JPS5934848B2 - Crank chamber compression type 2-stroke engine - Google Patents

Crank chamber compression type 2-stroke engine

Info

Publication number
JPS5934848B2
JPS5934848B2 JP8421075A JP8421075A JPS5934848B2 JP S5934848 B2 JPS5934848 B2 JP S5934848B2 JP 8421075 A JP8421075 A JP 8421075A JP 8421075 A JP8421075 A JP 8421075A JP S5934848 B2 JPS5934848 B2 JP S5934848B2
Authority
JP
Japan
Prior art keywords
chamber
fuel
piston
crank chamber
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
Application number
JP8421075A
Other languages
Japanese (ja)
Other versions
JPS528219A (en
Inventor
義治 井坂
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.)
Yamaha Motor Co Ltd
Original Assignee
Yamaha Motor Co Ltd
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 Yamaha Motor Co Ltd filed Critical Yamaha Motor Co Ltd
Priority to JP8421075A priority Critical patent/JPS5934848B2/en
Publication of JPS528219A publication Critical patent/JPS528219A/en
Publication of JPS5934848B2 publication Critical patent/JPS5934848B2/en
Expired 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
    • F02B75/00Other engines
    • F02B75/02Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/025Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two

Landscapes

  • Supercharger (AREA)

Description

【発明の詳細な説明】 本発明はクランク室圧縮式2サイクルエンジンに関する
もので、その目的とするところは、この種の2サイクル
エンジンにおいて、燃焼室に生じた既燃ガスの掃気を、
掃気行程の初期には、主と20して空気のみの場合を含
めて燃料成分の少い希薄混合気によつて行ない、次いで
燃料成分の比較的多い濃厚混合気によつて行なうことに
より排気孔から流出する未燃焼混合気の排出量を減少さ
せるとともに燃焼時における燃料の着火性を良好にす5
ることにある。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a crank chamber compression type two-stroke engine, and its purpose is to scavenge burnt gas generated in the combustion chamber in this type of two-stroke engine.
At the beginning of the scavenging stroke, the scavenging stroke is mainly carried out with a lean mixture with a small amount of fuel components, including the case where only air is used, and then with a rich mixture with a relatively large amount of fuel components. This reduces the amount of unburned air-fuel mixture that flows out from the engine and improves the ignitability of the fuel during combustion5.
There are many things.

以下に本発明の第1実施例を図面について説明すると、
第1図において符号10はシリンダを示し、符号20は
ピストンを示している。
The first embodiment of the present invention will be explained below with reference to the drawings.
In FIG. 1, reference numeral 10 indicates a cylinder, and reference numeral 20 indicates a piston.

シリンダ10は、クランクケース11の上部に30固着
されており、その周壁には吸気孔12、排気孔13、4
個の掃気孔14a〜14d及び燃料供給孔31が設けら
れている。
The cylinder 10 is fixed at 30 to the upper part of the crankcase 11, and has an intake hole 12, an exhaust hole 13, and 4 exhaust holes on its peripheral wall.
Scavenging holes 14a to 14d and fuel supply holes 31 are provided.

燃料供給孔31は、掃気孔14a〜14dよりも下刃に
設けられていて、その内端は燃焼室R1に選択的に開口
すると35ともにクラック室R2にビストン20の周壁
に設けた連通孔21を通して選択的に連通し、またその
外端は第2図のごとく、シリンダ10に設けた燃料室R
3の中央部に連通している。燃料室R3は円筒状に形成
されていて、その上端部には第3図に示すごとく、リー
ド弁34を介して気化器33に連通する流入口32が接
線力向に設けられている。なお、この気化器33は公知
の構成のものである。(第1図〜第3図参照)ピストン
20は、シリンダ10内に嵌挿されていて、前記燃料供
給孔31に対応する周側壁には連通孔21が穿設され、
また吸気孔12に対応する周側壁には通気口22が穿設
されている。
The fuel supply hole 31 is provided in the lower blade than the scavenging holes 14a to 14d, and when its inner end is selectively opened to the combustion chamber R1, the communication hole 35 and the communication hole 21 provided in the peripheral wall of the piston 20 are connected to the crack chamber R2. 2, and its outer end communicates selectively through the fuel chamber R provided in the cylinder 10, as shown in FIG.
It is connected to the center of 3. The fuel chamber R3 is formed in a cylindrical shape, and as shown in FIG. 3, an inlet 32 is provided in the upper end of the fuel chamber R3 in the tangential direction, communicating with the carburetor 33 via a reed valve 34. Note that this vaporizer 33 has a known configuration. (See FIGS. 1 to 3) The piston 20 is fitted into the cylinder 10, and a communication hole 21 is bored in the peripheral side wall corresponding to the fuel supply hole 31.
Further, a vent hole 22 is provided in the peripheral side wall corresponding to the intake hole 12 .

