JPH0451664B2 - - Google Patents

Info

Publication number
JPH0451664B2
JPH0451664B2 JP59025282A JP2528284A JPH0451664B2 JP H0451664 B2 JPH0451664 B2 JP H0451664B2 JP 59025282 A JP59025282 A JP 59025282A JP 2528284 A JP2528284 A JP 2528284A JP H0451664 B2 JPH0451664 B2 JP H0451664B2
Authority
JP
Japan
Prior art keywords
heating element
combustion chamber
injection
fuel
nozzle
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 - Lifetime
Application number
JP59025282A
Other languages
Japanese (ja)
Other versions
JPS59162358A (en
Inventor
Yoozefu Esupaa Furiidoritsuhi
Furai Toomasu
Komarotsufu Iuan
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.)
Robert Bosch GmbH
Original Assignee
Robert Bosch GmbH
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 Robert Bosch GmbH filed Critical Robert Bosch GmbH
Publication of JPS59162358A publication Critical patent/JPS59162358A/en
Publication of JPH0451664B2 publication Critical patent/JPH0451664B2/ja
Granted 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
    • F02M53/00Fuel-injection apparatus characterised by having heating, cooling or thermally-insulating means
    • F02M53/04Injectors with heating, cooling, or thermally-insulating means
    • F02M53/06Injectors with heating, cooling, or thermally-insulating means with fuel-heating means, e.g. for vaporising
    • 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
    • F02M57/00Fuel-injectors combined or associated with other devices
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B3/00Engines characterised by air compression and subsequent fuel addition
    • F02B3/06Engines 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)

Description

【発明の詳細な説明】 イ 技術分野 本発明は、燃焼室に燃料を噴射する装置、更に
詳細には噴射ノズルと、この噴射ノズルの燃焼室
面側に配置された発熱体を備えた燃焼室、特にデ
イーゼルエンジンの燃焼室に燃料を噴射する装置
に関する。
Detailed Description of the Invention (a) Technical Field The present invention relates to a device for injecting fuel into a combustion chamber, and more particularly to a combustion chamber equipped with an injection nozzle and a heating element disposed on the side of the combustion chamber of the injection nozzle. In particular, it relates to a device for injecting fuel into the combustion chamber of a diesel engine.

ロ 従来技術 このような種類の従来の装置では始動を助ける
ためにヒータープラグが組み込まれている。これ
らの部品によつて噴射領域には加熱、気化、並び
に燃料の一部に対する点火に対する好ましい条件
が得られ、それにより続いて全体の噴射燃料に対
して点火が行なわれる。このようなヒータープラ
グ及びヒーターピンは特別な部品であり、それを
燃焼室に組み込むことは敏感な流量特性に影響を
与えることになる。エネルギーの枯渇化に伴い燃
料がアルコールや植物油に代替されることが多く
なつていることを考えると、燃料を噴射する場合
混合気の形成や点火は更に難かしいものとなる。
B. Prior Art Conventional equipment of this type incorporates a heater plug to aid in starting. These components provide the injection region with favorable conditions for heating, vaporization and ignition of a portion of the fuel, which subsequently ignites the entire injected fuel. Such heater plugs and heater pins are special components, and their incorporation into the combustion chamber will affect sensitive flow characteristics. Considering that alcohol and vegetable oil are increasingly being substituted for fuel as energy becomes increasingly scarce, forming and igniting a mixture becomes even more difficult when fuel is injected.

更に噴射ノズルの後に点火装置を備えた混合室
が設けられている装置が知られている(例えばド
イツ特許公開公報第2715943号)。同装置の場合燃
焼室の壁面は加熱され、そこで燃焼が開始される
ようになつている。混合室は燃焼壁にねじ込まれ
るブツシングとして形成されており、そこに噴射
ノズルが支持されている。しかしこのような装置
は非常に高価であり使用する燃料並びにエンジン
の特性に注意深く適合させなければならないとい
う欠点がある。
Furthermore, devices are known in which a mixing chamber with an ignition device is provided after the injection nozzle (eg DE 27 15 943). In this device, the walls of the combustion chamber are heated, and combustion begins there. The mixing chamber is designed as a bushing screwed into the combustion wall, in which the injection nozzle is supported. However, such devices have the disadvantage that they are very expensive and must be carefully adapted to the fuel used and the characteristics of the engine.

