JPH07133724A - Combustion equipment of gasoline engine - Google Patents

Combustion equipment of gasoline engine

Info

Publication number
JPH07133724A
JPH07133724A JP28116693A JP28116693A JPH07133724A JP H07133724 A JPH07133724 A JP H07133724A JP 28116693 A JP28116693 A JP 28116693A JP 28116693 A JP28116693 A JP 28116693A JP H07133724 A JPH07133724 A JP H07133724A
Authority
JP
Japan
Prior art keywords
fuel
valve
air
closed
injection
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.)
Withdrawn
Application number
JP28116693A
Other languages
Japanese (ja)
Inventor
Shunichi Mori
俊一 森
Hiroshi Nakagawa
洋 中川
Yuji Oda
裕司 小田
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries 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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP28116693A priority Critical patent/JPH07133724A/en
Publication of JPH07133724A publication Critical patent/JPH07133724A/en
Withdrawn legal-status Critical Current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
    • F02B75/12Other methods of operation
    • F02B2075/125Direct injection in the combustion chamber for spark ignition engines, i.e. not in pre-combustion chamber
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/08Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition
    • F02B23/10Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition with separate admission of air and fuel into cylinder
    • F02B23/101Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition with separate admission of air and fuel into cylinder the injector being placed on or close to the cylinder centre axis, e.g. with mixture formation using spray guided concepts

Abstract

PURPOSE:To prolong injection periods of fuel and air, respectively, and moderate their high responsiveness by attaching a fuel holding chamber to the front part of a combustion chamber and interposing an opening-out type mixture injection valve between the two chambers while providing a fuel valve and an air valve of respectively electromagnetic open/close types inside the fuel holding chamber. CONSTITUTION:An electromagnetic open/close fuel valve 5 is opened when a piston 11 goes into its expansion stroke. On the other hand, an electromagnetic open/close air valve 8 is closed. A mixture injection valve 9 communicating with a combustion chamber 12a is also closed. The electromagnetic open/close fuel valve 5 is taken closed, by metering the required fuel, during a period from the intake stroke until the exhaust port is closed. Now that the exhaust port is closed, air is guided into a fuel holding chamber 9a by opening the electromagnetic open/close air valve 8, the opening-out type mixture injection valve 9 is pushed opened to the combustion chamber 12a side by raising the pressure and the mixture is injected into the combustion chamber 12a by atomizing it with air. When the compression stroke comes close to its end, the opening-out type mixture injection valve 9 is automatically closed and injection is completed.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は、ガソリンエンジンの燃
焼装置に関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a combustion device for a gasoline engine.

【0002】[0002]

【従来の技術】従来の小型高速2サイクルガソリンエン
ジンのシリンダ内噴射燃焼装置を図4〜図6により説明
すると、112がエンジン上部のシリンダヘッドで、同
シリンダヘッド112は、燃焼室112aが設けられ、
そこには、電磁開閉燃料弁105と電磁開閉空気弁10
9と点火プラグ113とが設けられている。
2. Description of the Related Art A conventional in-cylinder injection combustion device for a small high-speed two-cycle gasoline engine will be described with reference to FIGS. 4 to 6. Reference numeral 112 denotes a cylinder head above the engine, and the cylinder head 112 is provided with a combustion chamber 112a. ,
There are an electromagnetic opening / closing fuel valve 105 and an electromagnetic opening / closing air valve 10.
9 and a spark plug 113 are provided.

【0003】そして電磁開閉燃料弁105と電磁開閉空
気弁109出口の通路部112bとが燃焼室112aに
開口しており、電磁開閉燃料弁105から噴射された燃
料が電磁開閉空気弁109から噴射された空気により、
微細化されて、燃焼室112aへ噴射され、圧縮行程の
終わり頃のTDC付近で点火プラグ113のスパークに
より混合気に点火されて、燃焼する。以上の燃焼装置
は、所謂空気アシスト式シリンダ内噴射燃焼装置であ
る。
The electromagnetic opening / closing fuel valve 105 and the passage portion 112b at the outlet of the electromagnetic opening / closing air valve 109 are open to the combustion chamber 112a, and the fuel injected from the electromagnetic opening / closing fuel valve 105 is injected from the electromagnetic opening / closing air valve 109. By the air
It is atomized, injected into the combustion chamber 112a, and ignited in the air-fuel mixture by the spark of the spark plug 113 near the end of the compression stroke and burned. The above combustion device is a so-called air-assisted in-cylinder injection combustion device.

