JPH11324805A - Precombustion chamber type gas engine - Google Patents
Precombustion chamber type gas engineInfo
- Publication number
- JPH11324805A JPH11324805A JP10132371A JP13237198A JPH11324805A JP H11324805 A JPH11324805 A JP H11324805A JP 10132371 A JP10132371 A JP 10132371A JP 13237198 A JP13237198 A JP 13237198A JP H11324805 A JPH11324805 A JP H11324805A
- Authority
- JP
- Japan
- Prior art keywords
- combustion chamber
- ignition
- pilot
- fuel injection
- gas engine
- 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.)
- Granted
Links
- 238000002485 combustion reaction Methods 0.000 claims abstract description 133
- 239000000446 fuel Substances 0.000 claims abstract description 73
- 238000002347 injection Methods 0.000 claims abstract description 49
- 239000007924 injection Substances 0.000 claims abstract description 49
- 239000000203 mixture Substances 0.000 claims abstract description 24
- 239000000243 solution Substances 0.000 abstract 1
- 239000007789 gas Substances 0.000 description 33
- 239000003921 oil Substances 0.000 description 7
- 239000002737 fuel gas Substances 0.000 description 5
- 238000004891 communication Methods 0.000 description 4
- 230000006835 compression Effects 0.000 description 3
- 238000007906 compression Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 230000020169 heat generation Effects 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 230000009977 dual effect Effects 0.000 description 2
- 239000000428 dust Substances 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000002474 experimental method Methods 0.000 description 2
- 239000000295 fuel oil Substances 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 238000013461 design Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 238000011056 performance test Methods 0.000 description 1
- 238000010248 power generation Methods 0.000 description 1
- 239000000779 smoke Substances 0.000 description 1
Classifications
-
- 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
-
- 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
- Y02T10/30—Use of alternative fuels, e.g. biofuels
Landscapes
- Output Control And Ontrol Of Special Type Engine (AREA)
- Ignition Installations For Internal Combustion Engines (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
- Fuel-Injection Apparatus (AREA)
Abstract
Description
【0001】[0001]
【発明の属する技術分野】本発明は、主として定置型発
電設備の駆動源として有用な予燃焼室方式ガスエンジン
に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a pre-combustion chamber type gas engine which is useful mainly as a drive source for stationary power generation equipment.
【0002】[0002]
【従来の技術】近年、低公害の要請から希薄燃焼ガスエ
ンジンが注目されている。従来の希薄燃焼ガスエンジン
は、点火プラグを着火源とする予燃焼室方式が主流であ
った。また、これとは別に、パイロット噴射ガスエンジ
ン(デュアルフュエルエンジン)というエンジンも知ら
れている。このエンジンは、全熱量比の5〜15%程度
のパイロツト油(液体)を直接主燃焼室に噴射させ、こ
れを着火源としてガス燃料を燃焼させる構造のエンジン
である。これは一般的なディーゼルエンジンの主燃料噴
射弁から少量のパイロット燃料を噴射させることで実現
している。2. Description of the Related Art In recent years, lean-burn gas engines have attracted attention due to the demand for low pollution. Conventional lean burn gas engines mainly use a pre-combustion chamber system using a spark plug as an ignition source. Apart from this, an engine called a pilot injection gas engine (dual fuel engine) is also known. This engine has a structure in which pilot oil (liquid) having a ratio of about 5 to 15% of the total calorific value is directly injected into the main combustion chamber, and the fuel is burned using the fuel as an ignition source. This is achieved by injecting a small amount of pilot fuel from the main fuel injection valve of a typical diesel engine.
【0003】[0003]
【発明が解決しようとする課題】ところで、従来の点火
プラグ付予燃焼室方式ガスエンジンは、希薄混合気の燃
焼であるが故に、強力な点火エネルギを付与させない
と、失火を伴う燃焼変動を生ずることがある。また、同
一シリンダ径のディーゼルエンジンに比較すると、NO
xは約1/10と低く、環境に対して有利であるが、エ
ンジン熱効率が低い欠点がある。The conventional gas engine with a pre-combustion chamber equipped with a spark plug is a combustion of a lean air-fuel mixture. Therefore, unless a strong ignition energy is applied, a combustion fluctuation accompanied by a misfire occurs. Sometimes. Also, when compared to diesel engines with the same cylinder diameter, NO
x is as low as about 1/10, which is advantageous for the environment, but has the disadvantage of low engine thermal efficiency.
【0004】燃焼変動の改善に関しては、予燃焼室内の
燃焼を確実にするために予燃焼室内での点火プラグ位置
の最適化や予燃焼室内の混含気の均一化についての研究
が種々行われている。しかし、点火エネルギの増大に寄
与するものではないため、エンジン熱効率や燃焼変動の
改善を図るにも限界があった。Regarding the improvement of combustion fluctuations, various studies have been made on optimization of the position of a spark plug in the pre-combustion chamber and uniformization of mixed gas in the pre-combustion chamber in order to ensure combustion in the pre-combustion chamber. ing. However, since it does not contribute to an increase in ignition energy, there is a limit in improving engine thermal efficiency and combustion fluctuation.
