JPH10176630A - Fuel injection nozzle for diesel engine - Google Patents

Fuel injection nozzle for diesel engine

Info

Publication number
JPH10176630A
JPH10176630A JP33419496A JP33419496A JPH10176630A JP H10176630 A JPH10176630 A JP H10176630A JP 33419496 A JP33419496 A JP 33419496A JP 33419496 A JP33419496 A JP 33419496A JP H10176630 A JPH10176630 A JP H10176630A
Authority
JP
Japan
Prior art keywords
nozzle
fuel
sub
nozzle body
needle valve
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.)
Pending
Application number
JP33419496A
Other languages
Japanese (ja)
Inventor
Katsuhiko Shirai
克彦 白井
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.)
Daihatsu Motor Co Ltd
Original Assignee
Daihatsu Motor Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Daihatsu Motor Co Ltd filed Critical Daihatsu Motor Co Ltd
Priority to JP33419496A priority Critical patent/JPH10176630A/en
Publication of JPH10176630A publication Critical patent/JPH10176630A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/162Means to impart a whirling motion to fuel upstream or near discharging orifices
    • F02M61/163Means being injection-valves with helically or spirally shaped grooves

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

PROBLEM TO BE SOLVED: To promote the atomization of fuel and the dispersion thereof over a wide range by a fuel injection nozzle comprising a needle valve element which is held inside a nozzle body and is integrally formed with a pin part inserted through a nozzle hole formed through the head face of the nozzle body. SOLUTION: A nozzle body 1 is perforated with a plurality of subsidiary nozzle holes 11 such that their one ends are situated between a valve part 5 of a needle valve element 4 adapted to contact with a valve seat face 6 of the nozzle body 1 and a pin part 10 thereof and the other ends are situated on a head face 2 of the nozzle body 1. The needle valve element 4 is formed with spiral grooves 13 at the outer periphery of its part 12 exposed to a fuel sump 9 defined inside the nozzle body 1.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は、ディーゼル機関に
おいて、その燃焼室に燃料噴射供給するためのピントル
又はスロットル型の燃料噴射ノズルの改良に関するもの
である。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a pintle or throttle type fuel injection nozzle for supplying fuel to a combustion chamber of a diesel engine.

【0002】[0002]

【従来の技術と発明が解決しようとする課題】一般に、
ピントル又はスロットル型の燃料噴射ノズルは、従来か
ら良く知られ、且つ、例えば、実公昭61−8223号
公報等に記載されているように、ノズル本体内に収納し
たニードル弁体にピン部を一体的に設け、このピン部
を、前記ノズル本体における噴出孔内に挿入することに
より、前記噴出孔からの燃料を中空の円錐状に噴出する
ように構成したものである。
2. Description of the Related Art In general,
Pintle or throttle type fuel injection nozzles are well known in the art, and as described in, for example, Japanese Utility Model Publication No. 61-8223, a pin portion is integrated with a needle valve body housed in a nozzle body. The pin portion is inserted into the ejection hole of the nozzle body so that the fuel is ejected from the ejection hole in a hollow conical shape.

【0003】しかし、このように燃料を中空の円錐状に
噴出するだけでは、燃料の微細化には限度が存在するか
ら、排気ガス中に、HC等の未燃焼成分が多くなるので
あった。本発明は、ピントル又はスロットル型の燃料噴
射ノズルにおいて、その噴射燃料を寄り微細化して、未
燃焼成分の低減を図ることを技術的課題とするものであ
る。
However, simply ejecting the fuel in the shape of a hollow cone as described above has a limit in miniaturization of the fuel, so that unburned components such as HC are increased in the exhaust gas. SUMMARY OF THE INVENTION It is an object of the present invention to provide a pintle or throttle type fuel injection nozzle in which the injected fuel is made finer to reduce unburned components.