【0004】燃料は、燃料タンク101の燃料を供給ポ
ンプ102により、数kgf/cm 2 に加圧して、燃料
レギュレータ103により調圧後、電磁開閉燃料弁10
5を経て噴射される。この電磁開閉燃料弁105は、制
御装置115に電気的に接続され、エンジンクランク軸
回転角センサー116によりクランク角度信号を基準に
噴射時期、噴射期間(量)が制御される。
The fuel is supplied from the fuel tank 101.
Depending on the pump 102, several kgf / cm 2Pressurize to fuel
After the pressure is adjusted by the regulator 103, the electromagnetic opening / closing fuel valve 10
It is injected through 5. This electromagnetic opening / closing fuel valve 105
Electrically connected to the control device 115, and the engine crankshaft
Based on the crank angle signal by the rotation angle sensor 116
The injection timing and injection period (amount) are controlled.

【0005】空気は、空気溜106の空気を空気レギュ
レータ107により、数kgf/cm2 に調圧して、電
磁開閉空気弁109を経て噴射される。この電磁開閉空
気弁109は、制御装置115に電気的に接続され、電
磁開閉燃料弁105と同様に、エンジンクランク軸回転
角センサー116によりクランク角度信号を基準に噴射
時期、噴射期間(量)が制御される。
The air in the air reservoir 106 is adjusted to several kgf / cm 2 by an air regulator 107 and is injected through an electromagnetic opening / closing air valve 109. The electromagnetic opening / closing air valve 109 is electrically connected to the control device 115, and similarly to the electromagnetic opening / closing fuel valve 105, the engine crankshaft rotation angle sensor 116 sets the injection timing and the injection period (amount) on the basis of the crank angle signal. Controlled.

【0006】燃料の噴射時期は、小形2サイクルガソリ
ンエンジンでは、燃料の吹き抜けをなくすため、排気ポ
ートが閉止するTDC後、220°CA以後、開弁す
る。また燃料の噴射期間は、噴射弁の噴射孔面積、噴射
圧力とともに噴射を制御するもので、同一噴射弁では、
噴射期間により噴射量(負荷)を制御し、略5°CA〜
40°CA(アイドル〜最大噴射量)になる。一方、空
気の噴射時期、噴射期間は、燃料と略同一になるように
制御される。
In a small two-stroke gasoline engine, the fuel injection timing is to open the valve after 220 ° CA after TDC when the exhaust port is closed in order to prevent the fuel blow-through. Further, the fuel injection period controls the injection together with the injection hole area of the injection valve and the injection pressure.
The injection amount (load) is controlled by the injection period, and is approximately 5 ° CA
It becomes 40 ° CA (idle to maximum injection amount). On the other hand, the injection timing and injection period of air are controlled to be substantially the same as the fuel.

【0007】このように小型高速2サイクルエンジンの
シリンダ内噴射燃焼装置では、制御された燃料及び空気
が排気ポートの閉止後、略5°CA〜40°CAの圧縮
行程の初期の短期間に燃料室内へ噴射されて、圧縮TD
C前に点火、燃焼するようにしている。
As described above, in the in-cylinder injection combustion device for a small high speed two-cycle engine, the controlled fuel and air are injected into the fuel in a short period in the early stage of the compression stroke of about 5 ° CA to 40 ° CA after the exhaust port is closed. It is injected into the room and compressed TD
I ignite and burn before C.