一方噴射ノズルから噴射される燃料に対して方
向を変えず、又何らか変更も加えずに発熱体に接
触することなく燃料を通過させるような装置が知
られている。このような発熱体では燃料の点火性
を良くするために噴射の初めに通路にある空気を
燃焼室のものよりも温度を高くすることによつて
点火性を良くしている。その場合点火時噴射効果
により他の空気が燃焼室から発熱体の通路に吸入
され、そこで加熱される。加熱された空気に渦が
起こることにより燃料と混合され点火が促進され
ている。これは始動時や高回転時あるいは回転数
が少ない場合のような噴射圧が低い時に噴霧化が
悪くなるような駆動領域においては特に重要とな
る。いずれにしても噴射燃料の周辺領域において
点火に必要な噴霧化された燃料を予め形成してお
かなければならない。しかし従来では始動時や高
回転時、このような発熱体の機能では媒煙を減少
させることができないという欠点がある。
On the other hand, there is known a device that allows the fuel injected from an injection nozzle to pass through without changing its direction or making any changes and without coming into contact with a heating element. In such a heating element, the ignitability of the fuel is improved by making the temperature of the air in the passage higher than that of the combustion chamber at the beginning of injection. In this case, due to the ignition injection effect, additional air is drawn from the combustion chamber into the passage of the heating element and heated there. The swirling of the heated air mixes it with the fuel, promoting ignition. This is particularly important in drive ranges where atomization deteriorates when the injection pressure is low, such as during startup, high rotation, or low rotation speed. In any case, the atomized fuel required for ignition must be formed beforehand in the area surrounding the injected fuel. However, the conventional method has a drawback in that the function of the heating element cannot reduce smoke during startup or high rotation.

ハ 目的 従つて本発明はこのような従来の欠点を解消す
るために成されたもので、通常の噴射ノズルに対
する変形がわずかですみ、又エンジンや燃料の条
件に比較的簡単に合わせることが可能な燃焼室に
燃料を噴射する装置を提供することを目的とす
る。
C. Purpose Therefore, the present invention has been made in order to eliminate these conventional drawbacks, and requires only slight deformation of a normal injection nozzle, and can be relatively easily adapted to engine and fuel conditions. The purpose of the present invention is to provide a device for injecting fuel into a combustion chamber.

このような目的を達成するために、本発明で
は、噴射ノズルと、この噴射ノズルの後方で噴射
ノズルの燃焼室側に配置された発熱体とを備え、
前記発熱体には噴射燃料流を通過させその一部を
気化させる発熱壁で囲まれた通路が形成される、
燃焼室、特にデイーゼルエンジンの燃焼室に燃料
を噴射する装置において、前記通路を囲む発熱体
の内壁のノズル軸線に対する形状並びに位置と、
噴射ノズルから出る燃料流の円錐角ないし噴射角
を定めるパラメータとは、噴射燃料流の少なくと
も一部が内燃機関の所定駆動領域で発熱体の発熱
体内壁に当り気化するように設定され、また前記
発熱体がセラミツクスからなり、このセラミツク
スの面に積層される金属膜を形成する発熱素子を
担持する構成を採用した。
In order to achieve such an object, the present invention includes an injection nozzle and a heating element disposed behind the injection nozzle on the combustion chamber side of the injection nozzle,
The heating element is formed with a passage surrounded by a heating wall through which the injected fuel flow passes and partially vaporizes the injected fuel flow.
In a device for injecting fuel into a combustion chamber, particularly a combustion chamber of a diesel engine, the shape and position of the inner wall of the heating element surrounding the passage with respect to the nozzle axis;
The parameter that determines the cone angle or injection angle of the fuel flow coming out of the injection nozzle is set so that at least a part of the injected fuel flow hits the inner wall of the heating element of the heating element in a predetermined driving region of the internal combustion engine and is vaporized. A configuration was adopted in which the heating element is made of ceramics and supports a heating element formed by a metal film laminated on the surface of the ceramics.

ニ 実施例 以下図面に示す実施例に従い本発明を詳細に説
明する。
D. Examples The present invention will be described in detail below according to examples shown in the drawings.