【0004】[0004]

【課題を解決するための手段】この技術的課題を達成す
るため本発明の請求項1は、「ノズル本体内に収納した
ニードル弁体にピン部を一体的に設け、このピン部を、
前記ノズル本体にその先端面に開口するように穿設した
噴出孔内に挿入して成る燃料噴射ノズルにおいて、前記
ノズル本体に、複数個の副噴出孔を、当該副噴出孔の一
端が前記ニードル弁のうちノズル本体側の弁座面に接当
する弁部と前記ピン部との間の部分に他端が前記先端面
に各々に開口するように穿設する一方、前記ニードル弁
のうち前記ノズル本体に設けられている燃料溜室内にの
ぞむ部分における外周面に、螺旋溝を設ける。」と言う
構成にした。
In order to achieve this technical object, a first aspect of the present invention is to provide a structure in which a pin portion is integrally provided on a needle valve body housed in a nozzle body.
In a fuel injection nozzle which is inserted into an injection hole formed in the nozzle body so as to open at a tip end surface thereof, a plurality of auxiliary injection holes are provided in the nozzle body, and one end of the auxiliary injection hole is provided with the needle. The other end of the valve is bored in a portion between the valve portion and the pin portion that contacts the valve seat surface on the nozzle body side so that the other end opens to the tip end surface. A helical groove is provided on an outer peripheral surface of a portion of the nozzle main body that is viewed in the fuel reservoir. ".

【0005】また、本発明の請求項2は「ノズル本体内
に収納したニードル弁体にピン部を一体的に設け、この
ピン部を、前記ノズル本体にその先端面に開口するよう
に穿設した噴出孔内に挿入して成る燃料噴射ノズルにお
いて、前記ノズル本体に、複数個の副噴出孔を、当該副
噴出孔の一端が前記ニードル弁体のうちノズル本体側の
弁座面に接当する弁部と前記ピン部との間の部分に他端
が前記先端面に各々に開口するように穿設する一方、前
記各副噴出孔を、当該各副噴出孔からの燃料が軸線方向
から見て前記噴出孔に対して接線方向に噴出するように
構成する。」と言う構成にした。
According to a second aspect of the present invention, a pin portion is provided integrally with a needle valve body housed in a nozzle body, and the pin portion is bored in the nozzle body so as to open at a tip end surface thereof. A plurality of sub-injection holes, one end of which is in contact with the valve seat surface of the needle valve body on the nozzle body side in the nozzle body. The other end is bored in the portion between the valve portion and the pin portion so that the other end is opened at the tip end surface, while the fuel from each of the sub-ejection holes is axially When viewed from above, the nozzle is configured to be ejected tangentially to the ejection hole. "

【0006】[0006]

【発明の作用・効果】前記「請求項1」の構成におい
て、ノズル本体における燃料溜室内に供給された燃料
は、その圧力でニードル弁体を押し上げながら噴出孔か
ら中空の円錐状に噴出すると同時に、各副噴出孔からも
噴出することになる。このとき前記燃料溜室内から噴出
孔及び各副噴出孔に向かって流れる燃料には、前記ニー
ドル弁体のうち前記燃料溜室内の部分に設けた螺旋溝に
より旋回流が付与されることになり、この旋回流によ
り、前記噴出孔から燃料が噴出するときの円錐角度を広
げることができると共に、この中空の円錐状に対して旋
回運動を付与することができるから、燃料の微細化と広
い領域への分散とを図ることができる一方、前記各副噴
出孔から噴出する燃料にも、前記旋回流の影響が残存し
ているから、各副噴出孔から噴出する燃料を微細化する
ことができると共に広い領域に分散することができる。
According to the first aspect of the present invention, the fuel supplied into the fuel reservoir in the nozzle body is ejected from the ejection hole into a hollow conical shape while pushing up the needle valve body under the pressure. Therefore, the fuel is also ejected from each sub-ejection hole. At this time, the fuel flowing from the fuel reservoir toward the ejection hole and each of the sub-ejection holes is provided with a swirling flow by a spiral groove provided in a portion of the needle valve body in the fuel reservoir, By this swirling flow, the cone angle when fuel is ejected from the ejection hole can be widened, and a swirling motion can be imparted to the hollow cone, so that the fuel can be miniaturized and a wide area can be applied. On the other hand, since the influence of the swirl flow still remains on the fuel ejected from each of the sub-ejection holes, the fuel ejected from each of the sub-ejection holes can be miniaturized. It can be distributed over a wide area.