【0008】[0008]

【発明が解決しようとする課題】小型高速の2サイクル
ガソリンエンジンは、排気量約50cc/1cyl、回
転数10000rpmを越えるものも多く、このクラス
のシリンダ内噴射燃焼装置において、小量の燃料噴射量
を短時間に精度よく(約0.2s、0.5mm3/s
t)噴射する電磁開閉燃料弁は、電磁力を強くするた
め、非常に高電圧を必要として、実際には殆ど生産され
ていない。
Many small and high speed two-stroke gasoline engines have a displacement of about 50 cc / 1 cyl and a rotational speed of over 10000 rpm. Therefore, in this class of in-cylinder injection combustion device, a small amount of fuel injection is required. Accurately in a short time (about 0.2 s, 0.5 mm 3 / s
t) The electromagnetic opening / closing fuel valve for injection requires a very high voltage in order to strengthen the electromagnetic force, and in reality, it is scarcely produced.

【0009】従来使用されている電磁開閉燃料弁は、噴
射量が最小2mm3 /st程度で、この電磁開閉燃料弁
もその高応答性を得るため、電磁開閉燃料弁内のばね力
を弱くしており、このため、燃料供給圧も2〜3kg/
cm2 程度に低く設定されている。従って燃焼室内の圧
縮圧力が燃料噴射圧力以上になると、噴射できず、その
ため、圧縮行程の初期に噴射を終了する必要がある。
In the conventional electromagnetic opening / closing fuel valve, the injection amount is about 2 mm 3 / st at the minimum, and this electromagnetic opening / closing fuel valve also obtains its high response, so the spring force in the electromagnetic opening / closing fuel valve is weakened. Therefore, the fuel supply pressure is also 2-3 kg /
It is set as low as cm 2 . Therefore, if the compression pressure in the combustion chamber becomes equal to or higher than the fuel injection pressure, the injection cannot be performed, and therefore, it is necessary to end the injection at the beginning of the compression stroke.

【0010】電磁開閉空気弁も同様で、高応答性を得る
ため、空気圧力を高く設定できず、そのため、同じく圧
縮行程の初期に空気噴射を終了する必要がある。小型高
速の2サイクルエンジンの燃焼装置では、掃気ポートと
排気ポートとが同時に開く、所謂オーバラップ期間での
燃料の吹き抜けを減少(未燃燃料(HC)の排出量を減
少)させるため、燃料噴射時期を排気ポート終了後(圧
縮行程始め)に行うことが重要であるため、前記の理由
と相挨って噴射期間が極短時間に限られる。
The same applies to the electromagnetic on-off air valve, and in order to obtain a high response, the air pressure cannot be set high, so that it is necessary to end the air injection at the beginning of the compression stroke as well. In a small-sized high-speed two-cycle engine combustion device, fuel injection is performed in order to reduce blow-through of fuel in a so-called overlap period in which a scavenging port and an exhaust port are simultaneously opened (reduction of unburned fuel (HC) emissions). Since it is important to carry out the timing after the end of the exhaust port (beginning of the compression stroke), the injection period is limited to an extremely short time in addition to the above reason.

【0011】このように短時間に少量の燃料噴射、空気
噴射を行う必要があるが、実際には、前記のように高速
で応答制御可能な電磁式噴射弁が製作できないため、比
較的応答性の悪い電磁弁で対応して、排気ポートが閉止
する前に比較的早く燃料及び空気を噴射し、噴射期間を
長くとるようにしている。このため、未燃燃料(HC)
の排気への吹き抜けによる排ガスの汚染及び燃費率の悪
化が問題になっている。
Thus, it is necessary to inject a small amount of fuel and air in a short time, but in reality, as described above, it is not possible to manufacture an electromagnetic injection valve capable of high-speed response control, and therefore relatively responsive. The fuel valve and the air are injected relatively quickly before the exhaust port is closed, and the injection period is extended. Therefore, unburned fuel (HC)
There is a problem that exhaust gas is polluted by exhaust gas and the fuel efficiency is deteriorated.

【0012】本発明は前記の問題点に鑑み提案するもの
であり、その目的とする処は、電磁開閉燃料弁及び電磁
開閉空気弁の高応答性を大幅に緩和できる。また未燃ガ
スの吹き抜けを大幅に減少できるとともに、燃料消費率
を大幅に低減できる。さらに燃焼ガスによる電磁開閉燃
料弁及び電磁開閉空気弁の損傷を少なくできるガソリン
エンジンの燃焼装置を提供しようとする点にある。
The present invention has been proposed in view of the above problems, and the object thereof is to significantly reduce the high responsiveness of the electromagnetic opening / closing fuel valve and the electromagnetic opening / closing air valve. In addition, the blow-through of unburned gas can be greatly reduced and the fuel consumption rate can be greatly reduced. Another object of the present invention is to provide a combustion device for a gasoline engine, which can reduce damage to the electromagnetic opening / closing fuel valve and the electromagnetic opening / closing air valve due to combustion gas.