しかして、この連通口21の穿設位置は、ピストン上動
時の掃気完了後にクランク室R2内の負圧を燃料供給孔
31に付与し得るとともにピストン下動時の掃気開始前
にクランク室R2内の正圧を燃料供給孔31に付与し得
る位置である。なお、図中符号15は吸気管17、リー
ド弁16を介して吸気孔12に供給される空気量を制御
する絞り弁を示している。
Therefore, the location of the communication port 21 is such that negative pressure in the crank chamber R2 can be applied to the fuel supply hole 31 after the scavenging is completed when the piston moves upward, and at the same time, the negative pressure in the crank chamber R2 can be applied to the fuel supply hole 31 before the scavenging starts when the piston moves downward. This is the position where positive pressure inside can be applied to the fuel supply hole 31. Note that reference numeral 15 in the figure indicates a throttle valve that controls the amount of air supplied to the intake hole 12 via the intake pipe 17 and the reed valve 16.

このように構成した本実施例の作用を第4図を参照して
説明すると、ピストン20が不死?BI)C(第1図に
て示した位置)にあるときには、排気孔13、掃気孔1
4a〜14d及び燃料供給孔31か燃焼室R1に開口し
ているので、排気、掃気、及び燃料(濃混合気)供給が
同時に行なわれている。
The operation of this embodiment configured in this way will be explained with reference to FIG. 4.Is the piston 20 immortal? BI) When in C (position shown in Fig. 1), exhaust hole 13, scavenging hole 1
4a to 14d and the fuel supply hole 31 are open to the combustion chamber R1, so exhaust, scavenging, and fuel (rich mixture) supply are performed at the same time.

しかして、ピストン20が上昇すると、始めに燃料供給
孔31がピストン20の周側壁によつて閉じられ、その
後掃気孔14a〜14dがピストン20の周側壁によつ
て閉じられる。このときには、クランク室R2内に負圧
が生じ、吸気孔12から絞り弁15の開度によつて規定
された量の空気が通気口22を通してクランク室R2内
に流入する。しかるに、掃気孔14a〜14dが閉じた
後には、燃料供給孔31とピストン20の連通孔21が
合致し、クランク室R2内の負圧が燃料供給孔31に付
与される。この負圧は燃料供給孔31より燃料室R3に
付与され、燃料室R3内に残留している混合気が連通孔
21を通してクランク室R2内に吸引されるとともに、
絞り弁15と連動して作動する図示しない第2の絞り弁
を有する気化器33にて生じた濃混合気がリード弁34
を介して燃料室R3内に吸引される。なお、このとき濃
混合気は流入口32から渦流となつて燃料室R,内に流
入する。このように濃混合気が燃料室R3内:ζ吸引さ
れたところには、ピストン20が上)昇して燃料供給孔
31力S再びピストン20の周側壁によつて閉じられて
いる。
When the piston 20 moves up, the fuel supply hole 31 is first closed by the circumferential wall of the piston 20, and then the scavenging holes 14a to 14d are closed by the circumferential wall of the piston 20. At this time, a negative pressure is generated in the crank chamber R2, and an amount of air determined by the opening degree of the throttle valve 15 flows from the intake hole 12 into the crank chamber R2 through the vent hole 22. However, after the scavenging holes 14a to 14d are closed, the fuel supply hole 31 and the communication hole 21 of the piston 20 match, and the negative pressure in the crank chamber R2 is applied to the fuel supply hole 31. This negative pressure is applied to the fuel chamber R3 from the fuel supply hole 31, and the air-fuel mixture remaining in the fuel chamber R3 is sucked into the crank chamber R2 through the communication hole 21.
A rich air-fuel mixture generated in the carburetor 33 having a second throttle valve (not shown) that operates in conjunction with the throttle valve 15 is transferred to the reed valve 34
The fuel is sucked into the fuel chamber R3 through the fuel chamber R3. At this time, the rich air-fuel mixture flows into the fuel chamber R from the inlet 32 in the form of a vortex. In this way, where the rich air-fuel mixture is sucked into the fuel chamber R3, the piston 20 rises and the fuel supply hole 31 is closed again by the circumferential side wall of the piston 20.