【0005】また、従来のパイロット噴射ガスエンジン
は、NOxと煤塵を低減することには限界があり、ガス
エンジンの利点である排ガス低公害性を生かしきれてい
ない欠点があった。[0005] Further, the conventional pilot injection gas engine has a limit in reducing NOx and dust, and has a drawback in that it cannot make full use of the low pollution of exhaust gas, which is an advantage of the gas engine.
【0006】本発明は、上記事情を考慮し、低NOxを
維持しながら、より高いエンジン熱効率を得ることがで
き、それによりガスエンジンの低公害性(低CO2)を
生かすことのできる予燃焼室方式ガスエンジンを提供す
ることを目的とする。SUMMARY OF THE INVENTION In view of the above circumstances, the present invention provides a pre-combustion chamber capable of obtaining higher engine thermal efficiency while maintaining low NOx, thereby making use of the low pollution (low CO2) of a gas engine. It is an object of the present invention to provide a gas engine.
【0007】[0007]
【課題を解決するための手段】請求項1の発明は、ピス
トンとシリンダとシリンダヘッドにより画定される主燃
焼室に気体燃料を供給して燃焼させることにより駆動出
力を得るガスエンジンであって、シリンダヘッドに、主
燃焼室内の混合気の着火源となる点火プラグ付予燃焼室
とパイロット燃料噴射弁付予燃焼室とを設けたことを特
徴とする。A first aspect of the present invention is a gas engine which obtains a driving output by supplying gaseous fuel to a main combustion chamber defined by a piston, a cylinder, and a cylinder head and burning the gaseous fuel. The cylinder head is provided with a pre-combustion chamber with a spark plug and a pre-combustion chamber with a pilot fuel injection valve, which are ignition sources of the air-fuel mixture in the main combustion chamber.
【0008】請求項2の発明は、請求項1において、同
一燃焼サイクルにおいて前記点火プラグ付予燃焼室とパ
イロット燃料噴射弁付予燃焼室とをほぼ同時に、または
若干ずらして機能させて、これらを着火源として主燃焼
室の混合気を燃焼させることを特徴とする。According to a second aspect of the present invention, in the first aspect, the pre-combustion chamber with the ignition plug and the pre-combustion chamber with the pilot fuel injection valve are made to function substantially simultaneously or slightly shifted in the same combustion cycle, and these are operated. The mixture of the main combustion chamber is burned as an ignition source.
【0009】請求項3の発明は、請求項1または2にお
いて、前記パイロット燃料噴射弁につながる燃料噴射ポ
ンプを、クランクケースのカム室のドアに取り付けたこ
とを特徴とする。According to a third aspect of the present invention, in the first or second aspect, a fuel injection pump connected to the pilot fuel injection valve is attached to a door of a cam chamber of a crankcase.
【0010】[0010]
【発明の実施の形態】以下、本発明の実施形態を図面に
基づいて説明する。図1は実施形態のガスエンジンのシ
リンダヘッド部分の側断面図である。図において、2は
シリンダ、2aはシリンダライナ、3はピストン、4は
シリンダヘッドで、主燃焼室1は、ピストン3、シリン
ダライナ2a、シリンダヘッド4で囲まれている。この
例では、シリンダヘッド4の中央に点火プラグ付予燃焼
室ユニット10が配設され、両サイドにパイロット燃料
噴射弁付予燃焼室ユニット30が配設されている。Embodiments of the present invention will be described below with reference to the drawings. FIG. 1 is a side sectional view of a cylinder head portion of the gas engine according to the embodiment. In the figure, 2 is a cylinder, 2a is a cylinder liner, 3 is a piston, 4 is a cylinder head, and the main combustion chamber 1 is surrounded by a piston 3, a cylinder liner 2a and a cylinder head 4. In this example, a pre-combustion chamber unit 10 with a spark plug is arranged at the center of the cylinder head 4 and a pre-combustion chamber unit 30 with a pilot fuel injection valve is arranged on both sides.
【0011】点火プラグ付予燃焼室ユニット(以下、単
に「点火プラグ付予燃焼室」と言う場合もある)10
は、シリンダヘッド4に、予燃焼室噴口14と予燃焼室
本体13を組み込むことにより形成されている。15
は、予燃焼室噴口14内に確保された予燃焼室12内へ
直接燃料ガス(パイロットガス)を供給するための燃料
噴射孔である。主燃焼室1と予燃焼室12は、予燃焼室
12の下端部に設けられた複数の連絡孔17により連通
されている。予燃焼室本体13には点火プラグ11が装
着されており、これが予燃焼室12内の混合気の点火源
となる。点火プラグ付予燃焼室ユニット10の予燃焼室
12の容積比(圧縮上死点時の総燃焼室容積に対する
比)を数%と小さくして、超低NOx化を実現してい
る。Pre-combustion chamber unit with spark plug (hereinafter sometimes simply referred to as "pre-combustion chamber with spark plug") 10
Is formed by incorporating the pre-combustion chamber injection port 14 and the pre-combustion chamber main body 13 into the cylinder head 4. Fifteen
Is a fuel injection hole for directly supplying a fuel gas (pilot gas) into the pre-combustion chamber 12 secured in the pre-combustion chamber injection port 14. The main combustion chamber 1 and the pre-combustion chamber 12 are connected by a plurality of communication holes 17 provided at the lower end of the pre-combustion chamber 12. An ignition plug 11 is mounted on the pre-combustion chamber main body 13 and serves as an ignition source for the air-fuel mixture in the pre-combustion chamber 12. The volume ratio of the pre-combustion chamber 12 of the pre-combustion chamber unit 10 with a spark plug (the ratio to the total combustion chamber volume at the time of compression top dead center) is reduced to several percent, thereby realizing ultra-low NOx.