【0007】その結果、燃料噴射ノズルから噴射される
燃料の微細化と広い領域への分散とを大幅に向上できる
から、排気ガス中におけるHC等の未燃焼成分を確実に
低減できると言う効果を有する。また、前記「請求項
2」のように構成することにより、各副噴出孔からの燃
料が、噴出孔に対して接線の方向に噴出し、換言する
と、各副噴出孔から噴出される燃料に、渦巻き又はスパ
イラルの運動を付与することができて、各副噴出孔から
噴出する燃料の微細化及び広い領域への分散を更に向上
できるから、前記と略同等の効果を有する。
[0007] As a result, the fineness of the fuel injected from the fuel injection nozzle and the dispersion over a wide area can be greatly improved, so that unburned components such as HC in the exhaust gas can be surely reduced. Have. Further, by configuring as in the above “Claim 2”, the fuel from each sub-injection hole is ejected in a direction tangential to the ejection hole, in other words, the fuel ejected from each of the sub-injection holes. Since a spiral or spiral motion can be imparted, and the fuel jetted from each sub jet hole can be further miniaturized and dispersed over a wide area, the same effects as described above can be obtained.

【0008】[0008]

【発明の実施の形態】以下、本発明の実施の形態を、図
面について説明する。図1〜図3は、第1の実施形態を
示し、この図において符号1は、ノズル本体を示し、こ
のノズル本体1内には、その先端面2に開口するように
穿設した噴出孔3を開閉するニードル弁体4と、このニ
ードル弁体4をその下端の弁部5がノズル本体1側の弁
座面6に常時接当するように付勢するノズルばね7と、
前記弁座面6の箇所に燃料噴射ポンプ(図示せず)から
の圧力燃料が通路8を介して導入される燃料溜室9とを
備えている。
Embodiments of the present invention will be described below with reference to the drawings. 1 to 3 show a first embodiment, in which reference numeral 1 denotes a nozzle main body, and an ejection hole 3 formed in the nozzle main body 1 so as to open to a front end surface 2 thereof. A valve spring 4 for urging the needle valve 4 so that the valve portion 5 at the lower end thereof always contacts the valve seat surface 6 on the nozzle body 1 side;
A fuel reservoir 9 into which pressure fuel from a fuel injection pump (not shown) is introduced through a passage 8 is provided at the valve seat surface 6.

【0009】また、前記ニードル弁体4は、前記噴出孔
3内に挿入されるピン部10を一体的に備え、前記燃料
溜室9内に供給された燃料が、その圧力でニードル弁体
4をばね7に抗して押し上げながら噴出孔3から中空の
円錐状になって噴出するように構成されている。そし
て、前記ノズル本体1に、複数個の副噴出孔11を、当
該副噴出孔11の一端が前記ニードル弁体4のうちノズ
ル本体側の弁座面6に接当する弁部5と前記ピン部10
との間の部分に、他端が前記先端面2に各々に開口する
ように穿設する。
Further, the needle valve element 4 is integrally provided with a pin portion 10 inserted into the ejection hole 3, and the fuel supplied into the fuel storage chamber 9 is supplied to the needle valve element 4 by the pressure. Is pressed out against the spring 7 and is ejected from the ejection hole 3 in a hollow conical shape. The nozzle body 1 is provided with a plurality of sub-injection holes 11, the valve portion 5 having one end of the sub-injection hole 11 abutting on the valve seat surface 6 of the needle valve body 4 on the nozzle body side, and the pin. Part 10
And the other end is opened in the front end face 2 so as to open each.