【0013】[0013]

【課題を解決するための手段】上記の目的を達成するた
めに、本発明は、シリンダの燃焼室内に直接燃料を噴射
し、点火して、燃焼させるガソリンエンジンの燃焼装置
において、前記燃焼室の前部に燃料溜室を設け、同燃料
溜室と燃焼室との間に常時はばね力により閉止し且つ両
室の圧力差で開閉する外開き式混合気噴射弁を設けると
ともに、同燃料溜室内にそれぞれ制御装置によりエンジ
ン回転角信号を基準にサイクル毎に燃料及び空気の噴射
時期及び期間が制御される電磁開閉燃料弁及び電磁開閉
空気弁を設けている。
In order to achieve the above object, the present invention provides a gasoline engine combustion apparatus for injecting, igniting and burning fuel directly into a combustion chamber of a cylinder. A fuel storage chamber is provided in the front part, and an externally open air-fuel mixture injection valve that is normally closed by spring force and opens and closes due to the pressure difference between the fuel storage chamber and the combustion chamber is provided between the fuel storage chamber and the combustion chamber. An electromagnetic opening / closing fuel valve and an electromagnetic opening / closing air valve, in which the injection timing and period of fuel and air are controlled for each cycle by a control device based on the engine rotation angle signal, are provided in the room.

【0014】前記ガソリンエンジンの燃焼装置におい
て、制御装置により、前サイクルの燃焼終了後より次サ
イクルの圧縮工程に入るまでの間に前記電磁開閉燃料弁
を開閉して前記燃料溜室内に必要量の燃料を噴射すると
ともに、次サイクルの圧縮工程に入った後に前記電磁開
閉空気弁を開いて前記燃料溜室内に空気を噴射し、同燃
料溜室内の圧力上昇により前記混合気噴射弁を自動的に
開いて燃焼室内に混合気を噴射し、燃焼室内圧縮圧力の
上昇で前記混合気噴射弁を閉じ、混合気が着火燃焼し、
膨張行程で燃料室内圧力が空気噴射圧力よりも低下する
以前に前記電磁開閉空気弁を閉止するように制御しても
よい。
In the gasoline engine combustion apparatus, a control device opens and closes the electromagnetic opening / closing fuel valve between the end of combustion in the previous cycle and the start of the compression process in the next cycle, thereby controlling the required amount of fuel in the fuel storage chamber. While injecting fuel, after opening the compression process of the next cycle, the electromagnetic on-off air valve is opened to inject air into the fuel storage chamber, and the mixture injection valve is automatically operated by the pressure increase in the fuel storage chamber. Open and inject the air-fuel mixture into the combustion chamber, close the air-fuel mixture injection valve due to increase in the compression pressure in the combustion chamber, the air-fuel mixture ignites and burns,
The electromagnetic on-off air valve may be controlled to be closed before the fuel chamber pressure becomes lower than the air injection pressure in the expansion stroke.

【0015】[0015]