第1図にはノズル体10を備えた噴射ノズルが
図示されている。このノズル体10には燃料の流
れに抗して開放する弁ニードル12が摺動自在に
取り付けられている。この弁ニードルは弁座14
によつて規制されており、この弁座から円筒状の
噴射開口部16が続き、弁ニードル12に形成さ
れた絞り軸針18がこの噴射開口部16に嵌入す
る。この絞り軸針18に噴射軸針20が続き、そ
れによつて図示されたように燃料は角度がaの円
錐形状22となつて噴射される。ノズル体10は
ナツト24によりノズル保持体(図示せず)に固
定され、又これらの部分によつて構成されるユニ
ツトがエンジンの筐体(図示せず)に取りつけら
れる。
FIG. 1 shows an injection nozzle with a nozzle body 10. In FIG. A valve needle 12 that opens against the flow of fuel is slidably attached to the nozzle body 10. This valve needle is the valve seat 14
A cylindrical injection opening 16 follows from this valve seat, into which a throttle axis needle 18 formed in the valve needle 12 fits. This throttle shaft needle 18 is followed by an injection shaft needle 20, by means of which the fuel is injected in a conical shape 22 at an angle a, as shown. The nozzle body 10 is fixed to a nozzle holder (not shown) by a nut 24, and a unit constituted by these parts is attached to an engine casing (not shown).

噴射ノズルの下流にセラミツク製の発熱体30
が配置される。この発熱体はその内部に通路32
を有し、そこを通つて噴射開口部16から出る燃
料が噴射され燃焼室に導かれる。発熱体30はノ
ズル体10の径と異なる段差部分34と一部重な
り合い、後述する中間部材を介しナツト24によ
り締め付けられノズル体10の肩部36に押し当
てられる。ノズル体の段差部分34の下流で発熱
体30の内部には通路32の円筒状の円筒部38
とそれに続く円錐状に拡大する円錐部40が形成
される。
Ceramic heating element 30 downstream of the injection nozzle
is placed. This heating element has a passage 32 inside it.
, through which the fuel exiting the injection opening 16 is injected and guided into the combustion chamber. The heating element 30 partially overlaps a step portion 34 having a different diameter from the nozzle body 10, and is pressed against a shoulder portion 36 of the nozzle body 10 by being tightened by a nut 24 via an intermediate member to be described later. A cylindrical cylindrical portion 38 of the passage 32 is provided inside the heating element 30 downstream of the stepped portion 34 of the nozzle body.
A conical portion 40 that expands into a conical shape is formed.

通路32の円錐部40の内壁には成膜ないし蒸
着により形成された金属層として構成される発熱
素子42が取り付けられる。細片として形成され
た発熱素子42の端部44と46は発熱体30の
円筒状内壁の径方向に対抗する壁面に沿つて上方
に延び表面48に導かれる。発熱体30の表面4
8には円環セクター形状の2つの金属接点層5
0,52が形成され、それがそれぞれが発熱素子
42の各端部44,46と接続される。接点層5
0,52の互いに対抗した端部間で発熱体30に
は径方向に対抗する2つの隆起部54が形成さ
れ、その高さは接点板56,58の厚さに対応す
る。これらの隆起部54は接点層50,52を互
いに分離し絶縁する働きをする。
A heating element 42 configured as a metal layer formed by film formation or vapor deposition is attached to the inner wall of the conical portion 40 of the passage 32. The ends 44 and 46 of the heating element 42, which is formed as strips, extend upwardly along the radially opposite wall surface of the cylindrical inner wall of the heating element 30 and are guided to a surface 48. Surface 4 of heating element 30
8 includes two metal contact layers 5 in an annular sector shape.
0 and 52 are formed, which are connected to respective ends 44 and 46 of heating element 42, respectively. Contact layer 5
Between the opposing ends of the heating element 30, two radially opposing ridges 54 are formed, the height of which corresponds to the thickness of the contact plates 56, 58. These ridges 54 serve to separate and insulate contact layers 50, 52 from each other.

