JPS60500341A - How to run an engine with high heat of vaporization fuel - Google Patents
How to run an engine with high heat of vaporization fuelInfo
- Publication number
- JPS60500341A JPS60500341A JP58500687A JP50068783A JPS60500341A JP S60500341 A JPS60500341 A JP S60500341A JP 58500687 A JP58500687 A JP 58500687A JP 50068783 A JP50068783 A JP 50068783A JP S60500341 A JPS60500341 A JP S60500341A
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- fuel
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F3/00—Pistons
- F02F3/26—Pistons having combustion chamber in piston head
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- 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
- F02B1/00—Engines characterised by fuel-air mixture compression
- F02B1/02—Engines characterised by fuel-air mixture compression with positive ignition
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- 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
- F02B17/00—Engines characterised by means for effecting stratification of charge in cylinders
- F02B17/005—Engines characterised by means for effecting stratification of charge in cylinders having direct injection in the combustion chamber
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/08—Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition
- F02B23/10—Other 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
- F02B23/101—Other 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
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/08—Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition
- F02B23/10—Other 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
- F02B2023/108—Swirl flow, i.e. the axis of rotation of the main charge flow motion is vertical
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- 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
- F02B75/12—Other methods of operation
- F02B2075/125—Direct injection in the combustion chamber for spark ignition engines, i.e. not in pre-combustion chamber
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B2275/00—Other engines, components or details, not provided for in other groups of this subclass
- F02B2275/40—Squish effect
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Abstract
(57)【要約】本公報は電子出願前の出願データであるため要約のデータは記録されません。 (57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
【発明の詳細な説明】 高蒸発熱燃料で機関を運転する方法 本発明は、メタノール等σ)ごとき高い蒸発11”)潜熱も一有する燃料で火花 点火型内燃機関を述転才ろ方法に係る。より明細に言えば、そ才上は燃料プ)1 その主部分を蒸発さぜそして微粒化するため第1(1)段階において導入され、 そしてそのあとで、急速な点火f力ため点火プラグのイ\j近に濃厚な空気/黙 月混合物へ、提供3−ろため第2の段階において導入される機関運転方法に係る 。[Detailed description of the invention] How to run an engine with high heat of vaporization fuel The present invention uses a fuel that also has a high latent heat of vaporization, such as methanol (σ), to generate sparks. This article relates to a method for converting an ignition-type internal combustion engine. To be more specific, the fuel level is 1) introduced in the first (1) stage to evaporate and atomize its main portion; After that, due to the rapid ignition power, dense air/silence is created near the spark plug. Regarding the engine operating method introduced in the second stage of provision 3-filtration, .
高い蒸発の潜熱を有する燃料がfit 1!車車内内燃関において用いるたぬに 提案されている。メタノールは往復f′ストン機関燃訓σ)/、−y)l17) 第1σ)候補て・ある。なぜた、らばぞれは高メクタン価を有し、イーして石炭 から容易に生産され得るからである。しかし、メタノールに関連する欠点ば、そ J)高い蒸発J)潜熱と、その低い熱エネルギ熱ぼ量と、潤滑油を希釈1−そオ ′1.□によってピストンリング及びンリン〃ゞ孔θ)摩耗を増加させるその傾 向である。Fuel with high latent heat of vaporization fits 1! Tanuni used in the internal combustion engine of a car Proposed. Methanol is a reciprocating f' stone engine combustion model σ)/, -y)l17) There are candidates for 1st σ). Why, Rabazo has a high mectane value, and it is similar to coal. This is because it can be easily produced from. However, the disadvantages associated with methanol are that J) high evaporation J) latent heat and its low thermal energy calorific value dilutes lubricating oil '1. □ due to piston ring and ring hole θ) its tendency to increase wear. It is towards.
メタノールは様々の方法で・機関内に導入きれ得る。Methanol can be introduced into the engine in a variety of ways.
気化メタノール導入の場合、高い蒸発の潜熱は吸込空気が吸込装置を通ってシυ ンダへ流れるにしたがって燃料な吸込空気中・に均等に分配させることを困テ1 (にづ込装置に大量の加熱を行なうことである。しかし、液体メタノールの小滴 が依然としてシリンダに進入し、そこにおいてそれらはシリンダ壁に付着し、杉 の結果として潤滑油を希釈し、それによってシリンダ壁及びピストン・リングと の摩耗が早められることになる。In the case of vaporized methanol introduction, the high latent heat of vaporization is caused by the suction air passing through the suction device. It is difficult to evenly distribute the fuel into the intake air as it flows to the tank. (This involves applying a large amount of heat to the nudging device. However, a small drop of liquid methanol still enter the cylinder, where they stick to the cylinder wall and cedar dilutes the lubricating oil as a result of wear will be accelerated.