【作用】本発明のガソリンエンジンの燃焼装置は前記の
ように構成されており、制御装置により電磁開閉燃料弁
がエンジン回転角信号に同期して制御されるが、いま、
ピストンが膨張行程に入ると、電磁開閉燃料弁が開弁す
る。このとき、電磁開閉空気弁は、閉止している。また
燃焼室に連通した混合気噴射弁もシリンダ内圧力により
押圧されて、閉止している。電磁開閉燃料弁は、給気行
程から排気ポートが閉止するまでの期間、必要燃料をメ
ータリングして、閉止される。排気ポートが閉止される
と、制御装置により電磁開閉空気弁が開き、燃料溜室に
空気が導入され、空気溜室内の圧力が上昇して、比較的
弱いばね力により閉止されていた外開き式混合気噴射弁
が燃焼室側に押し開かれ、混合気が空気により霧化され
て、燃焼室に噴出する。圧縮行程が終わりに近づくと、
シリンダ内の圧力が上昇して、燃料溜室の空気圧よりも
高くなると、外開き式混合気噴射弁が自動的に閉止し
て、噴射が終了する。燃焼室内の混合気は、蒸発し、や
がてTDC近傍で点火プラグにより点火され、燃焼室全
体に火炎が伝播して、膨張行程に入り、やがて燃焼が終
了する。一方、膨張行程でのシリンダ内の圧力が噴射空
気圧以下になる前に電磁開閉空気弁が閉止する。この電
磁開閉空気弁が閉止後、電磁開閉燃料弁が再び開かれ
て、同様の制御サイクルが繰り返し行われる。
The gasoline engine combustion apparatus of the present invention is constructed as described above, and the electromagnetic on-off fuel valve is controlled by the control unit in synchronization with the engine rotation angle signal.
When the piston enters the expansion stroke, the electromagnetic opening / closing fuel valve opens. At this time, the electromagnetic opening / closing air valve is closed. Further, the air-fuel mixture injection valve communicating with the combustion chamber is also closed by being pressed by the cylinder internal pressure. The electromagnetic on-off fuel valve is closed by metering the required fuel during the period from the supply stroke to the closing of the exhaust port. When the exhaust port is closed, the electromagnetic opening / closing air valve is opened by the control device, air is introduced into the fuel storage chamber, the pressure in the air storage chamber rises, and it is closed by a relatively weak spring force. The air-fuel mixture injection valve is pushed toward the combustion chamber side, and the air-fuel mixture is atomized by air and ejected into the combustion chamber. Near the end of the compression stroke,
When the pressure in the cylinder rises and becomes higher than the air pressure in the fuel storage chamber, the outward-opening type mixture injection valve automatically closes, and the injection ends. The air-fuel mixture in the combustion chamber evaporates and is eventually ignited by the spark plug in the vicinity of TDC, the flame propagates throughout the combustion chamber, enters the expansion stroke, and eventually the combustion ends. On the other hand, the electromagnetic opening / closing air valve is closed before the pressure in the cylinder in the expansion stroke becomes equal to or lower than the injection air pressure. After the electromagnetic opening / closing air valve is closed, the electromagnetic opening / closing fuel valve is opened again, and the same control cycle is repeated.

【0016】[0016]

【実施例】次に本発明のガソリンエンジンの燃焼装置を
図1〜図3に示す一実施例により説明する。図1の10
がエンジン本体で、同エンジン本体10のシリンダヘッ
ド12の上部に形成される燃焼室12aには、点火プラ
グ13と外開き式混合気噴射弁9とが設けられている。
この外開き式混合気噴射弁9の上部内には、図2に示す
ように燃料溜室9aが設けられ、その下部には、ばね9
cにより閉止された外開き弁9bが設けられ、この外開
き弁9bが燃焼室12aに対面している。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Next, a combustion apparatus for a gasoline engine according to the present invention will be described with reference to an embodiment shown in FIGS. 1 of FIG.
Is a main body of the engine, and a combustion chamber 12a formed in an upper portion of a cylinder head 12 of the main body of the engine 10 is provided with an ignition plug 13 and an outward-opening mixture gas injection valve 9.
As shown in FIG. 2, a fuel storage chamber 9a is provided in the upper portion of the outwardly opening type air-fuel mixture injection valve 9, and a spring 9 is provided in the lower portion thereof.
An outer opening valve 9b closed by c is provided, and the outer opening valve 9b faces the combustion chamber 12a.