接点層50,52上に同様に円環セクター状の
接点板56,58が重ねられ、これらの接点板は
円環状の絶縁板60の一面に固定される。尚、上
記隆起部54は、円環セクター状の接点板56,
58も同様に互いに分離、絶縁して位置決めする
機能を有するとともに、このような隆起部を設け
ることにより特に接点層50,52に対して接点
板56,58を正確に位置決めして取り付けるの
が容易になる。絶縁板60は2つの金属スリーブ
62,64を有し、これらのスリーブは接点板5
6,58並びにノズル体10と絶縁されている接
続線66,68と接続される。絶縁板60とノズ
ル体10の肩部36間には皿状のバネ70が配置
され、このバネ70はナツト24によつて発熱体
30に作用する締め付け力を所定の値に制限しそ
れによつて発熱体30の破壊を防止する。同時に
又このバネによつて接触が確実になり、発熱素子
42への電流を確実に供給させることが可能にな
る。
Similarly, contact plates 56 and 58 in the form of annular sectors are superposed on the contact layers 50 and 52, and these contact plates are fixed to one side of an insulating plate 60 in the form of an annular ring. Note that the raised portion 54 has an annular sector-shaped contact plate 56,
Similarly, the contact plates 56 and 58 have the function of separating and insulating each other and positioning them, and by providing such a raised portion, it is easy to accurately position and attach the contact plates 56 and 58 to the contact layers 50 and 52. become. The insulating plate 60 has two metal sleeves 62, 64, which are connected to the contact plate 5.
6 and 58 as well as connecting wires 66 and 68 which are insulated from the nozzle body 10. A disk-shaped spring 70 is disposed between the insulating plate 60 and the shoulder 36 of the nozzle body 10, and this spring 70 limits the tightening force applied to the heating element 30 by the nut 24 to a predetermined value. This prevents the heating element 30 from being destroyed. At the same time, this spring also ensures a secure contact and ensures that current is supplied to the heating element 42.

通路32の円錐部40は円錐角bを有し、この
角度は噴射燃料流22の円錐角aよりも小さくな
るように選ばれる。円錐部40は軸方向にみてノ
ズル体10の噴射側端面に対抗して配置されてお
り、噴射燃料流22は内燃機関の全ての駆動領域
において円錐部40の発熱壁に当たり、そこで渦
状にされ、一部が蒸発ないし気化される。この過
程で第1図に矢印で図示されたように燃焼空気も
気化された燃料に達する。このようにして発熱体
30からはかなりの温度に加熱されほぼ全ての領
域で気化された燃料と空気の混合気が得られ、そ
れが燃焼室において急激にしかも完全に点火され
燃焼される。
The conical portion 40 of the passage 32 has a cone angle b, which angle is chosen to be smaller than the cone angle a of the injected fuel stream 22. The conical part 40 is arranged opposite to the injection end face of the nozzle body 10 when viewed in the axial direction, and the injected fuel flow 22 impinges on the heat-generating wall of the conical part 40 in all drive regions of the internal combustion engine and is swirled there. Some of it evaporates or vaporizes. During this process, the combustion air also reaches the vaporized fuel, as indicated by the arrows in FIG. In this way, a mixture of fuel and air is obtained from the heating element 30, which is heated to a considerable temperature and vaporized in almost all areas, and is rapidly and completely ignited and combusted in the combustion chamber.

噴射燃料流22の噴射角ないし円錐角aと発熱
体30の形状並びに寸法を相互に設定することに
より、又場合によつて発熱体30の温度の大きさ
並びに温度の空間的な分布を設定することにより
それぞれの燃料やエンジンに合わせて最適に燃料
を噴射させることが可能になる。
By mutually setting the injection angle or cone angle a of the injected fuel stream 22 and the shape and dimensions of the heating element 30, the magnitude of the temperature of the heating element 30 as well as the spatial distribution of the temperature can be set, as the case may be. This makes it possible to optimally inject fuel according to each fuel and engine.

第2図に図示された実施例では噴射ノズルとし
ていわゆる穿孔ノズルが用いられている。その場
合内側に向つて開く弁ニードル72によつて燃料
は底穴部74に導かれ、そこから噴射開口部76
を介して噴射燃料流78として噴射されセラミツ
ク製の発熱体82の円錐状に拡大する円錐部80
に達しそこで発熱した壁面に当たる。各噴射燃料
流78の噴射角cは円錐部80の円錐角bの半分
よりも大きくされるので、第1図の実施例と同様
な効果が得られる。
In the embodiment shown in FIG. 2, a so-called perforated nozzle is used as the injection nozzle. By means of an inwardly opening valve needle 72, the fuel is then led into a bottom bore 74 and from there into an injection opening 76.
The conical part 80 of the heating element 82 made of ceramic is injected as an injected fuel stream 78 through the conical part 80.
It reaches the point where it hits the wall which generates heat. Since the injection angle c of each injected fuel stream 78 is made larger than half the cone angle b of the cone section 80, an effect similar to that of the embodiment of FIG. 1 is obtained.

