249923A JPH0249923A (en) | 1990-02-20 |
| JPH0733771B2 true JPH0733771B2 (en) | 1995-04-12 |
Family
ID=16417739
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP20003588A Expired - Fee Related JPH0733771B2 (en) | 1988-08-12 | 1988-08-12 | 2-cycle internal combustion engine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0733771B2 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5140958A (en) * | 1990-06-27 | 1992-08-25 | Toyota Jidosha Kabushiki Kaisha | Two-stroke engine |
-
1988
- 1988-08-12 JP JP20003588A patent/JPH0733771B2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0249923A (en) | 1990-02-20 |
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