このため、燃料室R3内には濃混合気が貯蔵され、クラ
ンク室R2内には残留濃混合気が流入して希薄混合気(
空気に近いもの)が生成される。このとき、燃料室R3
内の濃混合気中の燃料はシリンダ周壁の熱により気化が
促進される。(なお、排気孔13は燃料供給孔31とピ
ストンの連通孔21が合致している間に閉じられる。)
その後、上死点TDCに上昇したピストン20が爆発に
よつて下降すると、クランク室R2内にては希薄混合気
が圧縮される。
Therefore, the rich mixture is stored in the fuel chamber R3, and the residual rich mixture flows into the crank chamber R2, resulting in a lean mixture (
(similar to air) is produced. At this time, fuel chamber R3
The fuel in the rich mixture inside the cylinder is accelerated to vaporize by the heat of the cylinder peripheral wall. (Note that the exhaust hole 13 is closed while the fuel supply hole 31 and the communication hole 21 of the piston are aligned.)
Thereafter, when the piston 20 that has risen to the top dead center TDC descends due to explosion, the lean air-fuel mixture is compressed in the crank chamber R2.

このため、燃料供給孔31が連通孔21と合致したとき
には、クランク室R2内の圧縮された希薄混合気が燃料
供給孔31より燃料室R3内に流入し、燃料室R3内の
濃混合気が加圧される。なお、排気孔13はこの加圧時
に燃焼室R1に開口し、既燃ガスが外部に噴出する。し
かして、ピストン20が掃気孔14a〜14dを開口す
る前には、燃料供給孔31がピストン20の周側壁によ
りクランク室R2に対して閉じられるので、燃料室R3
内に加圧状態の濃混合気が封入貯留される。
Therefore, when the fuel supply hole 31 matches the communication hole 21, the compressed lean mixture in the crank chamber R2 flows into the fuel chamber R3 through the fuel supply hole 31, and the rich mixture in the fuel chamber R3 flows into the fuel chamber R3. Pressurized. Note that the exhaust hole 13 opens into the combustion chamber R1 during this pressurization, and the burnt gas is ejected to the outside. Therefore, before the piston 20 opens the scavenging holes 14a to 14d, the fuel supply hole 31 is closed to the crank chamber R2 by the peripheral side wall of the piston 20, so that the fuel chamber R3
A pressurized concentrated air-fuel mixture is sealed and stored inside.

しかる後、掃気孔14a〜14dが開口し、クランク室
R2内にて加圧された希薄混合気が燃焼室R1内に流入
して残留既燃ガスを排気孔13より外部に排出する。そ
の後、燃料供給孔31が燃焼室R1に開口するので、燃
料室R3内の加圧濃混合気が燃料供給孔31から勢いよ
く燃焼室R1内に噴出し、先に流入した希薄混合気と効
率よく混合して所定の濃度を有する混合気となり、次の
燃焼時の着火性が良好となる。またこのとき、排気孔1
3からは先に掃気孔14a〜14dより流出した希薄混
合気(掃気)のみが外部に流出し、排気ガス中への未燃
焼ガスの流出が減少する。次に第5図〜第8図を参照し
て本発明の第2実施例を説明すると、この実施例におい
ては、シリンダ10の周側壁に、ピストン20の外周壁
に設けた一対の凹部23,23を介して燃料室R3に連
通する一対の副室R4,R4が形成されている。
Thereafter, the scavenging holes 14a to 14d open, the lean air-fuel mixture pressurized in the crank chamber R2 flows into the combustion chamber R1, and the residual burnt gas is discharged to the outside through the exhaust hole 13. After that, the fuel supply hole 31 opens into the combustion chamber R1, so the pressurized rich mixture in the fuel chamber R3 is vigorously jetted out from the fuel supply hole 31 into the combustion chamber R1, and is more efficient than the lean mixture that has flowed in earlier. The mixture is well mixed and has a predetermined concentration, resulting in good ignitability during the next combustion. Also at this time, exhaust hole 1
From No. 3, only the lean air-fuel mixture (scavenging air) that first flowed out from the scavenging holes 14a to 14d flows out to the outside, and the flow of unburned gas into the exhaust gas is reduced. Next, a second embodiment of the present invention will be described with reference to FIGS. 5 to 8. In this embodiment, a pair of recesses 23 provided in the outer circumferential wall of the piston 20 are provided in the circumferential wall of the cylinder 10. A pair of auxiliary chambers R4, R4 are formed which communicate with the fuel chamber R3 via 23.