第3図の実施例の場合には円錐部80の円錐角
bは各噴射燃料流78の噴射角cの2倍よりも大
きくされる。特にこの実施例の場合円錐部80は
噴射開口部76の排出面に対して軸方向に延びる
に従い外側にずらされているので、噴射燃料流7
8は円錐部80の加熱された壁面の入口領域84
に当たることになる。そこで燃料はコアンダ効果
(coanda効果)により外方に方向が変えられほぼ
円錐部80の壁面に平行して噴射されることにな
る。
In the embodiment of FIG. 3, the cone angle b of the cone 80 is greater than twice the injection angle c of each injected fuel stream 78. Particularly in this embodiment, the cone 80 is offset outwardly in its axial extension with respect to the discharge surface of the injection opening 76, so that the injected fuel flow 7
8 is the inlet region 84 of the heated wall of the conical section 80;
It will hit. The fuel is then redirected outward by the Coanda effect and is injected approximately parallel to the wall of the conical portion 80.

第4図の実施例の場合には噴射開口部76は中
央の底面の穴86から正接方向に出るので、各噴
射燃料流78には旋回が生じ、それによつて燃料
が発熱体の発熱面に均等に分布し大部分の燃料成
分が気化され空気と良く混合されるという好まし
い効果が得られる。
In the embodiment of FIG. 4, the injection openings 76 emerge tangentially from the central bottom hole 86, so that a swirl occurs in each injected fuel stream 78, thereby causing the fuel to reach the heating surface of the heating element. The desirable effect is that most of the fuel components are evenly distributed and vaporized and mixed well with the air.

このようにして本発明によれば通常の噴射ノズ
ルの筐体に対する変形が少なくてすみ又異なるエ
ンジン条件並びに燃料に比較的容易に適合させる
ことができるという利点が得られる。発熱体が噴
射ノズルに固定されるかあるいはこれと一体に形
成される。又発熱体が噴射ノズルとシリンダヘツ
ドの肩部間に固定するかあるいは直接シリンダヘ
ツドに固定することができる。
The invention thus provides the advantage that it requires less modification to the housing of a conventional injection nozzle and can be relatively easily adapted to different engine conditions and fuels. A heating element is fixed to or formed integrally with the injection nozzle. The heating element can also be fixed between the injection nozzle and the shoulder of the cylinder head or directly on the cylinder head.

又本発明では内燃機関の全ての駆動領域におい
て燃料流は噴射の周辺領域だけでなく全体の燃料
流の大部分が壁面に当たりそこで気化されること
によつて更に向上されることになる。それによつ
て始動や高回転時のような駆動領域においても媒
煙の発生を顕著に減少させることができると同時
に、発熱体によつて全ての駆動条件において燃料
を点火させることが可能になる。
Furthermore, in the present invention, the fuel flow in all drive regions of the internal combustion engine is further improved in that not only the peripheral region of the injection but also a large part of the entire fuel flow impinges on the wall surface and is vaporized there. This makes it possible to significantly reduce the generation of smoke even in drive ranges such as during startup and high rotation, and at the same time allows the heating element to ignite the fuel under all drive conditions.

又本発明の実施例ではいわゆるコアンダ効果が
用いられており、それによつて噴射燃料流は発熱
体の円錐部の終端領域に導き出されることにな
る。
The embodiments of the invention also use the so-called Coanda effect, whereby the injected fuel flow is guided into the end region of the cone of the heating element.

又本発明ではノズルとして軸針型ノズル、穿孔
型ノズル、又外方に開く弁ニードルをもつたノズ
ルに対しても適用することができる。
Further, the present invention can be applied to a shaft needle type nozzle, a perforated type nozzle, and a nozzle having a valve needle that opens outward.

