JPS601266Y2 - Diesel engine fuel injection nozzle - Google Patents
Diesel engine fuel injection nozzleInfo
- Publication number
- JPS601266Y2 JPS601266Y2 JP11625779U JP11625779U JPS601266Y2 JP S601266 Y2 JPS601266 Y2 JP S601266Y2 JP 11625779 U JP11625779 U JP 11625779U JP 11625779 U JP11625779 U JP 11625779U JP S601266 Y2 JPS601266 Y2 JP S601266Y2
- Authority
- JP
- Japan
- Prior art keywords
- injection
- nozzle
- groove
- main
- fuel 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.)
- Expired
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
- F02M61/18—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
- F02M61/1806—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for characterised by the arrangement of discharge orifices, e.g. orientation or size
- F02M61/184—Discharge orifices having non circular sections
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M45/00—Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship
- F02M45/02—Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship with each cyclic delivery being separated into two or more parts
- F02M45/04—Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship with each cyclic delivery being separated into two or more parts with a small initial part, e.g. initial part for partial load and initial and main part for full load
- F02M45/08—Injectors peculiar thereto
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/04—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
- F02M61/06—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series the valves being furnished at seated ends with pintle or plug shaped extensions
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
- F02M61/166—Selection of particular materials
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
- F02M61/18—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
- F02M61/1806—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for characterised by the arrangement of discharge orifices, e.g. orientation or size
- F02M61/1826—Discharge orifices having different sizes
-
- 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
- F02B3/00—Engines characterised by air compression and subsequent fuel addition
- F02B3/06—Engines characterised by air compression and subsequent fuel addition with compression ignition
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Description
【考案の詳細な説明】
この考案はディーゼルエンジンの燃料噴射ノズルに関す
る。[Detailed Description of the Invention] This invention relates to a fuel injection nozzle for a diesel engine.
従来、ディーゼルエンジンの燃料噴射ノズルとしては、
例えば第1図に示すようなものがある。Conventionally, fuel injection nozzles for diesel engines are
For example, there is one shown in FIG.
これは不ロットル型と呼ばれるもので、渦流室式ディー
ゼルエンジンに多く使用され:ている。This is called a no-throttle type and is often used in swirl chamber diesel engines.
このスロットル型噴射ノズルは、図外の燃料噴射ポンプ
より燃料通路1に圧送された燃料が噴射弁室2に入り、
ノズルの噴射開始圧力まで上昇すると針弁3の円錐形の
部分3aに上向きの力が働き、針弁3を持上げるように
なる。In this throttle type injection nozzle, fuel is pumped into a fuel passage 1 from a fuel injection pump (not shown) and enters an injection valve chamber 2.
When the pressure rises to the nozzle injection start pressure, an upward force acts on the conical portion 3a of the needle valve 3, lifting the needle valve 3.
この噴射初期では針弁3先端部と噴口4との間の環状面
積が小さいため燃料噴射量が少ない。At this early stage of injection, the annular area between the tip of the needle valve 3 and the injection port 4 is small, so the amount of fuel injected is small.
そして、バルブリフトが増大すると前記環状面積が増大
して主噴射が行われるのである。When the valve lift increases, the annular area increases and main injection is performed.
(掬養賢堂 昭和48N−発行1内燃機関講義 上巻ヨ
第250頁、第251頁参照。(See Kyokuyo Kendo 1978 N-Publisher 1 Lecture on Internal Combustion Engines, Volume 1, pages 250 and 251.
第2図A、 Bに示すものはディーゼルエンジンの騒音
対策用として、先行噴射をする削口5を持つビントーク
ス(pintaux)ノズルであり、寒冷時始動性改善
効果もあるため近年注目されている。The one shown in Figures 2A and B is a pintaux nozzle with a cutting hole 5 that performs advance injection as a noise countermeasure for diesel engines, and has been attracting attention in recent years because it also improves starting performance in cold weather. .