多点噴射に依る吸込マニホルドへのメタノールの噴射は、燃料導入のためのもう 一つの可能的方法である。Injection of methanol into the suction manifold using multi-point injection is an alternative method for fuel introduction. This is one possible method.
この方法はシリンダ対シリンダ燃料分配問題を無くするが、シリンダ壁における 油希釈の蓋然性を除去しない。実際において、蒸発に使用され得る時間の減少の 故に、そして排気熱がメタノールへ伝熱されないから、それは気化メタノール導 入に相対して油希釈問題をおそらく増加するであろう。This method eliminates the cylinder-to-cylinder fuel distribution problem, but Does not eliminate the possibility of oil dilution. In practice, the reduction in time available for evaporation Therefore, and since the exhaust heat is not transferred to methanol, it is the vaporized methanol conductor. would likely increase oil dilution problems relative to
本発明は機関燃焼室へのメタノールの2段階導入を提供することによって上記の 諸欠点を克服する機関運転方法に係る。この場合、燃焼室の一部分はピストンの 正面に中心凹所を有し、該凹所内に燃料の主部分が噴射されて蒸発と微粒化との ために閉じ込められ、それによって、シリンダ壁の濡れを最小限度にする。The present invention accomplishes the above by providing a two-stage introduction of methanol into the engine combustion chamber. It concerns an engine operating method that overcomes various drawbacks. In this case, a part of the combustion chamber is connected to the piston. It has a central recess in the front, and the main part of the fuel is injected into the recess to prevent evaporation and atomization. to minimize wetting of the cylinder wall.
従って、本発明の目的は、放出物の生成量を減じると同時に吸込チャージ並びに 機関の関連部分を冷却することによって機関の体積効率を向上させるために高い 蒸発の潜熱を有する燃料で機関を運転することである。It is therefore an object of the present invention to reduce the amount of emissions produced while at the same time reducing the suction charge and High to improve the volumetric efficiency of the engine by cooling the relevant parts of the engine It is the operation of an engine with fuel that has latent heat of vaporization.
本発明のもち一つの目的は、燃料が複数の段階で噴射されて最初に最小限度の壁 温れて燃料の主部分を適正に蒸発させそして微粒化し、そのちと第2に点火時点 に点火プラグの付近に濃厚な空気/燃料混合物を提供し以て一貫した忠実な火炎 の開始を保証する上述した如き機関を運転することである。One object of the present invention is that the fuel is injected in multiple stages so that the fuel is initially Once heated, the main part of the fuel is properly evaporated and atomized, and then secondly at the point of ignition. Provides a rich air/fuel mixture near the spark plug for a consistent and faithful flame is to operate the engine as described above to ensure the start of the engine.
自動車型の車輌における高い蒸発の潜熱を有するメタノールまたはその他の燃料 の使用は既知である。例えば、オズワルドほかの米国特許第4126997号及 び米国特許第4216744号は、第2図においてピストン内はち形くぼみ型燃 焼室と、機関に対し約12:1の圧縮比と、燃焼室の中心または軸線に実質的に 接近して位置される点火プラグとを有する機関における100%のメタノールの 使用を開示している。Methanol or other fuels with high latent heat of vaporization in automotive type vehicles The use of is known. For example, U.S. Pat. No. 4,126,997 to Oswald et al. and U.S. Pat. combustion chamber and a compression ratio of approximately 12:1 to the engine, substantially at the center or axis of the combustion chamber. of 100% methanol in engines with closely located spark plugs. Use is disclosed.
しかし、燃料の全てが同時に噴射され、そしてどのようにしてシリンダ壁の濡れ 及びその結果として生じる潤滑油の希釈が防がれるか説明されていない。But all of the fuel is injected at the same time, and how do we get the cylinder walls wet? and how the resulting dilution of the lubricating oil is prevented is not explained.