又本発明の実施例では噴射ノズルによつて排出
された燃料流に旋回が起こるような穴が噴射ノズ
ルに形成されるようになつており、それによつて
噴射燃料流の渦状態を更に大きくし気化を良好に
行なうようにすることができる。
Further, in an embodiment of the present invention, a hole is formed in the injection nozzle so that a swirl occurs in the fuel flow discharged by the injection nozzle, thereby further increasing the vortex state of the injected fuel flow. It is possible to achieve good vaporization.

又本発明では発熱体はセラミツクから構成さ
れ、発熱素子は好ましくは層状の導体路として発
熱体の内面あるいは外面に積層される。この導体
路は電流を制御することにより発熱させることが
できる。又セラミツク体に複数の加熱回路を設け
ることも可能である。それによつて発熱体の各領
域を他の領域と区別して加熱することが可能にな
り、それにより種々の加熱状態を発生させ、噴射
燃料流並びに点火の特性をそれぞれの内燃機関の
動作点に最適に調節することとが可能になる。
Further, in the present invention, the heating element is made of ceramic, and the heating element is preferably laminated as a layered conductor path on the inner or outer surface of the heating element. This conductor path can generate heat by controlling the current. It is also possible to provide a plurality of heating circuits in the ceramic body. This makes it possible to heat each region of the heating element separately from the other regions, thereby generating different heating conditions and optimizing the injection fuel flow and ignition characteristics to the operating point of the respective internal combustion engine. It becomes possible to adjust to.

更に本発明では発熱素子は発熱体の円錐状に拡
大する内面に取り付けられているので好ましい結
果が得られる。
Furthermore, in the present invention, favorable results are obtained because the heating element is attached to the conically expanding inner surface of the heating element.

ホ 効果 以上説明したように、本発明では、発熱体の内
壁のノズル軸線に対する形状並びに位置と、噴射
燃料流の円錐角ないし噴射角を定めるパラメータ
とが互いに調節されて噴射ノズルから噴射される
燃料流が発熱体の発熱体内壁に当り気化するよう
になる。また発熱体がセラミツクスからできてい
るので、耐熱性が高くなるとともに発熱体の内壁
を簡単に種々の形状に加工でき、それにより噴射
ノズルから噴射される燃料流をエンジンや燃料の
条件に合わせて効率よく発熱体の内壁に当て気化
させることができる。また発熱体に担持される発
熱素子がセラミツクスの面に積層される金属膜に
より形成されるので、この金属膜の厚さや形状並
びにその位置を種々のものに設定しやすくなり、
そそれにより任意の発熱特性を得ることができ、
噴射燃料流並びに点火特特性をそれぞれの内燃機
関の動作点に最適に調節できる、等種々の作用効
果が得られる。
Effects As explained above, in the present invention, the shape and position of the inner wall of the heating element with respect to the nozzle axis and the parameter that determines the cone angle or injection angle of the injected fuel flow are mutually adjusted so that the fuel is injected from the injection nozzle. The flow hits the inner wall of the heating element and becomes vaporized. In addition, since the heating element is made of ceramics, it has high heat resistance and the inner wall of the heating element can be easily shaped into various shapes, allowing the fuel flow injected from the injection nozzle to be adjusted to suit the engine and fuel conditions. It can be efficiently vaporized by applying it to the inner wall of the heating element. In addition, since the heating element carried by the heating element is formed by a metal film laminated on the ceramic surface, it is easy to set the thickness, shape, and position of this metal film to various values.
By doing so, it is possible to obtain arbitrary heat generation characteristics,
Various effects are obtained, such as the ability to optimally adjust the injected fuel flow as well as the ignition characteristics to the operating point of the respective internal combustion engine.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本発明の第1の実施例を示す拡大した
断面図、第2図、第3図はそれぞれ本発明の異な
る他の実施例を示した断面図、第4図は第2図実
施例の変形を示すノズルの断面に形成される流れ
の状態を示した説明図である。 10……ノズル体、12……弁ニードル、16
……噴射開口部、22……噴射燃料、24……ナ
ツト、30……発熱体、32……通路、38……
円筒部、40……円錐部、42……発熱線、5
0,52……接点層、56,58……接点板、6
0……絶縁板、66,68……接続線、70……
皿状ばね。
FIG. 1 is an enlarged sectional view showing a first embodiment of the present invention, FIGS. 2 and 3 are sectional views showing other different embodiments of the present invention, and FIG. 4 is an enlarged sectional view showing a first embodiment of the present invention. It is an explanatory view showing the state of the flow formed in the cross section of the nozzle showing the modification of the example. 10... Nozzle body, 12... Valve needle, 16
... Injection opening, 22 ... Injected fuel, 24 ... Nut, 30 ... Heating element, 32 ... Passage, 38 ...
Cylindrical part, 40...Cone part, 42...Heating wire, 5
0,52...Contact layer, 56,58...Contact plate, 6
0... Insulating plate, 66, 68... Connection wire, 70...
Disc spring.