【0012】また、パイロット燃料噴射弁付予燃焼室ユ
ニット(以下、単に「パイロット燃料噴射弁付予燃焼
室」と言う場合もある)30は、予燃焼室31内に臨ま
せてパイロット燃料噴射弁32を備えており、パイロッ
ト燃料の噴射により予燃焼室31内の混合気を点火させ
る。主燃焼室1と予燃焼室31は、予燃焼室下端部に設
けられた単数または複数の連絡孔33により連通されて
いる。A pre-combustion chamber unit with a pilot fuel injection valve (hereinafter sometimes simply referred to as a “pre-combustion chamber with a pilot fuel injection valve”) 30 faces the inside of a pre-combustion chamber 31 and has a pilot fuel injection valve. 32, and ignites the air-fuel mixture in the pre-combustion chamber 31 by injection of pilot fuel. The main combustion chamber 1 and the pre-combustion chamber 31 are communicated by one or more communication holes 33 provided at the lower end of the pre-combustion chamber.
【0013】このエンジンの場合、点火プラグ付予燃焼
室10を主着火源として使用してエンジンを起動させ
る。つまり、ディーゼル起動はしないので、パイロット
燃料噴射弁付予燃焼室ユニット30を小さくできる。パ
イロット油量を全熱量比の0.2〜5%程度とすると、
予燃焼室31の容積比は全体の1〜3%程度に小さくす
ることができる。従って、シリンダヘッド4の両サイド
に配置することが可能となる。これは、従来の予燃焼型
ディーゼルエンジンの予燃焼室の容積比が20〜30%
と設計されているのと大きく異なる点である。In the case of this engine, the engine is started using the pre-combustion chamber 10 with a spark plug as a main ignition source. That is, since the diesel is not started, the size of the pre-combustion chamber unit 30 with the pilot fuel injection valve can be reduced. When the pilot oil amount is about 0.2 to 5% of the total calorific value ratio,
The volume ratio of the pre-combustion chamber 31 can be reduced to about 1 to 3% of the whole. Therefore, it can be arranged on both sides of the cylinder head 4. This is because the volume ratio of the pre-combustion chamber of the conventional pre-combustion type diesel engine is 20 to 30%.
This is a major difference from the design.
【0014】また、パイロット燃料噴射弁32につなが
る燃料噴射ポンプは、図2、図3に示すように、クラン
クケースのカム室のドアに取り付けられている。図2、
図3において、50はクランクケース、51はカム軸、
52はクランクケース上面、53はカム室のドア、54
はカム面点検窓であり、カム室のドア53の座に燃料噴
射ポンプ60が設けられている。この場合、パイロット
油量がディーゼル運転を仮定した場合の定格噴射量に対
して0.2〜5%程度と非常に少ないので、一般のディ
ーゼルエンジン用のものと比べて非常に小型の燃料噴射
ポンプ60が取り付けられている。A fuel injection pump connected to the pilot fuel injection valve 32 is mounted on a door of a cam chamber of a crankcase as shown in FIGS. FIG.
3, 50 is a crankcase, 51 is a camshaft,
52 is the top of the crankcase, 53 is the door of the cam chamber, 54
Reference numeral denotes a cam surface inspection window, and a fuel injection pump 60 is provided at a seat of a door 53 of the cam chamber. In this case, since the pilot oil amount is as small as about 0.2 to 5% of the rated injection amount assuming diesel operation, the fuel injection pump is very small as compared with a general diesel engine. 60 is attached.
【0015】次に運転モードについて説明する。運転モ
ードとしては、 (1)火花点火による予燃焼室方式ガスエンジン (2)パイロット着火ガスエンジン (3)2種着火源(火花点火、パイロット着火)ガスエ
ンジン のいずれかを任意に選択できる。点火源の数と方法が複
数ある上、それらが並列系となっているので、点火源の
信頼性が高まっている。Next, the operation mode will be described. As the operation mode, any one of (1) a pre-combustion chamber gas engine using spark ignition, (2) a pilot ignition gas engine, and (3) a two-type ignition source (spark ignition, pilot ignition) gas engine can be arbitrarily selected. Since there are a plurality of ignition sources and a plurality of methods, and they are arranged in parallel, the reliability of the ignition sources is increased.