ジョンの米国特許第1117810号は機関に使用するためのガソリンとメタノ ールとを混合する装置を説明しており、そして燃焼室または前述した諸問題を回 避する態様で機関を運転する方法に就ては説明力1為されていない。John's US Pat. No. 1,117,810 is a gasoline and methane It describes a device for mixing the combustion chamber or the aforementioned problems. No explanatory power has been given as to how to operate the engine in a manner that avoids this.
エカートほかの米国特許第4022165号は、二つの別々の燃料量がそれらの 間に時間遅れを置いて機関内に噴射番される燃料噴射装置を説明している。機関 の1作動ナイクル間に2個の別個の燃料噴射ノズルが使用されて同じン1)ンゲ 内VC@初に燃料の大きな量が噴射きれ、そのあとで、より小さい量が噴射され る。U.S. Pat. No. 4,022,165 to Eckert et al. discloses that two separate amounts of fuel are This describes a fuel injection system that injects fuel into the engine with a time delay in between. institution Two separate fuel injection nozzles are used between the two operating units of the same unit (1) operating unit. Inner VC @ A large amount of fuel is injected at first, and then a smaller amount is injected. Ru.
燃料の大きい脅はまっすぐなジェットとしてシリンダ内だ深く噴射され、一方、 より小さい量は点火フ0ラグのイ」近に導入される。しかし、燃・焼室の作用に 就ては説明が為されておらず、また壁濡れ及び油希釈を防ぐたぬの空気、/燃料 チャージの調時及び運動に就でいかなる方法も開示されていない。A large amount of fuel is injected deep into the cylinder as a straight jet, while A smaller amount is introduced closer to the ignition flag. However, due to the action of the combustion chamber No explanation has been given regarding this, and the air/fuel No method of timing and movement of the charge is disclosed.
アラヤほかの米国特許第672!2,490号も2段階燃料噴射装置、を開示し ているが、該装置においては噴射は最初に吸込行程または膨張行程の終りに近い 一点において生じ、そして次いで圧縮行程の初めの一点で生じる。これは本発明 とは異なり、前述した欠点を克服するには不満足である。U.S. Pat. No. 672!2,490 to Araya et al. also discloses a two-stage fuel injection system. However, in this device, injection is first performed near the end of the suction or expansion stroke. It occurs at one point and then at one point at the beginning of the compression stroke. This is the invention However, it is unsatisfactory in overcoming the drawbacks mentioned above.
エイずトの米国特許第3216407号及び第3439655号は、何れも、内 燃機関内への燃料の複式噴射を提供−rる機械的構造を示している。しかし、機 関を運転する方法は、開示される本発明のそれとは異なる。U.S. Patent Nos. 3,216,407 and 3,439,655 to E.I.T. 1 shows a mechanical structure that provides multiple injections of fuel into a combustion engine; However, the machine The method of operating the valve is different from that of the disclosed invention.
最後に、フリッカほかの米国特許第66.41986号は接線人D W分を有す るピストン内はち形態焼室のみを示している。Finally, U.S. Patent No. 66.41986 to Fricker et al. Only the bee-shaped baking chamber inside the piston is shown.
本発明のその他の目的、特長及び利点は、次ぎのその詳細な説明と、本発明の運 転方式を利用する機関の構造を概略的に図示する1枚の図面とを参照することに よってより明らかになるであろう。Other objects, features and advantages of the invention will be found in the following detailed description and operation of the invention. With reference to a drawing schematically illustrating the structure of an engine utilizing the transfer system. Therefore, it will become clearer.
上述のごとく、高い蒸発の潜熱を有するメタノールまたはその他の燃料を使用す ることの従来の欠点は、ピストン内はち形くぼみ型の凹所を有する燃焼室と協働 して燃料の複式噴射を利用する直接燃料噴射概念の適用によって克服され得る。As mentioned above, using methanol or other fuels with high latent heat of vaporization The traditional drawback of this is that the piston has a bee-shaped recess that cooperates with the combustion chamber. can be overcome by applying a direct fuel injection concept that utilizes multiple injections of fuel.