ー力、ピストン20には、副室R4をクランク室R2に
選択的に連通せしめる一対の第2の連通孔24,24が
穿設されている。また、副室R4,R4は燃料室R3よ
り下刃に設けられていて、燃焼室R1には直接開口する
ことがない。
- The piston 20 is provided with a pair of second communication holes 24, 24 for selectively communicating the auxiliary chamber R4 with the crank chamber R2. Furthermore, the auxiliary chambers R4, R4 are provided lower than the fuel chamber R3, and do not directly open into the combustion chamber R1.

また、凹部23,23は連通孔21より上刃に設けられ
、第2連通孔24,24は連通孔21より下刃に設けら
れている。その他の構成は前述の第1実施例と実質的に
同じであるので同一部分には同一符号を付してその説明
は省略する〇このように構成した本実施例の作用を第8
図を参照して説明すると、ピストン20が下死点BI)
C(第5図にて示した位置)にあるときには、排気孔1
3、掃気孔14a〜14d及び燃料供給孔31が燃焼室
R1に開口しているので、排気、掃気及び燃料供給が同
時に行なわれている。
Further, the recesses 23, 23 are provided in the upper blade than the communication hole 21, and the second communication holes 24, 24 are provided in the lower blade than the communication hole 21. The rest of the structure is substantially the same as the first embodiment described above, so the same parts are given the same reference numerals and the explanation thereof will be omitted.
To explain with reference to the figure, the piston 20 is at the bottom dead center BI)
When in position C (position shown in Figure 5), exhaust hole 1
3. Since the scavenging holes 14a to 14d and the fuel supply hole 31 open into the combustion chamber R1, exhaust, scavenging, and fuel supply are performed simultaneously.