【0016】実際には、起動時は点火プラグ着火、負荷
時はパイロット噴射着火を併用するのが望ましく、そう
することで積極的に燃焼効率を改善することができる
が、負荷時に火花着火を停止させても運転上は差し支え
ない。In practice, it is desirable to use ignition plug ignition at the time of start-up and pilot injection ignition at the time of load, so that combustion efficiency can be positively improved. Even if you do, there is no problem in driving.
【0017】(1)火花点火による運転モードのとき:
この運転モードでは、燃料としては気体燃料(ガス)の
みを用い、点火プラグ付予燃焼室を、主燃焼室1の気体
燃料と空気との混合気の点火源とする。具体的には、排
気行程後半から吸気行程前半において、点火プラグ付予
燃焼室ユニット10(以降の各符号は図1による)の燃
料噴射孔15から、予燃焼室12内にパイロットガスを
供給する。パイロットガスは、パイロツトガスヘッダ
(図示略)内の圧力と主燃焼室1内の圧力との差圧によ
り供給され、その量は前記差圧を変えることにより調整
される。また、主燃焼室には、燃料ガスと空気の混合気
を吸気行程において供給する。圧縮行程では、ピストン
3により主燃焼室1内の希薄混含気が圧縮されること
で、同混合気の一部が点火プラグ付予燃焼室ユニット1
0の連絡孔17を介して予燃焼室12に流入する。流入
の際に、予燃焼室12内の燃料ガスと希薄混合気が混ざ
り、平均空気過剰率1.0程度の濃度となる。この状態
になったところで、点火プラグ11のギャップ間におい
て火花放電を生じさせて、予燃焼室内の混合気を着火燃
焼させる。予燃焼室12において燃焼した火炎は、主燃
焼室1へ伝播し、主燃焼室1の混合気の着火源となり、
主燃焼室1内の混合気全体を燃焼させる。(1) In the operation mode by spark ignition:
In this operation mode, only gaseous fuel (gas) is used as fuel, and the pre-combustion chamber with a spark plug is used as an ignition source for a mixture of gaseous fuel and air in the main combustion chamber 1. Specifically, the pilot gas is supplied into the pre-combustion chamber 12 from the fuel injection holes 15 of the pre-combustion chamber unit 10 with a spark plug (hereinafter each reference numeral is shown in FIG. 1) from the latter half of the exhaust stroke to the first half of the intake stroke. . The pilot gas is supplied by a pressure difference between a pressure in a pilot gas header (not shown) and a pressure in the main combustion chamber 1, and the amount thereof is adjusted by changing the pressure difference. Further, a mixture of fuel gas and air is supplied to the main combustion chamber during an intake stroke. In the compression stroke, a part of the air-fuel mixture in the main combustion chamber 1 is compressed by the piston 3 so that a part of the air-fuel mixture is reduced.
It flows into the pre-combustion chamber 12 through the communication hole 17 of 0. At the time of inflow, the fuel gas and the lean gas mixture in the pre-combustion chamber 12 are mixed, and the concentration becomes about 1.0 as the average excess air ratio. In this state, a spark discharge is generated between the gaps of the ignition plug 11 to ignite and burn the air-fuel mixture in the pre-combustion chamber. The flame burned in the pre-combustion chamber 12 propagates to the main combustion chamber 1 and becomes an ignition source for the air-fuel mixture in the main combustion chamber 1.
The entire mixture in the main combustion chamber 1 is burned.
【0018】(2)パイロット燃料噴射による着火の運
転モードのとき:この運転モードでは、主燃料として気
体燃料を用いるものの、副燃料として液体燃料をパイロ
ット油として使用する。そして、パイロット燃料噴射弁
付予燃焼室ユニット30の予燃焼室31内に、パイロッ
ト燃料噴射弁32よりパイロット油を噴射する。即ち、
吸気行程において主燃焼室1に燃料と空気の混合気を供
給すると、圧縮行程では、ピストン3により主燃焼室1
内の希薄混合気が圧縮されて、予燃焼室連絡孔33を介
して予燃焼室31に流入する。そこで、上死点直前の1
0〜30°(クランク角度)あたりで、パイロット燃料
噴射弁32から少量の燃料油を噴射する。そうすると、
噴射した燃料が着火燃焼し、これが点火源となって混合
気が着火燃焼する。そして、予燃焼室31にて燃焼した
火炎が、主燃焼室1へ伝播し、主燃焼室1の混合気の着
火源となって、主燃焼室1の混合気全体が燃焼する。(2) In the operation mode of ignition by pilot fuel injection: In this operation mode, gas fuel is used as main fuel, but liquid fuel is used as pilot oil as auxiliary fuel. Then, pilot oil is injected from the pilot fuel injection valve 32 into the pre-combustion chamber 31 of the pre-combustion chamber unit 30 with the pilot fuel injection valve. That is,
When a mixture of fuel and air is supplied to the main combustion chamber 1 in the intake stroke, the main combustion chamber 1 is moved by the piston 3 in the compression stroke.