【0010】更に、前記ニードル弁4のうち前記ノズル
本体1に設けられている燃料溜室9内にのぞむ部分12
における外周面に、螺旋溝13を設けるのである。この
構成において、ノズル本体1における燃料溜室9内に供
給された燃料は、その圧力でニードル弁体4を押し上げ
ながら噴出孔3から中空の円錐状になって噴出すると同
時に、各副噴出孔11からも噴出することになる。
Further, a portion 12 of the needle valve 4 which is viewed in a fuel reservoir 9 provided in the nozzle body 1
Is provided with a spiral groove 13 on the outer peripheral surface. In this configuration, the fuel supplied into the fuel reservoir 9 in the nozzle body 1 is ejected in a hollow conical shape from the ejection hole 3 while pushing up the needle valve body 4 with the pressure, and at the same time, the fuel is supplied to each of the sub-ejection holes 11. Will also erupt.

【0011】このとき前記燃料溜室9内から噴出孔3及
び各副噴出孔11に向かって流れる燃料には、前記ニー
ドル弁体4のうち前記燃料溜室9内の部分12に設けた
螺旋溝13により旋回流が付与されることになり、この
旋回流により、前記噴出孔3から燃料が噴出するときの
円錐角度を広げることができると共に、この中空の円錐
状の燃料に対して旋回運動を付与することができるか
ら、燃料の微細化と広い領域への分散とを図ることがで
きる一方、前記各副噴出孔11から噴出する燃料にも、
前記旋回流の影響が残存しているから、各副噴出孔11
から噴出する燃料を微細化することができると共に広い
領域に分散することができるのである。
At this time, the fuel flowing from the inside of the fuel reservoir 9 toward the ejection hole 3 and each of the sub-ejection holes 11 is provided with a spiral groove provided in a portion 12 of the needle valve body 4 in the fuel reservoir 9. A swirl flow is given by the fuel flow 13, and by this swirl flow, the cone angle when fuel is ejected from the ejection hole 3 can be widened, and a swirling motion is performed on the hollow conical fuel. Since it is possible to provide the fuel, it is possible to reduce the size of the fuel and to disperse the fuel in a wide area.
Since the influence of the swirling flow remains, each sub-jet hole 11
The fuel ejected from the fuel can be miniaturized and dispersed over a wide area.

【0012】この場合において、図示したように、燃料
溜室9の内周面を、ノズル本体4のうち螺旋溝13を設
けた部分12の外周面に近接するように構成することに
より、旋回流を更に強くすることができるのであり、ま
た、前記各副噴出孔11における長さ寸法Lを、当該副
噴出孔11の内径Dの5倍以下にすることにより、各副
噴出孔11から噴出される燃料に、前記旋回流の影響が
より強く残存して、各副噴出孔11から噴出される燃料
に、図3に矢印Aで示すように、渦巻き又はスパイラル
の運動を付与することができるから、燃料の微細化と広
い領域への分散とを更に向上できるのである。
In this case, as shown in the drawing, the inner peripheral surface of the fuel storage chamber 9 is configured to be close to the outer peripheral surface of the portion 12 of the nozzle body 4 where the spiral groove 13 is provided, so that the swirling flow is achieved. Can be further strengthened, and the length L of each sub-ejection hole 11 is set to be 5 times or less the inner diameter D of the sub-ejection hole 11, so that the jetting from each sub-ejection hole 11 is performed. Since the influence of the swirling flow remains more strongly on the fuel that flows, the spiral or spiral motion can be imparted to the fuel ejected from each sub-ejection hole 11 as shown by the arrow A in FIG. In addition, it is possible to further improve the miniaturization and dispersion of the fuel over a wide area.