また、このときには副室R4,R4が凹部23,23に
より燃料室R3に連通しているので、副室R4,R4内
の空気は燃料室R3内に残留している濃混合気を伴なつ
て燃焼室R,内に流入する。しかして、ピストン20が
上昇すると、始めに副室R4,R4がピストン20の周
側壁によつて閉じられ、つづいて燃料供給孔31が燃焼
室R1に対して閉じられ、その後掃気孔14a,14d
が閉じられる。このときには、クランク室R2内に負圧
力j生じ、吸気孔12から絞り弁15の開度によつて規
定された量の空気がリード弁16を通してクランク室R
2内に流人する。しかるに、掃気孔14a〜14dが閉
じた直後、燃料室R3及び副室R4,R4がそれぞれ連
通孔21及び第2連通孔24,24と合致し、クランク
室R2内の負圧が燃料室R3及び副室R4,R4にそれ
ぞれ付与される。このため、燃料室R3内の濃混合気及
び副室R4,R4内に残留している希薄混合気がそれぞ
れクランク室R2内に吸引されるとともに、気化器33
にて生じた濃混合気がリード弁34を介して燃料室R3
内に吸引される。このように濃混合気は燃料室R3内に
吸引されているときに副室R4,R4はピストン20の
周側壁によつて再び閉じられ、濃混合気が燃料室R3に
充満したところに燃料室R3がピストン20の周側壁に
よつてクランク室R2に対して再び閉じられる。これに
より燃料室R3内tζは濃混合気が貯留され、副室R4
,R4には負圧が付与される。(なお、排気孔13は燃
料供給孔31とピストンの連通孔21が合致している間
に閉じられる。)その後、上死点TDCに上昇したピス
トン20が爆発によつて下降すると、クランク室R2内
にては希薄混合気が圧縮される。
Also, at this time, since the subchambers R4, R4 communicate with the fuel chamber R3 through the recesses 23, 23, the air in the subchambers R4, R4 is accompanied by the rich air-fuel mixture remaining in the fuel chamber R3. It flows into the combustion chamber R. When the piston 20 rises, first the auxiliary chambers R4 and R4 are closed by the circumferential wall of the piston 20, then the fuel supply hole 31 is closed to the combustion chamber R1, and then the scavenging holes 14a and 14d are closed.
is closed. At this time, a negative pressure j is generated in the crank chamber R2, and an amount of air determined by the opening degree of the throttle valve 15 from the intake hole 12 passes through the reed valve 16 and flows into the crank chamber R.
I'm exiled within 2. However, immediately after the scavenging holes 14a to 14d are closed, the fuel chamber R3 and the auxiliary chambers R4, R4 coincide with the communication hole 21 and the second communication holes 24, 24, respectively, and the negative pressure in the crank chamber R2 is reduced to the fuel chamber R3 and the subchamber R4, R4. These are provided to subchambers R4 and R4, respectively. Therefore, the rich mixture in the fuel chamber R3 and the lean mixture remaining in the auxiliary chambers R4 and R4 are sucked into the crank chamber R2, and the carburetor 33
The rich air-fuel mixture generated in is passed through the reed valve 34 to the fuel chamber R3.
sucked inside. While the rich air-fuel mixture is being drawn into the fuel chamber R3, the auxiliary chambers R4 and R4 are closed again by the circumferential wall of the piston 20, and the fuel chamber is filled with the rich air-fuel mixture into the fuel chamber R3. R3 is again closed to the crank chamber R2 by the circumferential wall of the piston 20. As a result, a rich air-fuel mixture is stored in the fuel chamber R3, and the auxiliary chamber R4
, R4 are applied with negative pressure. (The exhaust hole 13 is closed while the fuel supply hole 31 and the communication hole 21 of the piston are aligned.) Thereafter, when the piston 20, which has risen to the top dead center TDC, descends due to the explosion, the crank chamber R2 Inside, the lean mixture is compressed.

このため、燃料供給孔31が連通孔21と合致したとき
には、クランク室R2内の圧縮混合気が燃料供給孔31
より燃料室R3内に流入し、燃料室R3内の濃混合気が
加圧され、また副室R4,R4が第2連通孔24,24
と合致したときには、クランク室R2内の圧縮混合気が
副室R4,R4内に流入する。排気孔13はこの加圧時
に燃焼室R1に開口し、既燃ガスが外部に噴出する。し
かして、ピストン20が掃気孔14a〜14dを開口す
る前には、燃料供給孔13及び副室R4,R4力S共に
ピストン20の周側壁によりクランク室R2に対して閉
じられるので、燃料室R3内には加圧状態の濃混合気が
封入され、副室R4,R4内には加圧状態の希薄混合気
が封入される。
Therefore, when the fuel supply hole 31 matches the communication hole 21, the compressed air-fuel mixture in the crank chamber R2 flows through the fuel supply hole 31.
The rich mixture in the fuel chamber R3 is pressurized, and the auxiliary chambers R4, R4 are connected to the second communication holes 24, 24.
When it matches, the compressed air-fuel mixture in the crank chamber R2 flows into the auxiliary chambers R4 and R4. The exhaust hole 13 opens into the combustion chamber R1 during this pressurization, and the burnt gas is ejected to the outside. Therefore, before the piston 20 opens the scavenging holes 14a to 14d, both the fuel supply hole 13 and the auxiliary chambers R4 and R4 force S are closed to the crank chamber R2 by the peripheral side wall of the piston 20, so that the fuel chamber R3 A pressurized rich air-fuel mixture is sealed in the subchambers R4, R4, and a pressurized lean air-fuel mixture is sealed in the auxiliary chambers R4 and R4.