そのような構造は図面に概略的に図示されており、読図は火花点火型の内燃機関 の一部分10を示している。それは通常のシリンダ・ブロック12を有し、該ブ ロック内に2ストン14がシリンダ・ヘッド18の面16と協働してそれらの間 に燃焼室20を画成するように摺動自在に据付けられている。この場合、ピスト ン14はピストン内わん形くぼみ型の構造を画成する中心凹所2,2を有する。Such a structure is schematically illustrated in the drawing, and the reading is similar to that of a spark-ignition internal combustion engine. 10 is shown. It has a normal cylinder block 12, which Within the lock a two-stone 14 cooperates with the face 16 of the cylinder head 18 to create a space between them. It is slidably installed so as to define a combustion chamber 20 in the combustion chamber 20 . In this case, the piste The piston 14 has a central recess 2,2 defining a bowl-shaped structure within the piston.
凹所22はぴしゃぴしゃ区域の約40〜75%を提供するように設計され、そし て機関そのものはメタノール燃料を最も有効に用いろように約16:1の圧縮比 で作動する。The recess 22 is designed to provide approximately 40-75% of the snapping area and The engine itself has a compression ratio of approximately 16:1 to use methanol fuel most effectively. It operates with.
シリンダヘッド18は普通の吸気弁24と排気弁26とを有する。弁24は適度 の旋回率を得るように設計される吸込通路28を通じて空気を供給される。排気 ガスは出口通路30を通じて吐出される。該通路は熱保存をより良好ならしめる ためにセラミックまたは薄板金で内張すされ得る。Cylinder head 18 has conventional intake valves 24 and exhaust valves 26. Valve 24 is moderate Air is supplied through a suction passage 28 designed to obtain a rotation rate of . exhaust Gas is discharged through outlet passage 30. The passage provides better heat preservation It can be lined with ceramic or sheet metal.
32を以て概略的に示される燃料噴射器は本質的に凹所22上の燃焼室20の中 心にそのノズル34を突入させるよう゛にン)】ンぶゞ・ヘッド18の中心に位 置されている。該噴射器は既知の型式であり、したがって、その構造及び作用の 細部は説明されない。この場合においては、ノズル34VC供給するポンフ0装 置は中庸の圧力レベル(噴射器のため約18.ろkg/ cm” C260ps i ’) )で作動12、そしてノズルそれ自体は、後述される目的のために合 理的に良好な微粒化特性と比較的低い貫通特性を有する円錐形燃料スプレーを提 供すると言えば充分である。A fuel injector, indicated schematically at 32, is located essentially within the combustion chamber 20 above the recess 22. Place the nozzle 34 in the center of the engine head 18. It is placed. The injector is of known type and therefore of its construction and operation. Details are not explained. In this case, no pump is supplied with 34 VC of nozzle. The pressure level is moderate (approximately 18 kg/cm" C260 ps due to the injector) i'))) and the nozzle itself is fitted for the purpose described below. The present invention presents a conical fuel spray with good atomization properties and relatively low penetration properties. Suffice it to say, I will provide it.
哉火フ0ラグ36は図示のごとく燃料噴射ノズル34の先端に隣接してその電極 を突出させるように燃焼室の中心にできるだけ接近して位置される。The fire flag 36 is located adjacent to the tip of the fuel injection nozzle 34 as shown in the figure. located as close as possible to the center of the combustion chamber so as to protrude.
ピストン14は、機関が上死点位置ののち概ね65゜のクランク角に亘って回転 したときの位置で示されている。また、破線によって示されるごとく、噴射ノズ ル34からの燃料のだめの概ね80°の円錐噴射角が示されている。もし燃料が ピストン14が上死点位置の近くに位置するとき噴射されるならば、噴射される 燃料の事実上全てが直接的に凹所22内に進み、従ってシリンダ壁を濡らさない ことは明らかであろう。もし単に少量の燃料が噴射されるに過ぎないならば、そ れ隣接して閉じ込められて、点火のためこの区域に濃厚な空気燃料混合物を提供 する。The piston 14 rotates through a crank angle of approximately 65 degrees after the engine is at the top dead center position. It is shown in the position when Also, as shown by the dashed line, the injection nozzle A conical injection angle of approximately 80° of the fuel reservoir from the fuel tank 34 is shown. If the fuel If it is injected when the piston 14 is located near the top dead center position, it is injected. Virtually all of the fuel goes directly into the recess 22 and therefore does not wet the cylinder walls. That should be obvious. If only a small amount of fuel is injected, then is confined adjacent to provide a rich air-fuel mixture to this area for ignition. do.