【0013】次に、図4及び図5は、第2の実施形態を
示す。この第2の実施形態は、各副噴出孔11を、当該
各副噴出孔11からの燃料が軸線方向から見て前記噴出
孔3に対して矢印Bで示すように接線方向に噴出するよ
うに構成した点を除き、その他の構成は前記第1の実施
形態と同じである。このように、各副噴出孔11を、当
該各副噴出孔11からの燃料が軸線方向から見て前記噴
出孔3に対して矢印Bで示すように接線方向に噴出する
ように構成したことにより、各副噴出孔11からの燃料
が、噴出孔3に対して接線の方向に噴出し、換言する
と、各副噴出孔11から噴出される燃料に、渦巻き又は
スパイラルの運動を付与することができるから、燃料の
微細化及び広い領域への分散を更に向上できるのであ
る。
Next, FIGS. 4 and 5 show a second embodiment. In the second embodiment, the fuel from each of the sub-ejection holes 11 is ejected in a tangential direction to the orifice 3 as shown by an arrow B when viewed from the axial direction. Except for the configuration, the other configuration is the same as that of the first embodiment. As described above, each sub-injection hole 11 is configured so that fuel from each sub-injection hole 11 is ejected in a tangential direction to the above-described injection hole 3 as shown by an arrow B when viewed from the axial direction. The fuel from each sub-injection hole 11 is ejected in a direction tangential to the ejection hole 3, in other words, the fuel ejected from each of the sub-injection holes 11 can be imparted with a spiral or spiral motion. Therefore, it is possible to further improve the miniaturization and dispersion of the fuel over a wide area.

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

【図1】本発明の第1の実施形態を示す縦断正面図であ
る。
FIG. 1 is a longitudinal sectional front view showing a first embodiment of the present invention.

【図2】図1の要部拡大図である。FIG. 2 is an enlarged view of a main part of FIG.

【図3】図2の底面図である。FIG. 3 is a bottom view of FIG. 2;

【図4】本発明の第2の実施形態を示す要部拡大断面図
である。
FIG. 4 is an enlarged sectional view of a main part showing a second embodiment of the present invention.

【図5】図4の底面図である。FIG. 5 is a bottom view of FIG. 4;

【符号の説明】[Explanation of symbols]

1 ノズル本体 2 先端面 3 噴出孔 4 ニードル弁体 5 弁部 6 弁座面 9 燃料溜室 10 ピン部 11 副噴出孔 12 燃料溜室内にのぞむ部分 13 螺旋溝 DESCRIPTION OF SYMBOLS 1 Nozzle main body 2 Tip surface 3 Injection hole 4 Needle valve element 5 Valve portion 6 Valve seat surface 9 Fuel reservoir 10 Pin portion 11 Sub-injection hole 12 Part to be viewed in fuel reservoir 13 Spiral groove