The lean mixture is compressed and flows into the pre-combustion chamber 31 through the pre-combustion chamber communication hole 33. So, just before top dead center,
A small amount of fuel oil is injected from pilot fuel injector 32 around 0 to 30 ° (crank angle). Then,
The injected fuel is ignited and combusted, and the mixture becomes the ignition source to ignite and combust. Then, the flame burned in the pre-combustion chamber 31 propagates to the main combustion chamber 1 and serves as an ignition source for the air-fuel mixture in the main combustion chamber 1 so that the entire air-fuel mixture in the main combustion chamber 1 burns.
【0019】図4はパイロット燃料油量を変化させなが
ら性能試験を実施した結果(正味熱効率とNOx・スモ
ーク度の関係)を、各種燃焼方式(デュアルフュエルエ
ンジン、ディーゼルエンジン、予燃焼室方式火花点火ガ
スエンジン)と比較して示している。本図から、パイロ
ット燃料噴射でのエンジン性能は、予燃焼室方式火花点
火ガスエンジンと同レベルの排気ガス性状(NOxと煤
塵)を達成しながら、熱効率は火花点火よりも高く、デ
ィーゼルエンジンと同レベルであることが分かる。FIG. 4 shows the results of performance tests (relationship between net thermal efficiency and NOx / smoke degree) while changing the pilot fuel oil amount, based on various combustion types (dual fuel engine, diesel engine, pre-combustion chamber type spark ignition). Gas engine). From this figure, it can be seen that the engine performance in the pilot fuel injection achieves the same level of exhaust gas properties (NOx and dust) as the pre-combustion chamber type spark ignition gas engine, but the thermal efficiency is higher than that of the spark ignition and is the same as that of the diesel engine. It turns out that it is a level.
【0020】なお、パイロット燃料噴射の場合、点火プ
ラグ付予燃焼室10のパイロットガスは不要となる。ま
た、パイロット油量は全熱量比0.2〜5%程度にでき
るので、常時噴射させてもガバニングに影響を与えな
い。従って、燃料噴射ポンプのラックは固定しても差し
支えなく、複雑なリンク機構が不要である。また、エン
ジン運転時の調速は、エンジンガバナによって燃料ガス
量を調整することにより実施することができる。In the case of pilot fuel injection, pilot gas in the pre-combustion chamber 10 with a spark plug is not required. In addition, since the pilot oil amount can be set to a total heat amount ratio of about 0.2 to 5%, governing is not affected even if it is always injected. Therefore, the rack of the fuel injection pump may be fixed, and a complicated link mechanism is not required. In addition, speed control during engine operation can be performed by adjusting the amount of fuel gas by the engine governor.
【0021】(3)ハイブリッドイグニッションガスエ
ンジン運転モード:この運転モードでは、同一燃焼サイ
クルにおいて、中央の点火プラグ付予燃焼室10と、両
サイドのパイロット燃料噴射弁付予燃焼室30をほぼ同
時に、または若干ずらして作用させ、これらを着火源と
して主燃焼室1の混合気を燃焼させる。従って、多点点
火による混合気の燃焼促進を実現できる。さらに、これ
ら着火源の火花点火時期及びパイロット燃料噴射時期と
噴射量を最適調整することにより、混合気の燃焼性が改
善され、短期燃焼化による熱効率改善の効果が得られ
る。(3) Hybrid ignition gas engine operation mode: In this operation mode, in the same combustion cycle, the central pre-combustion chamber 10 with a spark plug and the pre-combustion chambers 30 with pilot fuel injection valves on both sides are almost simultaneously. Alternatively, the gas mixture in the main combustion chamber 1 is burned using these as ignition sources. Therefore, it is possible to promote the combustion of the air-fuel mixture by the multipoint ignition. Furthermore, by optimally adjusting the spark ignition timing, pilot fuel injection timing, and injection quantity of these ignition sources, the combustibility of the air-fuel mixture is improved, and the effect of improving thermal efficiency by short-term combustion is obtained.
【0022】このように、ハイブリッドイグニッション
ガスエンジンモードで運転した場合の多点点火による急
速燃焼化の作用効果について補足する。図5(a)は単
一燃焼室方式(予燃焼室を持たない主燃焼室だけの方
式)と予燃焼室方式(本実施形態と類似の場合)の熱発
生率の比較実験をした結果を示している。図5(a)に
おいて、PCCは予燃焼室方式を示し、OCは単一燃焼
室方式を示す。但し、OCの場合、点火プラグ1個の場
合=OC(1 Spark Plug)と、点火プラグ2個の場合=
OC(2 Spark Plugs)についても比較した。実験に際し
ては、図5(b)に示すように、中央とサイドに第1、
第2の点火プラグ(Spark Plug)A、Bを配置し、点火
プラグ1個の場合は中央の点火プラグAのみ使用し、点
火プラグ2個の場合は両方の点火プラグA、Bを使用し
た。The effect of rapid combustion by multipoint ignition when operating in the hybrid ignition gas engine mode will be supplemented. FIG. 5 (a) shows the results of a comparison experiment of the heat release rate between the single combustion chamber system (only the main combustion chamber without a pre-combustion chamber) and the pre-combustion chamber system (similar to this embodiment). Is shown. In FIG. 5A, PCC indicates a pre-combustion chamber system, and OC indicates a single combustion chamber system. However, in the case of OC, one spark plug = OC (1 Spark Plug) and two spark plugs =
OC (2 Spark Plugs) was also compared. At the time of the experiment, as shown in FIG.