本発明の主特徴は、初めに燃料の大きなチャージな点火の充分前にそれが蒸発さ えしそして微粒化され得るよ5に提供し、そして空気/燃料チャージの信頼でき る点火を提供する時点及“び場所において第2のチャージを提供する独得の燃料 噴射調時である。The main feature of the invention is that the large charge of fuel is vaporized well before ignition. 5 and can be atomized and provide a reliable air/fuel charge. Proprietary fuel that provides a second charge at the point and location that provides the ignition It is time to adjust the injection.
より明細に述べると、機関は次ぎのごとき燃焼方法で作動する。機関がその吸気 行程を開始するに従って、吸気弁24の開放は中庸の旋回運動を以て空気またし 1ガスを前記燃焼室20内へ導入する。ピストン14がその上死点位置からその 下降を開始するにしたがって、燃料の第1の大きなチャージ(全体の概ね75〜 90%)が、ノズル34から燃焼室20内へ噴射される。More specifically, the engine operates with the following combustion method. The engine takes its intake As the stroke begins, the opening of the intake valve 24 allows air to flow through the air with a moderate swirling motion. 1 gas is introduced into the combustion chamber 20. The piston 14 moves from its top dead center position to its As we begin our descent, the first large charge of fuel (approximately 75~ 90%) is injected into the combustion chamber 20 from the nozzle 34.
既に説明された如く、ピストン14は吸気行程の開始時においてその上死点の近 くに位7置しているから燃料のこの全チャージはピストン14の凹所22へ導か れる。装入する旋回空気は凹所22内に進入して燃料を蒸発させそしてそれを微 粒化する。燃料は概ねピストン14が図面に示される位置に達する時点までに完 了されるように短かい持続時間急速度で噴射される。As already explained, the piston 14 is near its top dead center at the beginning of the intake stroke. Since the piston is located at the 7th position, this entire charge of fuel is directed into the recess 22 of the piston 14. It will be done. The swirling air charge enters the recess 22 to vaporize the fuel and atomize it. Granulate. The fuel is generally complete by the time piston 14 reaches the position shown in the drawings. It is injected at a rapid rate for a short duration so that it can be detected.
即ち、燃料の壷初の部分の噴射は、吸込行程の開始時における上死点位置ののち 約500〜60°の間に終わらせられる。その結果として、吸込行程の残りの間 、ピストン14が下降し、そしてさらに旋回空気が開放吸気弁24を通じてシリ ンダに進入するに従って、蒸発させられ且つ微粒化された燃料霧は凹所22から 外方へシリンダ空間20の残部へ散乱する。かくのごとき構成は、大きな燃料小 滴がシリンダ壁に接触する可能性なおそらく無くさせる。なぜならば、それらは 燃焼凹所22の内側の室壁まで外方へ遠心作用を受けさせられ、そこにおいてそ れらは蒸発するに従って該室壁から熱を吸収するからである。また、この吸込行 程間における空気中に浮かぶ燃料の蒸発は吸込チャージを冷却し、従って機関の 体積効率を改善する。より低温の吸込温度は、また、より低温の総合ナイクル温 度を生じる結果になり、それによって熱効率が改善され、そして燃焼間に生成さ れる窒素酸化物(1旬X)が減じられる。That is, the injection of the first part of the pot of fuel occurs after the top dead center position at the beginning of the suction stroke. It ends between about 500 and 60 degrees. As a result, during the remainder of the suction stroke , the piston 14 descends, and further swirling air enters the series through the open intake valve 24. As it enters the tank, the evaporated and atomized fuel mist exits from the recess 22. Scattered outwardly into the remainder of the cylinder space 20. Such a configuration requires a large amount of fuel Possibly eliminating the possibility of the droplet contacting the cylinder wall. because they are The inner chamber wall of the combustion recess 22 is subjected to an outward centrifugal action, where the This is because as they evaporate, they absorb heat from the chamber walls. Also, this suction line Evaporation of fuel floating in the air during engine cooling cools the suction charge, thus cooling the engine. Improve volumetric efficiency. A cooler suction temperature also results in a cooler overall Nycl temperature. resulting in higher temperatures, thereby improving thermal efficiency and producing less heat during combustion. Nitrogen oxides (1X) are reduced.