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】ノズル本体内に収納したニードル弁体にピ
ン部を一体的に設け、このピン部を、前記ノズル本体に
その先端面に開口するように穿設した噴出孔内に挿入し
て成る燃料噴射ノズルにおいて、 前記ノズル本体に、複数個の副噴出孔を、当該副噴出孔
の一端が前記ニードル弁体のうちノズル本体側の弁座面
に接当する弁部と前記ピン部との間の部分に他端が前記
先端面に各々に開口するように穿設する一方、前記ニー
ドル弁のうち前記ノズル本体に設けられている燃料溜室
内にのぞむ部分における外周面に、螺旋溝を設けたこと
を特徴とするディーゼル機関用燃料噴射ノズル。
1. A pin portion is integrally provided on a needle valve body housed in a nozzle body, and the pin portion is inserted into an ejection hole formed in the nozzle body so as to open at a tip end surface thereof. In the fuel injection nozzle, a plurality of sub-injection holes are provided in the nozzle body, and one end of the sub-injection hole contacts the valve seat surface of the needle valve body on the nozzle body side and the pin portion. A spiral groove is formed on the outer peripheral surface of a portion of the needle valve that is viewed in a fuel reservoir provided in the nozzle body, while the other end is bored in the portion between the two so that the other end opens to the distal end surface. A fuel injection nozzle for a diesel engine, wherein the nozzle is provided.
【請求項2】ノズル本体内に収納したニードル弁体にピ
ン部を一体的に設け、このピン部を、前記ノズル本体に
その先端面に開口するように穿設した噴出孔内に挿入し
て成る燃料噴射ノズルにおいて、 前記ノズル本体に、複数個の副噴出孔を、当該副噴出孔
の一端が前記ニードル弁体のうちノズル本体側の弁座面
に接当する弁部と前記ピン部との間の部分に他端が前記
先端面に各々に開口するように穿設する一方、前記各副
噴出孔を、当該各副噴出孔からの燃料が軸線方向から見
て前記噴出孔に対して接線方向に噴出するように構成し
たことを特徴とするディーゼル機関用燃料噴射ノズル。
2. A pin portion is integrally provided on a needle valve body housed in a nozzle main body, and the pin portion is inserted into an ejection hole formed in the nozzle main body so as to open at a tip end surface thereof. In the fuel injection nozzle, a plurality of sub-injection holes are provided in the nozzle body, and one end of the sub-injection hole contacts the valve seat surface of the needle valve body on the nozzle body side and the pin portion. While the other end is drilled in the portion between them so that the other end opens to the front end face, each of the sub-ejection holes is formed such that the fuel from each of the sub-ejection holes is viewed from the axial direction with respect to the above-mentioned emission hole. A fuel injection nozzle for a diesel engine, which is configured to jet in a tangential direction.
JP33419496A 1996-12-13 1996-12-13 Fuel injection nozzle for diesel engine Pending JPH10176630A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP33419496A JPH10176630A (en) 1996-12-13 1996-12-13 Fuel injection nozzle for diesel engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP33419496A JPH10176630A (en) 1996-12-13 1996-12-13 Fuel injection nozzle for diesel engine

Publications (1)

Publication Number Publication Date
JPH10176630A true JPH10176630A (en) 1998-06-30

Family

ID=18274604

Family Applications (1)

Application Number Title Priority Date Filing Date
JP33419496A Pending JPH10176630A (en) 1996-12-13 1996-12-13 Fuel injection nozzle for diesel engine

Country Status (1)

Country Link
JP (1) JPH10176630A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1213474A3 (en) * 2000-10-19 2004-01-07 Robert Bosch Gmbh Fuel injection valve
FR2860558A1 (en) * 2003-10-06 2005-04-08 Renault Sas Fuel injector for use in e.g. diesel engine, has nozzle including two outer orifices that extend at distance from central axis of nozzle and having outer opening with circular shape which extends from axis
US20160177905A1 (en) * 2013-08-19 2016-06-23 Kangmei Wang Centrifugal Conical-Spray Nozzle
CN111905937A (en) * 2020-07-17 2020-11-10 陕西航空电气有限责任公司 Oil nozzle

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1213474A3 (en) * 2000-10-19 2004-01-07 Robert Bosch Gmbh Fuel injection valve
FR2860558A1 (en) * 2003-10-06 2005-04-08 Renault Sas Fuel injector for use in e.g. diesel engine, has nozzle including two outer orifices that extend at distance from central axis of nozzle and having outer opening with circular shape which extends from axis
US20160177905A1 (en) * 2013-08-19 2016-06-23 Kangmei Wang Centrifugal Conical-Spray Nozzle
US10006427B2 (en) * 2013-08-19 2018-06-26 Kangmei Wang Centrifugal conical-spray nozzle
CN111905937A (en) * 2020-07-17 2020-11-10 陕西航空电气有限责任公司 Oil nozzle

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