Second spark plugs (Spark Plugs) A and B were arranged. In the case of one spark plug, only the center spark plug A was used, and in the case of two spark plugs, both spark plugs A and B were used.
【0023】図5(a)に示される熱発生率パターン
は、多点点火(点火プラグ2個の場合)や、強力な点火
エネルギの発生(予燃焼室を着火源とするPCCの場
合)が、急速燃焼を実現するためにきわめて有効な技術
であることを証明している。すなわち、点火プラグの本
数を2本(図中一点鎖線)にすると、上死点後40度近
辺までに熱発生が完了しており、点火プラグ1本(図中
破線)に比較すると、短期燃焼していることが分かる。
また、更に強力な点火エネルギを有する予燃焼室方式
(図中実線)によれば、上死点後30度近辺までに熱発
生が完了しており、より短期燃焼が実現できることが分
かる。短期燃焼は熱効率の向上に寄与するので、本実施
形態のように、強力な点火エネルギを有する点火源を多
数配置する(予燃焼室を3つ配置する)ことにより、燃
焼改善に寄与することができ、高熱効率を実現すること
ができるようになる。The heat release rate pattern shown in FIG. 5 (a) indicates multipoint ignition (in the case of two spark plugs) or generation of strong ignition energy (in the case of PCC using a pre-combustion chamber as an ignition source). Has proven to be a very effective technology for realizing rapid combustion. That is, when the number of spark plugs is set to two (dashed line in the figure), heat generation is completed by about 40 degrees after the top dead center. You can see that it is doing.
Further, according to the pre-combustion chamber system having a stronger ignition energy (solid line in the figure), heat generation is completed by around 30 degrees after the top dead center, and it can be seen that short-term combustion can be realized. Since short-term combustion contributes to improvement of thermal efficiency, it is possible to contribute to improvement of combustion by arranging a large number of ignition sources having strong ignition energy (arranging three pre-combustion chambers) as in the present embodiment. And high thermal efficiency can be realized.
【0024】ちなみに、点火エネルギについて比較して
みると、点火プラグのみの場合は約0.1Jであるが、
点火プラグ付予燃焼室(予燃焼室容積比2%)の場合
は、供給燃料ガスの熱量を点火エネルギとすることがで
きることから、3000Jにもなる。また、パイロット
噴射の場合は、パイロット燃料の油量を全熱量比の1%
とすると、約600Jになる。従って、点火プラグ付予
燃焼室10及びパイロット燃料噴射弁付予燃焼室30に
よる多点点火が燃焼改善に寄与するところは非常に大き
いことが分かる。By comparison, the ignition energy is about 0.1 J in the case of only the spark plug,
In the case of the pre-combustion chamber with a spark plug (the pre-combustion chamber volume ratio is 2%), the heat quantity of the supplied fuel gas can be used as the ignition energy. In the case of pilot injection, the amount of oil in the pilot fuel is 1% of the total calorific value ratio.
Then, it becomes about 600J. Therefore, it can be seen that the multipoint ignition by the pre-combustion chamber 10 with the spark plug and the pre-combustion chamber 30 with the pilot fuel injection valve greatly contributes to the improvement of combustion.
【0025】なお、上記実施形態では、中央に点火プラ
グ付予燃焼室10を配置し、両サイドにパイロット燃料
噴射弁付予燃焼室30を配置した場合を示したが、中央
にパイロット燃料噴射弁付予燃焼室30を配置し、両サ
イドに点火プラグ付予燃焼室10を配置してもよい。In the above embodiment, the case where the pre-combustion chamber 10 with the ignition plug is arranged at the center and the pre-combustion chamber 30 with the pilot fuel injection valve is arranged at both sides is shown. The pre-combustion chamber with an ignition plug 30 may be arranged, and the pre-combustion chamber with an ignition plug 10 may be arranged on both sides.
【0026】[0026]
【発明の効果】以上説明したように、請求項1及び2の
発明によれば、シリンダヘッドに、主燃焼室内の混合気
の着火源となる点火プラグ付予燃焼室とパイロット燃料
噴射弁付予燃焼室とを設けたので、火花点火による着
火、パイロット燃料噴射による着火、2種同時着火のい
ずれかの運転モードを任意に選択することができる。従
って、起動時は点火プラグ着火、負荷時はさらにパイロ
ット噴射着火を併用することにより、低NOxを維持し
ながら、高いエンジン熱効率を得ることができ、これに
よりガスエンジンの低公害性(低CO2)を生かすこと
ができる。また、請求項3の発明によれば、小さな燃料
噴射ポンプでもクランクケースを特別に改造せずに設置
することができる。As described above, according to the first and second aspects of the present invention, the cylinder head is provided with a pre-combustion chamber with a spark plug and a pilot fuel injection valve, which serves as an ignition source for air-fuel mixture in the main combustion chamber. Since the pre-combustion chamber is provided, any one of the operation modes of ignition by spark ignition, ignition by pilot fuel injection, and simultaneous ignition of two types can be selected. Accordingly, high engine thermal efficiency can be obtained while maintaining low NOx by using the ignition plug ignition at the time of starting and the pilot injection ignition at the time of load, whereby the low pollution (low CO2) of the gas engine is achieved. Can be utilized. According to the third aspect of the present invention, even a small fuel injection pump can be installed without special modification of the crankcase.