【0017】上記燃料溜室9aの上部には、電磁開閉燃
料弁5及び電磁開閉空気弁8が設けられている。電磁開
閉燃料弁5は、一般の小型電磁弁で、制御装置15と電
気的に接続されている。また電磁開閉空気弁8は、制御
装置15と電気的に接続されている。上記制御装置15
には、エンジンククランク角度センサー16からのエン
ジン回転角信号(ピストン位置信号)が入力し、ピスト
ン位置に同期して、電磁開閉燃料弁5及び電磁開閉空気
弁8の開閉時期が制御されるようになっている。
An electromagnetic opening / closing fuel valve 5 and an electromagnetic opening / closing air valve 8 are provided above the fuel storage chamber 9a. The electromagnetic opening / closing fuel valve 5 is a general small electromagnetic valve, and is electrically connected to the control device 15. The electromagnetic opening / closing air valve 8 is electrically connected to the control device 15. The control device 15
The engine rotation angle signal (piston position signal) from the engine crank angle sensor 16 is input to the valve so that the opening / closing timings of the electromagnetic opening / closing fuel valve 5 and the electromagnetic opening / closing air valve 8 are controlled in synchronization with the piston position. It has become.

【0018】図1の1は燃料タンク、2は燃料供給ポン
プ、3は燃料レギュレータ、4は燃料供給管、6は空気
溜、7は空気レギュレータ、14が点火プラグ制御装
置、図1、図2の11がピストン、図2の8aは電磁開
閉空気弁8のコイル、8bは電磁開閉空気弁8の弁部、
8cは電磁開閉空気弁8のばねである。図3は、同燃焼
装置のクランク角タイムブロック線図である。
1, 1 is a fuel tank, 2 is a fuel supply pump, 3 is a fuel regulator, 4 is a fuel supply pipe, 6 is an air reservoir, 7 is an air regulator, 14 is a spark plug control device, and FIGS. 11 is a piston, 8a in FIG. 2 is a coil of the electromagnetic opening / closing air valve 8, 8b is a valve portion of the electromagnetic opening / closing air valve 8,
Reference numeral 8c is a spring of the electromagnetic opening / closing air valve 8. FIG. 3 is a crank angle time block diagram of the combustion device.

【0019】次に前記図1〜図3に示すガソリンエンジ
ンの燃焼装置の作用を具体的に説明する。制御装置15
により電磁開閉燃料弁5がエンジン回転角信号に同期し
て制御されるが、いま、ピストン11が膨張行程に入る
と、電磁開閉燃料弁5が開弁する。このとき、電磁開閉
空気弁8は、閉止している。また燃焼室12aに連通し
た混合気噴射弁9もシリンダ内圧力により押圧されて、
閉止している。電磁開閉燃料弁5は、給気行程から排気
ポートが閉止するまでの期間、必要燃料をメータリング
して、閉止される。
Next, the operation of the gasoline engine combustion apparatus shown in FIGS. 1 to 3 will be described in detail. Controller 15
The electromagnetic open / close fuel valve 5 is controlled in synchronization with the engine rotation angle signal. However, when the piston 11 enters the expansion stroke, the electromagnetic open / close fuel valve 5 opens. At this time, the electromagnetic opening / closing air valve 8 is closed. Further, the air-fuel mixture injection valve 9 communicating with the combustion chamber 12a is also pressed by the cylinder pressure,
It's closed. The electromagnetic opening / closing fuel valve 5 is closed by metering the required fuel during the period from the supply stroke to the closing of the exhaust port.

【0020】排気ポートが閉止されると、制御装置15
により電磁開閉空気弁8が開き、燃料溜室9aに空気が
導入され、空気溜室9a内の圧力が上昇して、比較的弱
いばね力により閉止されていた外開き式混合気噴射弁9
が燃焼室12a側に押し開かれ、混合気が空気により霧
化されて、燃焼室12aに噴出する。圧縮行程が終わり
に近づくと、シリンダ内の圧力が上昇して、燃料溜室9
aの空気圧よりも高くなると、外開き式混合気噴射弁9
が自動的に閉止して、噴射が終了する。燃焼室12a内
の混合気は、蒸発し、やがてTDC近傍で点火プラグ1
3により点火され、燃焼室12a全体に火炎が伝播し
て、膨張行程に入り、やがて燃焼が終了する。
When the exhaust port is closed, the controller 15
The electromagnetic open / close air valve 8 is opened by this, the air is introduced into the fuel storage chamber 9a, the pressure in the air storage chamber 9a rises, and the outer opening type air-fuel mixture injection valve 9 which has been closed by a comparatively weak spring force.
Is pushed open to the combustion chamber 12a side, and the air-fuel mixture is atomized by the air and ejected into the combustion chamber 12a. When the compression stroke approaches the end, the pressure in the cylinder rises and the fuel storage chamber 9
When it becomes higher than the air pressure of a, the outward-opening type mixture injection valve 9
Automatically closes and the injection ends. The air-fuel mixture in the combustion chamber 12a evaporates, and eventually the spark plug 1 near TDC.
3 is ignited, the flame propagates to the entire combustion chamber 12a, enters the expansion stroke, and eventually the combustion ends.