しかる後、掃気孔14a〜14dが開口し、クランク室
R2内にて加圧された希薄混合気が燃焼室R1内に流入
して残留既燃ガスを排気孔13より外部に排出する。そ
の後、燃料供給孔31が燃焼室R1に開口し、一力副室
R4,R4がピストン20に設けた凹部2323を介し
て燃料室R2に連通するので、燃料室R3内に貯留され
ていた濃混合気が自刃で燃焼室R1内に噴出するととも
に副室R4,R4内の加圧状態の希薄混合気によつて押
出され確実に燃焼室R1内に流入する。このため、燃焼
室R1内には、所定量の燃料が確実にしかも勢いよく供
給され、燃焼室内の空気と効率よく混合して燃焼時の着
火性が良好となる。なお、この第2実施例においては、
副室R4,R4を設けたので、ピストン上昇時にクラン
ク室R2内に流入する気体を略空気のみとすることがで
き、掃気時に排気孔13より外部に流出する未燃ガス量
を更に減少させることができる。以上詳述したとおり、
本発明においては上記各実施例針こて例示したことく、
燃料供給孔31(燃料室R3の開口)がクランク室圧縮
行程時(ピストンの下動時)にピストン20の連通孔2
1を通してクランク室R2に連通したときクランク室R
2内′ζ生じた圧縮状態の希薄混合気により燃料室R2
内の濃混合気を圧縮し、また燃料供給孔31が燃焼室圧
縮行程時(ピストンの上動時)にピストン20の連通孔
21を通してクランク室R2に連通したときクランク室
R2内に生じた負圧によ,り気化器33から一逆市弁3
4を通して濃混合気を燃料室R3内に吸入させるように
して、掃気行程の初期には主としてクランク室R2内に
吸入された空気により掃気を行ないその後に燃料室R3
内の濃混合気を燃焼室R1内に噴出するようにした点に
その特徴があり、これにより排気孔から流出する未燃焼
混合気の排出量を減少させることができるとともに燃焼
時における燃料の着火性を艮好にすることができる。
Thereafter, the scavenging holes 14a to 14d open, the lean air-fuel mixture pressurized in the crank chamber R2 flows into the combustion chamber R1, and the residual burnt gas is discharged to the outside through the exhaust hole 13. Thereafter, the fuel supply hole 31 opens into the combustion chamber R1, and the sub-chambers R4, R4 communicate with the fuel chamber R2 via the recess 2323 provided in the piston 20, so that the rich fuel stored in the fuel chamber R3 is removed. The air-fuel mixture is injected into the combustion chamber R1 by its own blade, and is pushed out by the pressurized lean air-fuel mixture in the auxiliary chambers R4 and R4, and reliably flows into the combustion chamber R1. Therefore, a predetermined amount of fuel is reliably and vigorously supplied into the combustion chamber R1, and is efficiently mixed with the air in the combustion chamber, resulting in good ignitability during combustion. In addition, in this second embodiment,
Since the auxiliary chambers R4 and R4 are provided, the gas that flows into the crank chamber R2 when the piston rises can be almost exclusively air, and the amount of unburned gas flowing out from the exhaust hole 13 during scavenging can be further reduced. I can do it. As detailed above,
In the present invention, as illustrated in each of the above-mentioned embodiments of the needle trowel,
When the fuel supply hole 31 (opening of the fuel chamber R3) is connected to the communication hole 2 of the piston 20 during the crank chamber compression stroke (during the downward movement of the piston)
When communicating with the crank chamber R2 through 1, the crank chamber R
2'ζ Due to the compressed lean mixture generated in the fuel chamber R2
When the fuel supply hole 31 communicates with the crank chamber R2 through the communication hole 21 of the piston 20 during the combustion chamber compression stroke (when the piston moves upward), the negative energy generated in the crank chamber R2 is compressed. Depending on the pressure, from the vaporizer 33 to the reverse city valve 3
At the beginning of the scavenging stroke, the air sucked into the crank chamber R2 is used to perform scavenging, and then the air is drawn into the fuel chamber R3.
The feature is that the rich mixture inside the combustion chamber is injected into the combustion chamber R1, which makes it possible to reduce the amount of unburned mixture flowing out from the exhaust hole, and also to reduce the ignition of fuel during combustion. You can make your sexuality look better.