このノズルは燃料噴射初期、つまり針弁3のリフト量が
小さい領域では主噴口4近傍に開口した削口5より先行
噴射し、そしてバルブリフト量が増大して主噴口4の環
状面積が増大すると該主噴口4より主噴射を行うように
したものであり、特に第2図Bに示すものにあっては針
弁3先端部に噴射初期に主噴口4を閉塞するつば部6を
設けて先行噴射を積極的に行わせるようにしたものであ
る。This nozzle injects fuel in advance from the cutting hole 5 opened near the main nozzle 4 in the early stage of fuel injection, that is, in the region where the lift of the needle valve 3 is small, and when the valve lift increases and the annular area of the main nozzle 4 increases. The main injection is performed from the main nozzle 4, and in particular, in the one shown in FIG. The system is designed to actively perform injection.
このように、削口5より先行噴射するようにしたものに
あっては主噴口4近傍の空気利用率が高まるため、第1
図に示すスロットル型のものと比較して着火性が向上す
る利点が挙げられる。In this way, in the case where the injection is performed in advance from the cutting hole 5, the air utilization rate near the main nozzle 4 increases, so the first
It has the advantage of improved ignition performance compared to the throttle type shown in the figure.
■養賢堂 昭和4坪発行1内燃機関講義 上巻ヨ第30
0頁参照。■Yokendo Published by Showa 4 Tsubo 1 Internal Combustion Engine Lecture Volume 1 Yo No. 30
See page 0.
しかしながら、削口5による先行噴射によって主噴口4
周りの空気利用率が高まるといっても、該削口5が単純
なホール形状であるため、先行噴射流は充分に微粒化さ
れた噴霧とはならず、噴射流のままであって空気と混合
が十分に、かつ速かに行われず空気利用率の大幅な改善
は期待できないので、スモーク発生の低減につながらな
いものである。However, due to the advance injection from the cutting port 5, the main nozzle 4
Even though the utilization rate of the surrounding air is increased, because the cutting hole 5 has a simple hole shape, the preceding jet stream does not become a sufficiently atomized spray, and it remains a jet stream and is not mixed with air. Since mixing is not carried out sufficiently and quickly, a significant improvement in air utilization cannot be expected, and therefore it does not lead to a reduction in smoke generation.
また、着火遅れも充分短縮できないため、ノッキング発
生防止も効果的に行われず、従つて騒音低減にもあまり
有効でないという問題があった。Furthermore, since the ignition delay cannot be sufficiently shortened, the occurrence of knocking cannot be effectively prevented, and therefore, there is a problem that it is not very effective in reducing noise.
この考案はかかる従来の欠点を解消するためになされた
もので、主噴口近傍に溝を形成上で、この溝内に削口を
開口させると共に、該溝に前記削口を覆って多孔質部材
を装着し、この多孔質部材により、先行噴射燃料を充分
に微粒化すると共に噴射角を拡大して空気利用率の大幅
な改善を図ったものである。This invention was made in order to eliminate such conventional drawbacks.A groove is formed near the main nozzle, a cutting hole is opened in the groove, and a porous member is placed in the groove to cover the cutting hole. This porous member sufficiently atomizes the pre-injected fuel and expands the injection angle, significantly improving air utilization.
以下、この考案の実施例を図面と共に前記従来の構成と
同一部分に同一符号を付して詳述する。Hereinafter, an embodiment of this invention will be described in detail with reference to the drawings, in which the same parts as those of the conventional structure are given the same reference numerals.
即ち、本考案にあっては第3図に例示するように、主噴
口4の近傍に削口5を開口させて噴射初期に該削口5よ
り燃料を先行噴射するようにした構成にあって、前記主
噴口4の近傍に溝7を形成して、この溝7内に前記削口
5を開口させると共に、該溝7に削口5を覆って発泡金
属、スチールウール、焼結合金、セラミックス等の多孔
質部材8を装着しである。That is, in the present invention, as illustrated in FIG. 3, a cutting hole 5 is opened near the main injection port 4, and fuel is injected in advance from the cutting hole 5 at the initial stage of injection. , a groove 7 is formed in the vicinity of the main nozzle 4, the cutting port 5 is opened in the groove 7, and the cutting port 5 is covered in the groove 7 with foamed metal, steel wool, sintered alloy, ceramics, etc. A porous member 8 such as the above is attached.