【0021】一方、膨張行程でのシリンダ内の圧力が噴
射空気圧以下になる前に電磁開閉空気弁8が閉止する。
この電磁開閉空気弁8が閉止後、電磁開閉燃料弁5が再
び開かれて、同様の制御サイクルが繰り返し行われる。
On the other hand, the electromagnetic opening / closing air valve 8 is closed before the pressure in the cylinder in the expansion stroke becomes lower than the injection air pressure.
After the electromagnetic opening / closing air valve 8 is closed, the electromagnetic opening / closing fuel valve 5 is opened again, and the same control cycle is repeated.

【0022】[0022]

【発明の効果】本発明のガソリンエンジンの燃焼装置は
前記のように燃料の噴射期間(メータリング期間)及び
空気の噴射期間を長くとることが可能であり、そのた
め、電磁開閉燃料弁及び電磁開閉空気弁の高応答性を大
幅に緩和できる。また混合気の噴射時期を排気ポート閉
止後にすることが可能であり、そのため、未燃ガスの吹
き抜けを大幅に減少できるとともに、燃料消費率を大幅
に低減できる。
As described above, the combustion apparatus for a gasoline engine according to the present invention can take a long fuel injection period (metering period) and air injection period. Therefore, an electromagnetic opening / closing fuel valve and an electromagnetic opening / closing valve are provided. The high responsiveness of the air valve can be greatly eased. Further, the injection timing of the air-fuel mixture can be set after the exhaust port is closed, so that the blow-through of unburned gas can be greatly reduced and the fuel consumption rate can be greatly reduced.

【0023】また電磁開閉燃料弁及び電磁開閉空気弁を
直接燃焼室に曝すことがないので、燃焼ガスによる電磁
開閉燃料弁及び電磁開閉空気弁の損傷を少なくできる。
Further, since the electromagnetic opening / closing fuel valve and the electromagnetic opening / closing air valve are not directly exposed to the combustion chamber, damage to the electromagnetic opening / closing fuel valve and the electromagnetic opening / closing air valve due to combustion gas can be reduced.

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

【図1】本発明のガソリンエンジンの燃焼装置の一実施
例を示す系統図である。
FIG. 1 is a system diagram showing an embodiment of a gasoline engine combustion apparatus of the present invention.

【図2】同燃焼装置の燃焼室及びその周辺部を示す縦断
側面図である。
FIG. 2 is a vertical cross-sectional side view showing a combustion chamber and its peripheral portion of the combustion apparatus.

【図3】同燃焼装置のクランク角タイムブロック線図で
ある。
FIG. 3 is a crank angle time block diagram of the combustion device.

【図4】従来の小型高速2サイクルガソリンエンジンの
シリンダ内噴射燃焼装置を示す系統図である。
FIG. 4 is a system diagram showing an in-cylinder injection combustion device of a conventional small-sized high-speed two-cycle gasoline engine.

【図5】同燃焼装置の燃焼室及びその周辺部を示す縦断
側面図である。
FIG. 5 is a vertical cross-sectional side view showing a combustion chamber and its peripheral portion of the combustion apparatus.

【図6】同燃焼装置のクランク角タイムブロック線図で
ある。
FIG. 6 is a crank angle time block diagram of the combustion device.