また、本発明を上記第2実施例のごとく実施した場合に
は、排気孔からの未燃ガスの流出量を更に減少させたの
で、前記副室内に供給されるクランク室内の圧縮状態の
希薄混合気により前記燃料室内の濃混合気を燃焼室内へ
よソー層円滑に供給して燃焼室内における燃料の着火性
を高めることができる。
Further, when the present invention is implemented as in the second embodiment, the amount of unburned gas flowing out from the exhaust hole is further reduced, so that the compressed state in the crank chamber supplied to the pre-chamber is diluted. The rich air-fuel mixture in the fuel chamber can be smoothly supplied into the combustion chamber by air, thereby improving the ignitability of the fuel in the combustion chamber.

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

第1図は本発明の第1実施例を示す縦断面図,第2図は
第1図の2−2線に沿つてみた横断底面図、第3図は第
2図の3−3線に沿つてみた縦断面図、第4図は第1実
施例の作動説明図であつて各孔の開閉時期を示す図であ
る。 また第5図は本発明の第2実施例を示す縦断面図、第6
図は燃料室と副室の連通状態を示す横断平面図、第7図
は副室とクランク室の連通状態を示す横断平面図、第8
図は第2実施例の作動説明図であつて各孔及び副室の開
閉時期を示す図である。符号の説明、10・・・・・シ
リンダ、11・・・・・・クランクケース、12・・・
・・・吸気孔、13・・・・・・排気孔、14a,14
d・・・・・・掃気孔、15・・・・・・絞り弁、17
・・・・・・吸気管、20・・・・・・ピストン、21
・・・・・・連通孔、23・・・・・・凹部、24・・
・・・・第2連通孔、31・・・・・・燃料供給孔(燃
料室の開口)、33・・・・・・気化器、34・・・・
・・リード弁(逆止弁)、R1・・・・・・燃焼室、R
2・・・・・・クランク室、R3・・・・・・燃料室、
R4・・・・・・副室。
Fig. 1 is a vertical sectional view showing a first embodiment of the present invention, Fig. 2 is a cross-sectional bottom view taken along line 2-2 in Fig. 1, and Fig. 3 is a cross-sectional bottom view taken along line 3-3 in Fig. 2. FIG. 4, a longitudinal sectional view taken along the line, is an explanatory diagram of the operation of the first embodiment, and is a diagram showing the timing of opening and closing of each hole. Further, FIG. 5 is a vertical sectional view showing the second embodiment of the present invention, and FIG.
The figure is a cross-sectional plan view showing the state of communication between the fuel chamber and the sub-chamber, FIG. 7 is a cross-sectional plan view showing the state of communication between the sub-chamber and the crank chamber, and FIG.
The figure is an explanatory diagram of the operation of the second embodiment, and is a diagram showing the opening/closing timing of each hole and subchamber. Explanation of symbols: 10...Cylinder, 11...Crankcase, 12...
...Intake hole, 13...Exhaust hole, 14a, 14
d...Scavenging hole, 15... Throttle valve, 17
...Intake pipe, 20...Piston, 21
...Communication hole, 23...Recess, 24...
...Second communication hole, 31...Fuel supply hole (opening of fuel chamber), 33...Carburizer, 34...
... Reed valve (check valve), R1 ... Combustion chamber, R
2... Crank chamber, R3... Fuel chamber,
R4... Antechamber.

Claims (1)