前述の削口5および溝7並に多孔質部材8の配置関係は
、例えば第4図Aに示すよう番ト主噴ロ4近傍に溝7を
同心円状に形成して、こめ溝7内に複数の削口5を開口
させて該溝7に削口5を覆って多孔質部材8を装着した
り、同B図&と示すように溝7を半円状にして複数の削
口5・を該溝7に開口させ、あるいは同図Cに示す如く
溝1を直線的に形成して該溝7に複数の削口5を開口さ
せたりすることができ、これはエンジンの要求特性に応
じて任意に設定できる。The above-mentioned arrangement relationship of the cutting hole 5 and the groove 7 as well as the porous member 8 is such that the groove 7 is formed concentrically in the vicinity of the main injection hole 4 and the groove 7 is formed in the groove 7 as shown in FIG. 4A. A plurality of cutting holes 5 may be opened and a porous member 8 may be attached to the grooves 7 to cover the cutting holes 5, or the grooves 7 may be made semicircular and a plurality of cutting holes 5. Alternatively, the groove 1 can be formed linearly and a plurality of cutting holes 5 can be opened in the groove 7 as shown in FIG. It can be set arbitrarily.
第5図は以上の構成によりなる燃料噴射ノズルNの取付
状態を示すもので、図中9はシリンダヘッド1.、「0
は渦流室、11は始動用のグロープラグ、1「2i″、
はシリンダブロック、13はピストン、14は主燃料室
を示す。FIG. 5 shows the installation state of the fuel injection nozzle N having the above structure, and 9 in the figure shows the cylinder head 1. , “0
is a swirl chamber, 11 is a glow plug for starting, 1 "2i",
13 is a cylinder block, 13 is a piston, and 14 is a main fuel chamber.
次に以上あ構成よりなる燃料噴射ノズルNの作用を説明
すると、図外の燃料ポンプより圧送された燃料は通路1
を通って噴射弁室2に入り、針弁3を押上げる。Next, to explain the operation of the fuel injection nozzle N having the above configuration, the fuel pumped under pressure from the fuel pump (not shown) is sent to the passage 1.
It enters the injection valve chamber 2 through it and pushes up the needle valve 3.
針弁3のリフト量が小さくつば部6が主噴口4を閉塞し
ている期間、燃料は削口5よO渦流室10に噴射する先
行噴射IAが行われるが、′コ1こて、本考案によれば
削口5は主噴口4近傍に形成した溝7内に開口し、しか
も、この削口5は溝7内に装着した多孔質部材8により
覆われているため、この先行噴射燃料は多孔質部材8を
通過することにより充分微粒化されると共に、シャワー
状に噴霧が広がる。During the period when the lift of the needle valve 3 is small and the flange 6 is blocking the main nozzle 4, advance injection IA is performed in which fuel is injected from the cutting hole 5 into the O swirl chamber 10. According to the invention, the cutting hole 5 opens into a groove 7 formed near the main nozzle 4, and since the cutting hole 5 is covered with a porous member 8 installed in the groove 7, this pre-injected fuel The particles are sufficiently atomized by passing through the porous member 8, and the spray is spread out in a shower-like manner.
また、このように噴射燃料が微粒化されており、しかも
噴射初期では噴射弁室2の圧力が高くないため噴霧は主
噴口4近傍にとどまり、のって、噴口4近傍の空気を十
分に利用することができスモーク発生を著しく低減でき
るのである。In addition, since the injected fuel is atomized in this way, and the pressure in the injection valve chamber 2 is not high at the beginning of injection, the spray remains near the main nozzle 4, and the air near the nozzle 4 is fully utilized. This makes it possible to significantly reduce smoke generation.