【図1】 本発明の実施形態のガスエンジンの要部側断
面図である。FIG. 1 is a side sectional view of a main part of a gas engine according to an embodiment of the present invention.
【図2】 本発明の実施形態のガスエンジンにおける燃
料噴射ポンプの取付状態を示す平面図である。FIG. 2 is a plan view showing a mounting state of a fuel injection pump in the gas engine according to the embodiment of the present invention.
【図3】 図2のIII−III矢視図である。FIG. 3 is a view taken in the direction of arrows III-III in FIG. 2;
【図4】 実施形態のエンジンの性能の説明に用いる特
性図である。FIG. 4 is a characteristic diagram used to explain the performance of the engine of the embodiment.
【図5】 同エンジンの性能の説明に用いる特性図で、
(a)は単一燃焼室方式と予燃焼室方式の熱発生率の比
較図、(b)は点火プラグの配置箇所を示す平面図であ
る。FIG. 5 is a characteristic diagram used to explain the performance of the engine,
(A) is a comparison diagram of the heat generation rates of the single combustion chamber system and the pre-combustion chamber system, and (b) is a plan view showing the location of the ignition plug.
1 主燃焼室 2 シリンダ 3 ピストン 4 シリンダヘッド 10 点火プラグ付予燃焼室ユニット(点火プラグ付予
燃焼室) 11 点火プラグ 12 予燃焼室 30 パイロット燃料噴射弁予燃焼室ユニット(パイロ
ット燃料噴射弁予燃焼室) 31 予燃焼室 32 パイロット燃料噴射弁 53 カム室のドア 60 燃料噴射ポンプReference Signs List 1 main combustion chamber 2 cylinder 3 piston 4 cylinder head 10 pre-combustion chamber unit with spark plug (pre-combustion chamber with spark plug) 11 spark plug 12 pre-combustion chamber 30 pilot fuel injector pre-combustion chamber unit (pilot fuel injector pre-combustion) Chamber) 31 pre-combustion chamber 32 pilot fuel injection valve 53 door of cam chamber 60 fuel injection pump
───────────────────────────────────────────────────── フロントページの続き (51)Int.Cl.6 識別記号 FI F02B 43/02 F02B 43/02 F02D 19/10 F02D 19/10 F02M 61/14 310 F02M 61/14 310P 310U F02P 13/00 303 F02P 13/00 303A (72)発明者 坂上 健幸 東京都大田区蒲田本町一丁目10番1号 株 式会社新潟鉄工所内──────────────────────────────────────────────────の Continued on the front page (51) Int.Cl. 6 Identification code FI F02B 43/02 F02B 43/02 F02D 19/10 F02D 19/10 F02M 61/14 310 F02M 61/14 310P 310U F02P 13/00 303 F02P 13/00 303A (72) Inventor Takeyuki Sakagami 1-10-1 Kamatahonmachi, Ota-ku, Tokyo Inside Niigata Iron Works Co., Ltd.
Claims (3)
より画定される主燃焼室に気体燃料を供給して燃焼させ
ることにより駆動出力を得るガスエンジンであって、前
記シリンダヘッドに、前記主燃焼室内の混合気の着火源
となる点火プラグ付予燃焼室とパイロット燃料噴射弁付
予燃焼室とを設けたことを特徴とする予燃焼室方式ガス
エンジン。1. A gas engine for obtaining a drive output by supplying gaseous fuel to a main combustion chamber defined by a piston, a cylinder, and a cylinder head and burning the gaseous fuel. A pre-combustion chamber type gas engine comprising a pre-combustion chamber with a spark plug and a pre-combustion chamber with a pilot fuel injection valve, which serve as ignition sources for air.
グ付予燃焼室とパイロット燃料噴射弁付予燃焼室とをほ
ぼ同時に、または若干ずらして機能させて、これらを着
火源として主燃焼室の混合気を燃焼させることを特徴と
する請求項1記載の予燃焼室方式ガスエンジン。2. In the same combustion cycle, the pre-combustion chamber with a spark plug and the pre-combustion chamber with a pilot fuel injection valve are made to function substantially simultaneously or slightly displaced from each other, and the mixture in the main combustion chamber is used as an ignition source. The pre-combustion chamber type gas engine according to claim 1, wherein the gas is burned.
料噴射ポンプを、クランクケースのカム室のドアに取り
付けたことを特徴とする請求項1または2記載の予燃焼
室方式ガスエンジン。3. The pre-combustion chamber gas engine according to claim 1, wherein a fuel injection pump connected to the pilot fuel injection valve is mounted on a door of a cam chamber of a crankcase.