装入する空気及び排気ガスによる燃料の蒸発及び露化は、全吸込行程を通じて続 く。そのあと、圧縮行程の後期部分間、ピストンの上死点前の概ね3 D’〜5 0’の位置において、全燃料チャージの第2のより小さい(10〜25 s ) 部分がノズル34を通じて噴射される。そのような小さい燃料の量の貫通度は低 い;従ってこの燃料のほとんどは噴射器ノズル34の先端の付近にとどまって点 火直前の点火プラグ36の付近における空気/・燃料比を濃厚化する。これは− 貫した忠実な火炎創始を保証し、そしてNOx制御と組合わされた高効率のため 、大量の排気ガス再循環(E()R)に依る部分負荷における希薄運転を容易な らしめる。次いで、点火プラグによって燃焼が開始される。Evaporation and exposure of the fuel by the air charge and exhaust gases continues throughout the entire intake stroke. Ku. After that, during the latter part of the compression stroke, approximately 3 D' to 5 before the top dead center of the piston. At 0' position, the second smaller (10-25 s) of total fuel charge A portion is injected through nozzle 34. Penetration for such small fuel quantities is low. Therefore, most of this fuel remains near the tip of the injector nozzle 34 and does not point. The air/fuel ratio near the spark plug 36 just before the fire is enriched. This is- Guarantees consistent and faithful flame initiation and for high efficiency combined with NOx control , facilitates lean operation at part load with extensive exhaust gas recirculation (E()R). make it look like Combustion is then initiated by the spark plug.
もし全てのメタノールが圧縮行程の後期において噴射されるならば、蒸発し二必 要とされる熱は圧縮されたガスの熱から主として抽出さ牙1、る:従って、1犬 な熱力学的効率損失が生じ得る。メタノールの蒸発の潜熱はその発熱量の約5% である;従って、この熱の圧縮ガスからの抽出は燃料の発熱量の5%の損失に等 しい。If all the methanol is injected late in the compression stroke, it will evaporate and The required heat is extracted primarily from the heat of the compressed gas: therefore, the heat required is extracted from the heat of the compressed gas. Significant thermodynamic efficiency losses can occur. The latent heat of vaporization of methanol is about 5% of its calorific value. therefore, the extraction of this heat from the compressed gas is equivalent to a loss of 5% of the heating value of the fuel. Yes.
吸込行程の全体に亘っての、反び/または圧縮行程σノ初期部分間における[貞 接ンリンぶ゛噴射は、ごの損失を防止するが、そ−れはシリンダ壁の濡れ及びそ の関連ピストン・リング並びにシリンダ孔の摩耗という欠点を督する。本発明は 良好な体積効率を提供する態様で燃料を微粒化しそして蒸発させるピストン内ば ち形くぼみ型・燃焼室内への2段階燃料噴射?乙よって上記問題を除去する。こ れと同時に、蒸発に必要な熱は包囲するシリンダ壁及びピストン表面から取られ 、これ(・てよってそれらを冷却し、さらに空気またガスの装入するチャージか らも熱が取出され、これによってまた体積効率及び熱効率を向上させる。warpage throughout the suction stroke and/or during the initial part of the compression stroke σ. Contact jetting prevents loss of gas, but it reduces wetting of the cylinder wall and its The associated piston rings and cylinder bores suffer from wear. The present invention A chamber within the piston that atomizes and vaporizes the fuel in a manner that provides good volumetric efficiency. Two-stage fuel injection into the combustion chamber? Party B will eliminate the above problem. child At the same time, the heat required for evaporation is taken from the surrounding cylinder wall and piston surface. , this is a charge that cools them down and then charges them with air or gas. Heat is also extracted from them, which also improves volumetric and thermal efficiency.
以上述べたことから、本発明は・燃料がシリンダ表面を濡らさないように高い蒸 発の潜熱を有する燃料を用いる自動車型内燃機関を運転する方法を提供すること と、蒸発のために必要とされる熱は吸込まれた空気及びピストン表面から取られ ることが理解されるであろう。吸込まれた空気の冷却は体積効率及び熱効率を改 善し且つNOxの生成を減じる。ピストンの冷却はその耐久性を向上させ、そし て過度且つ高価なピストン冷却手段に頼ることなしに機関の過給を容易ならしぬ る。In light of the above, the present invention is aimed at: To provide a method for operating an automobile-type internal combustion engine using a fuel having latent heat of , the heat required for evaporation is taken from the inhaled air and the piston surface. It will be understood that Cooling of the inhaled air improves volumetric and thermal efficiency. and reduce NOx production. Cooling the piston increases its durability and to facilitate engine supercharging without resorting to excessive and expensive piston cooling means. Ru.