【特許請求の範囲】 1 クランク室圧縮式2サイクルエンジンにおいて、該
エンジンの吸気孔にクランク室内に空気のみの場合を含
む比較的希薄な混合気を流入させる吸気管を取付け、か
つシリンダ周壁の一部に逆止弁を通して比較的濃厚な混
合気が供給される燃料室を設けてこの燃料室を該エンジ
ンの掃気孔の下刃に位置するシリンダの内周壁に開口さ
せ、この燃料室の開口がピストン周壁に設けた連通孔を
介してクランク室圧縮行程時と燃焼室圧縮行程時とに開
閉自在にクランク室内へ連通するようにし、その開閉時
期を、クランク室圧縮行程時にはクランク室内に生じた
圧縮混合気により前期燃料室内の混合気を圧縮し、また
燃焼室圧縮行程時にはクランク室内に生じた負圧により
前記燃料室内に前記逆上弁を通して混合気を吸入させる
ように設定して、掃気行程の初期には主として前記吸気
孔を通してクランク室内に吸入された希薄混合気により
掃気を行ないその後に前記燃料室内の濃厚混合気を燃焼
室内に供給するようにしたことを特徴とする2サイクル
エンジン。 2 前記燃料室の側部に少なくとも一個の副室を形成し
てこの副室を前記燃料室の開口の下方に位置するシリン
ダの内周壁に開口させ、一方前記ピストンの周壁に該ピ
ストンが不死点近傍に達したとき前記副室の開口を前記
燃料室に連通させる凹所を設け、前記副室の開口をピス
トンの周壁に設けた連通孔を介して間欠的にクランク室
内に連通させるようにし、その連通時期をクランク室圧
縮行程時であつて前記凹所が副室の開口を燃料室に連通
させる時期前にクランク室内に生じた圧縮混合気を前記
副室内に付与するように設定し、その後に前記燃料室の
開口が前記燃焼室内に開口したとき前記副室の開口を前
記ピストンの凹所を介して前記燃料室内に連通させるよ
うにしたことを特徴とする特許請求の範囲第1項に記載
のクランク室圧縮式2サイクルエンジン。
[Scope of Claims] 1. In a crank chamber compression type two-stroke engine, an intake pipe is attached to the intake hole of the engine for introducing a relatively lean air-fuel mixture, including the case where only air is present, into the crank chamber, and one part of the cylinder peripheral wall is installed. A fuel chamber to which a relatively rich air-fuel mixture is supplied through a check valve is provided in the engine, and this fuel chamber is opened to the inner circumferential wall of the cylinder located at the lower blade of the scavenging hole of the engine. Through a communication hole provided in the piston peripheral wall, communication is made into the crank chamber so that it can be opened and closed during the crank chamber compression stroke and during the combustion chamber compression stroke, and the timing of opening and closing is determined based on the compression generated in the crank chamber during the crank chamber compression stroke. The air-fuel mixture in the first fuel chamber is compressed by the air-fuel mixture, and during the combustion chamber compression stroke, the air-fuel mixture is set to be sucked into the fuel chamber through the reverse valve by the negative pressure generated in the crank chamber during the scavenging stroke. A two-stroke engine characterized in that initially, scavenging is performed mainly by a lean mixture sucked into a crank chamber through the intake hole, and then a rich mixture in the fuel chamber is supplied into a combustion chamber. 2. At least one auxiliary chamber is formed in a side part of the fuel chamber, and the auxiliary chamber is opened to an inner circumferential wall of the cylinder located below the opening of the fuel chamber, while the piston is formed on the circumferential wall of the piston at an indestructible point. A recess is provided that communicates the opening of the sub-chamber with the fuel chamber when the piston reaches the vicinity, and the opening of the sub-chamber is intermittently communicated with the crank chamber through a communication hole provided in the peripheral wall of the piston. The communication timing is set so that the compressed air-fuel mixture generated in the crank chamber is applied to the sub-chamber during the crank chamber compression stroke and before the time when the recess communicates the opening of the sub-chamber with the fuel chamber, and then Claim 1, characterized in that when the opening of the fuel chamber opens into the combustion chamber, the opening of the auxiliary chamber communicates with the fuel chamber through a recess of the piston. Crank chamber compression type two-stroke engine as described.
JP8421075A 1975-07-08 1975-07-08 Crank chamber compression type 2-stroke engine Expired JPS5934848B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP8421075A JPS5934848B2 (en) 1975-07-08 1975-07-08 Crank chamber compression type 2-stroke engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP8421075A JPS5934848B2 (en) 1975-07-08 1975-07-08 Crank chamber compression type 2-stroke engine

Publications (2)

Publication Number Publication Date
JPS528219A JPS528219A (en) 1977-01-21
JPS5934848B2 true JPS5934848B2 (en) 1984-08-24

Family

ID=13824107

Family Applications (1)

Application Number Title Priority Date Filing Date
JP8421075A Expired JPS5934848B2 (en) 1975-07-08 1975-07-08 Crank chamber compression type 2-stroke engine

Country Status (1)

Country Link
JP (1) JPS5934848B2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2220031B (en) * 1988-06-25 1992-07-01 T & N Technology Ltd Pistons

Also Published As

Publication number Publication date
JPS528219A (en) 1977-01-21

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