また、このように空気利用率が向上して着火遅れが短縮
されることから騒音低減効果も大きく、更に始動性改善
をも実現できるのである。Furthermore, since the air utilization rate is improved and the ignition delay is shortened in this way, the noise reduction effect is large and starting performance can also be improved.
続いて、針弁3のリフト量が大きくなり、つば部6が主
噴口4を開口すると、主噴口4の通路断面積が削口5の
それよりも大となるため、燃料は主に主噴口4より噴射
されて主噴流IBとなる。Subsequently, when the lift amount of the needle valve 3 increases and the flange 6 opens the main nozzle 4, the passage cross-sectional area of the main nozzle 4 becomes larger than that of the cut hole 5, so that the fuel mainly flows through the main nozzle. 4 and becomes the main jet IB.
こうして噴射された主噴流IBは渦流室2の中心付近の
空気を充分利用し、安定した燃焼が行われる。The main jet stream IB injected in this way makes full use of the air near the center of the swirl chamber 2, and stable combustion is performed.
以上のようにこの考案によれば、削口は主噴口近傍に形
成した溝内に開口し、しかも、この削口は溝内に装着し
た多孔質部材で覆われているため溝形成部分で多孔質部
材によって、先行噴射時に噴射燃料を十分に微粒化させ
ると共に、噴霧角を拡大できるため圭噴白周りの空気と
の混合が充分かつ迅速に行われ、空気利用率を大幅に改
善してスモーク発生の低減、着火遅れの短縮化による騒
音低減、始動性の改善を実現できるという優れた実用上
の効果を有する。As described above, according to this invention, the cutting hole opens into the groove formed near the main nozzle, and since this cutting hole is covered with a porous member installed in the groove, the groove is formed with porous holes. The quality material allows the injected fuel to be sufficiently atomized during advance injection, and the spray angle can be expanded, so it is mixed with the air around Keishinaku sufficiently and quickly, greatly improving the air utilization rate and producing smoke. It has excellent practical effects in that it can reduce noise, reduce noise by shortening ignition delay, and improve startability.
第1,2図はそれぞれ従来のノズルを示す断面説明図、
第3図はとめ考案のノズルの一実施例を示す断面説明図
、□第4図A、B、Cは主噴口と削口並に溝、多孔質部
材とめ関係を示すノズル底面図、第5図はこめ考案のノ
ズルの取付状態を示す断面図である。
:′1・・・・・・燃料通路、2・・・・・・噴射弁室
、3・・・・・・針弁、4・・・・・・主噴口、5・=
・・・・削口、7・・・・・・溝、8・・・・・・多孔
質部材。Figures 1 and 2 are cross-sectional explanatory diagrams showing conventional nozzles, respectively;
Figure 3 is a cross-sectional explanatory diagram showing an example of a nozzle designed with a grommet, □ Figure 4 A, B, and C are bottom views of the nozzle showing the relationship between the main nozzle, the cutting hole, the groove, and the porous member, and Figure 5. The figure is a cross-sectional view showing the installed state of the nozzle proposed by Kome. :'1...Fuel passage, 2...Injection valve chamber, 3...Needle valve, 4...Main injection port, 5...=
...Drilling hole, 7...Groove, 8...Porous member.
Claims (1)
射し、この先行噴射に続いて主噴口から主噴射するディ
ーゼルエンジンの燃料噴射ノズルにおいて、前記主噴口
近傍に溝を形成して、この溝内に前記削口を開口させる
と共に、該溝に前記削口を覆って多孔質部材を装着した
ことを特徴とするディーゼルエンジンの燃料噴射ノズル
。In a fuel injection nozzle for a diesel engine that performs preliminary injection from a cutting hole that opens near the main nozzle of the fuel injection nozzle, and performs main injection from the main nozzle following this preliminary injection, a groove is formed near the main nozzle, and the groove is formed in the vicinity of the main nozzle. A fuel injection nozzle for a diesel engine, characterized in that the cut hole is opened in the groove, and a porous member is attached to the groove to cover the cut hole.