【符号の説明】[Explanation of symbols]

5 電磁開閉燃料弁 8 電磁開閉空気弁 9 混合気噴射弁 9a 燃料溜室 10 エンジン本体 11 ピストン 12a 燃焼室 13 点火プラグ 15 制御装置 5 Electromagnetic open / close fuel valve 8 Electromagnetic open / close air valve 9 Air-fuel mixture injection valve 9a Fuel storage chamber 10 Engine body 11 Piston 12a Combustion chamber 13 Spark plug 15 Control device

───────────────────────────────────────────────────── フロントページの続き (51)Int.Cl.6 識別記号 庁内整理番号 FI 技術表示箇所 F02M 69/10 ─────────────────────────────────────────────────── ─── Continuation of the front page (51) Int.Cl. 6 Identification code Office reference number FI technical display area F02M 69/10

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】 シリンダの燃焼室内に直接燃料を噴射
し、点火して、燃焼させるガソリンエンジンの燃焼装置
において、前記燃焼室の前部に燃料溜室を設け、同燃料
溜室と燃焼室との間に常時はばね力により閉止し且つ両
室の圧力差で開閉する外開き式混合気噴射弁を設けると
ともに、同燃料溜室内にそれぞれ制御装置によりエンジ
ン回転角信号を基準にサイクル毎に燃料及び空気の噴射
時期及び期間が制御される電磁開閉燃料弁及び電磁開閉
空気弁を設けたことを特徴とするガソリンエンジンの燃
焼装置。
1. In a combustion apparatus for a gasoline engine, in which fuel is directly injected into a combustion chamber of a cylinder, ignited and burned, a fuel storage chamber is provided in front of the combustion chamber, and the fuel storage chamber and the combustion chamber are connected to each other. An externally open air-fuel mixture injection valve that is normally closed by spring force and opened / closed by the pressure difference between the two chambers is installed between the fuel injection chamber and the fuel storage chamber by the control device based on the engine rotation angle signal. Also, a combustion device for a gasoline engine is provided with an electromagnetic opening / closing fuel valve and an electromagnetic opening / closing air valve for controlling the injection timing and period of air.
【請求項2】 前記制御装置により、前サイクルの燃焼
終了後より次サイクルの圧縮工程に入るまでの間に前記
燃料弁を開閉して前記燃料溜室内に必要量の燃料を噴射
するとともに、次サイクルの圧縮工程に入った後に前記
電磁開閉空気弁を開いて前記燃料溜室内に空気を噴射
し、同燃料溜室内の圧力上昇により前記混合気噴射弁を
自動的に開いて燃焼室内に混合気を噴射し、燃焼室内圧
縮圧力の上昇で前記混合気噴射弁を閉じ、混合気が着火
燃焼し、膨張行程で燃料室内圧力が空気噴射圧力よりも
低下する以前に前記電磁開閉空気弁を閉止するように制
御することを特徴とした請求項1記載のガソリンエンジ
ンの燃焼装置。
2. The control device opens and closes the fuel valve to inject a required amount of fuel into the fuel storage chamber between the end of combustion in the previous cycle and the start of the compression process in the next cycle. After entering the compression process of the cycle, the electromagnetic on-off air valve is opened to inject air into the fuel storage chamber, and the air-fuel mixture injection valve is automatically opened due to the pressure increase in the fuel storage chamber to open the air-fuel mixture in the combustion chamber. Is injected, and the mixture injection valve is closed by the increase of the compression pressure in the combustion chamber, the mixture is ignited and burned, and the electromagnetic opening / closing air valve is closed before the pressure in the fuel chamber falls below the air injection pressure in the expansion stroke. 2. The combustion apparatus for a gasoline engine according to claim 1, wherein the combustion apparatus is controlled as follows.
JP28116693A 1993-11-10 1993-11-10 Combustion equipment of gasoline engine Withdrawn JPH07133724A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP28116693A JPH07133724A (en) 1993-11-10 1993-11-10 Combustion equipment of gasoline engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP28116693A JPH07133724A (en) 1993-11-10 1993-11-10 Combustion equipment of gasoline engine

Publications (1)

Publication Number Publication Date
JPH07133724A true JPH07133724A (en) 1995-05-23

Family

ID=17635275

Family Applications (1)

Application Number Title Priority Date Filing Date
JP28116693A Withdrawn JPH07133724A (en) 1993-11-10 1993-11-10 Combustion equipment of gasoline engine

Country Status (1)

Country Link
JP (1) JPH07133724A (en)

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