Priority Applications (8)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP13237198A JP3930639B2 (en) | 1998-05-14 | 1998-05-14 | Pre-combustion chamber type gas engine |
| US09/307,899 US6209511B1 (en) | 1998-05-14 | 1999-05-10 | Lean combustion gas engine |
| DK99401167T DK0957246T3 (en) | 1998-05-14 | 1999-05-12 | Gas engine with lean combustion |
| NO19992306A NO327837B1 (en) | 1998-05-14 | 1999-05-12 | Lean-burning gas engine |
| DE69932282T DE69932282T2 (en) | 1998-05-14 | 1999-05-12 | Magermotor |
| ES99401167T ES2268834T3 (en) | 1998-05-14 | 1999-05-12 | POOR COMBUSTION GAS ENGINE. |
| EP99401167A EP0957246B1 (en) | 1998-05-14 | 1999-05-12 | Lean combustion gas engine |
| AT99401167T ATE333039T1 (en) | 1998-05-14 | 1999-05-12 | LEAN ENGINE |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP13237198A JP3930639B2 (en) | 1998-05-14 | 1998-05-14 | Pre-combustion chamber type gas engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH11324805A true JPH11324805A (en) | 1999-11-26 |
| JP3930639B2 JP3930639B2 (en) | 2007-06-13 |
Family
ID=15079817
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP13237198A Expired - Lifetime JP3930639B2 (en) | 1998-05-14 | 1998-05-14 | Pre-combustion chamber type gas engine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP3930639B2 (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2002061523A (en) * | 2000-08-17 | 2002-02-28 | Niigata Eng Co Ltd | Starting device for pilot ignition gas engine |
| JP2004197623A (en) * | 2002-12-17 | 2004-07-15 | Mitsubishi Heavy Ind Ltd | Combustion control device for gas engine |
| JP2005090381A (en) * | 2003-09-18 | 2005-04-07 | Niigata Power Systems Co Ltd | Pilot oil ignition gas engine |
| US7028645B2 (en) | 2001-08-29 | 2006-04-18 | Niigata Power Systems Co., Ltd. | Pilot oil ignition gas engine and method of operating pilot oil ignition gas engine |
| KR101132038B1 (en) | 2004-04-16 | 2012-04-02 | 바르실라 핀랜드 오이 | A method of operating a gas engine |
| JP2014522941A (en) * | 2011-07-08 | 2014-09-08 | ヴェルツィラ シュヴェイツ アーゲー | 2-stroke internal combustion engine, 2-stroke internal combustion engine operating method, and 2-stroke engine conversion method |
| CN114790934A (en) * | 2022-03-09 | 2022-07-26 | 吉林大学 | Ignition device of natural gas engine precombustion chamber |
| CN117803486A (en) * | 2024-02-27 | 2024-04-02 | 潍柴动力股份有限公司 | Control method and device for hydrogen engine combustion system |
-
1998
- 1998-05-14 JP JP13237198A patent/JP3930639B2/en not_active Expired - Lifetime
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2002061523A (en) * | 2000-08-17 | 2002-02-28 | Niigata Eng Co Ltd | Starting device for pilot ignition gas engine |
| US6990946B2 (en) | 2000-08-17 | 2006-01-31 | Niigata Power Systems Co., Ltd. | Starting system for pilot-ignition gas engine |
| US7028645B2 (en) | 2001-08-29 | 2006-04-18 | Niigata Power Systems Co., Ltd. | Pilot oil ignition gas engine and method of operating pilot oil ignition gas engine |
| US7117826B2 (en) | 2001-08-29 | 2006-10-10 | Niigata Power Systems Co., Ltd. | Pilot oil ignition gas engine and method of operating pilot oil ignition gas engine |
| JP2004197623A (en) * | 2002-12-17 | 2004-07-15 | Mitsubishi Heavy Ind Ltd | Combustion control device for gas engine |
| JP2005090381A (en) * | 2003-09-18 | 2005-04-07 | Niigata Power Systems Co Ltd | Pilot oil ignition gas engine |
| KR101132038B1 (en) | 2004-04-16 | 2012-04-02 | 바르실라 핀랜드 오이 | A method of operating a gas engine |
| JP2014522941A (en) * | 2011-07-08 | 2014-09-08 | ヴェルツィラ シュヴェイツ アーゲー | 2-stroke internal combustion engine, 2-stroke internal combustion engine operating method, and 2-stroke engine conversion method |
| CN114790934A (en) * | 2022-03-09 | 2022-07-26 | 吉林大学 | Ignition device of natural gas engine precombustion chamber |
| CN114790934B (en) * | 2022-03-09 | 2023-11-17 | 吉林大学 | Ignition device for precombustion chamber of natural gas engine |
| CN117803486A (en) * | 2024-02-27 | 2024-04-02 | 潍柴动力股份有限公司 | Control method and device for hydrogen engine combustion system |
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|---|---|
| JP3930639B2 (en) | 2007-06-13 |
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