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP11625779U JPS601266Y2 (en) | 1979-08-23 | 1979-08-23 | Diesel engine fuel injection nozzle |
DE19803031298 DE3031298A1 (en) | 1979-08-23 | 1980-08-19 | INJECTION DEVICE FOR THE FUEL SUPPLY OF A DIESEL ENGINE |
GB8027386A GB2057057A (en) | 1979-08-23 | 1980-08-22 | Fuel injector for diesel engine |
FR8018413A FR2463861A1 (en) | 1979-08-23 | 1980-08-22 | FUEL INJECTOR FOR DIESEL ENGINE |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP11625779U JPS601266Y2 (en) | 1979-08-23 | 1979-08-23 | Diesel engine fuel injection nozzle |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS5634060U JPS5634060U (en) | 1981-04-03 |
JPS601266Y2 true JPS601266Y2 (en) | 1985-01-14 |
Family
ID=14682627
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP11625779U Expired JPS601266Y2 (en) | 1979-08-23 | 1979-08-23 | Diesel engine fuel injection nozzle |
Country Status (4)
Country | Link |
---|---|
JP (1) | JPS601266Y2 (en) |
DE (1) | DE3031298A1 (en) |
FR (1) | FR2463861A1 (en) |
GB (1) | GB2057057A (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6085216A (en) * | 1983-10-18 | 1985-05-14 | Isuzu Motors Ltd | Vortex flow combustion chamber type diesel engine |
JPS6073876U (en) * | 1983-10-28 | 1985-05-24 | いすゞ自動車株式会社 | fuel injection nozzle |
JPS60261974A (en) * | 1984-06-11 | 1985-12-25 | Isuzu Motors Ltd | Fuel injection nozzle for diesel engine |
CA1289429C (en) * | 1985-07-19 | 1991-09-24 | Roy Stanley Brooks | Nozzles for fuel injection systems |
FR2663084B1 (en) * | 1990-06-07 | 1992-07-31 | Semt Pielstick | INJECTION DEVICE FOR AN INTERNAL COMBUSTION ENGINE. |
NL2002079C (en) * | 2008-10-10 | 2010-04-13 | Univ Eindhoven Tech | FUEL INJECTOR FOR A BURNING ENGINE. |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR791105A (en) * | 1934-07-04 | 1935-12-04 | Siemens Ag | Injection device for diesel engines with pre-injection and main injection |
US2627254A (en) * | 1947-06-12 | 1953-02-03 | Texas Co | Fuel injection nozzle |
FR1056529A (en) * | 1951-07-20 | 1954-03-01 | Injection nozzle for internal combustion engines | |
CH372501A (en) * | 1959-05-25 | 1963-10-15 | Saurer Ag Adolph | Injection internal combustion engine |
US3559892A (en) * | 1968-06-18 | 1971-02-02 | Ambac Ind | Fuel injection nozzle with auxiliary spray orifice |
DE2655793A1 (en) * | 1976-12-09 | 1978-06-22 | Maschf Augsburg Nuernberg Ag | CONTROLLED MULTI-HOLE INJECTION NOZZLE |
-
1979
- 1979-08-23 JP JP11625779U patent/JPS601266Y2/en not_active Expired
-
1980
- 1980-08-19 DE DE19803031298 patent/DE3031298A1/en not_active Withdrawn
- 1980-08-22 GB GB8027386A patent/GB2057057A/en not_active Withdrawn
- 1980-08-22 FR FR8018413A patent/FR2463861A1/en active Granted
Also Published As
Publication number | Publication date |
---|---|
DE3031298A1 (en) | 1981-03-26 |
FR2463861B1 (en) | 1985-03-01 |
JPS5634060U (en) | 1981-04-03 |
FR2463861A1 (en) | 1981-02-27 |
GB2057057A (en) | 1981-03-25 |
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