さらにまた、本発明によって提供されるごとき直接にシリンダ内での燃料の良好 な機械的微粒化は、吸気熱を供給する必要を無くし、、Lかもなおそれは良好な 燃料分配を保証する。説明された特殊の調時方法に依る燃料の主部分の直接燃料 噴射はメタノールがシリンダ壁面の油膜を希釈する公算を最小にする。また、点 火直前におけるより小さい量の燃料の第2段噴射は、希薄混合気と高EGR率と を以て、点火性を危うくすることなしに機関の運転を容易ならしめる。Furthermore, the ability of fuel to flow directly into the cylinder as provided by the present invention is further improved. Mechanical atomization eliminates the need to supply suction heat, and it is also possible to Ensure fuel distribution. Direct fueling of the main part of the fuel according to the special timing method described Injection minimizes the likelihood that methanol will dilute the oil film on the cylinder wall. Also, the point The second stage injection of a smaller amount of fuel just before the fire results in a lean mixture and high EGR rate. This makes engine operation easier without jeopardizing ignitability.
本発明はその一推奨実施例において示され、そして説明されたが、多くの変更及 び修正が本発明の範囲から逸脱することなしにそれに対して為され得ることは、 本発明が関係する技術に熟練している人々には明らかであろう。Although the invention has been shown and described in one preferred embodiment thereof, there are many modifications and variations. and that modifications may be made thereto without departing from the scope of the invention. It will be obvious to those skilled in the art to which this invention pertains.
■(ト)際論査報告■(g) International research report
Claims (1)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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PCT/US1983/000029 WO1984002744A1 (en) | 1983-01-10 | 1983-01-10 | Method of operating an engine with a high heat of vaporization fuel |
Publications (1)
Publication Number | Publication Date |
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JPS60500341A true JPS60500341A (en) | 1985-03-14 |
Family
ID=22174801
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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JP58500687A Pending JPS60500341A (en) | 1983-01-10 | 1983-01-10 | How to run an engine with high heat of vaporization fuel |
Country Status (2)
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JP (1) | JPS60500341A (en) |
WO (1) | WO1984002744A1 (en) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS62129514A (en) * | 1985-11-30 | 1987-06-11 | Isuzu Motors Ltd | Combustion chamber for internal combustion engine |
US4955339A (en) * | 1988-11-18 | 1990-09-11 | Toyota Jidosha Kabushiki Kaisha | Internal combustion engine |
US5271362A (en) * | 1990-06-27 | 1993-12-21 | Toyota Jidosha Kabushiki Kaisha | Two-stroke engine |
JPH04228850A (en) * | 1990-12-27 | 1992-08-18 | Toyota Motor Corp | In-cylinder injection type internal combustion engine |
GB2280931A (en) * | 1993-08-13 | 1995-02-15 | Edwin Seymour Marsden | Four-stroke engine. |
DE19637993C1 (en) * | 1996-09-18 | 1998-02-26 | Daimler Benz Ag | Direct injection internal combustion engine |
DE69711933T2 (en) | 1997-02-01 | 2002-08-22 | Ford Global Technologies, Inc. | DIRECTLY INJECTED SPARK IGNITION ENGINE |
GB9702109D0 (en) * | 1997-02-01 | 1997-03-26 | Ford Motor Co | Direct injection spark ignition engine |
WO2021011528A1 (en) | 2019-07-15 | 2021-01-21 | The Research Foundation For The State University Of New York | Method for control of advanced combustion through split direct injection of high heat of vaporization fuel or water fuel mixtures |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
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DE1808650A1 (en) * | 1968-11-13 | 1970-06-18 | Bosch Gmbh Robert | Fuel injector |
US3908624A (en) * | 1970-03-23 | 1975-09-30 | Mitsubishi Heavy Ind Ltd | Internal combustion engine |
US3999532A (en) * | 1973-11-23 | 1976-12-28 | Kornhauser Daniel W | Internal combustion engine fuel system |
FR2343893A1 (en) * | 1976-03-08 | 1977-10-07 | Oswald Roger | FUEL ENGINE OTHER THAN A PETROLEUM PRODUCT |
-
1983
- 1983-01-10 JP JP58500687A patent/JPS60500341A/en active Pending
- 1983-01-10 WO PCT/US1983/000029 patent/WO1984002744A1/en unknown
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