Claims (1)

【特許請求の範囲】 1 噴射ノズルと、この噴射ノズルの後方で噴射
ノズルの燃焼室側に配置された発熱体とを備え、
前記発熱体には噴射燃料流を通過させその一部を
気化させる発熱壁で囲まれた通路が形成される、
燃焼室、特にデイーゼルエンジンの燃焼室に燃料
を噴射する装置において、前記通路を囲む発熱体
30,82の内壁のノズル軸線に対する形状並び
に位置と、噴射ノズルから出る燃料流22,78
の円錐角aないし噴射角cを定めるパラメータと
は、噴射燃料流22,78の少なくとも一部が内
燃機関の所定駆動領域で発熱体30,82の発熱
体内壁に当り気化するように設定され、また前記
発熱体30,82がセラミツクスからなり、この
セラミツクスの面に積層される金属膜を形成する
発熱素子42を担持することを特徴とする燃焼室
に燃料を噴射する装置。 2 前記発熱体30,82は燃焼室側端部に円錐
状に拡大する通路部40,80を有し、前記燃料
流22,78の少なくとも一部が前記駆動領域で
この円錐状に拡大する通路部40,80の壁面に
当たるように、前記パラメータが選択されること
を特徴とする特許請求の範囲第1項に記載の燃焼
室に燃料を噴射する装置。 3 噴射ノズルは噴射開口部を通過する噴射軸針
を備えた弁ニードルを有し、この噴射軸針を通つ
て噴射される燃料流は円錐形状となり、燃料流の
円錐角は発熱体30の円錐状に拡大する通路部4
0の円錐角bよりも大きいことを特徴とする特許
請求の範囲第2項に記載の燃焼室に燃料を噴射す
る装置。 4 噴射ノズルはノズル軸線に対して所定の角度
を有する少なくとも一つの噴射開口部76を有
し、その噴射開口部のノズル軸線に対する噴射角
度cは発熱体82の円錐状に拡大する円錐通路部
80の角度bの半分よりも大きいことを特徴とす
る特許請求の範囲第2項に記載の燃焼室に燃料を
噴射する装置。 5 噴射ノズルはノズル軸線に対して所定の角度
を有する少なくとも一つの噴射開口部を有し、そ
の噴射開口部のノズル軸線に対する噴射角度cは
発熱体の円錐通路部80の円錐角bの半分よりも
わずかに小さく、又この円錐通路部80は噴射開
口部76に対し軸方向に延びるに従い外側にずれ
ていて噴射燃料流が円錐通路部80の入口領域8
4に接するように当たることを特徴とする特許請
求の範囲第2項に記載の燃焼室に燃料を噴射する
装置。 6 噴射ノズルには噴射燃料流が旋回するような
噴射穴76が形成されることを特徴とする特許請
求の範囲第4項又は第5項に記載の燃焼室に燃料
を噴射する装置。 7 発熱素子42は発熱体30,82の円錐通路
部40,80の壁面に形成されることを特徴とす
る特許請求の範囲第1項から第6項までのいずれ
か1項に記載の燃焼室に燃料を噴射する装置。 8 発熱素子42を形成する金属被膜層の端部は
ノズル体10に面した発熱体面48に延びてお
り、発熱体30は接点板56,58、絶縁板6
0、皿状のばね70を介してノズル体10に取り
付けられることを特徴とする特許請求の範囲第7
項に記載の燃焼室に燃料を噴射する装置。 9 接点板58,58は絶縁板60に固定されて
かつ接続線66,68に接続され、この接続線は
絶縁板60並びにノズル体10を経て外部に導か
れることを特徴とする特許請求の範囲第8項に記
載の燃焼室に燃料を噴射する装置。 10 絶縁板60は円環セクター状の接点板5
6,58と接触し、又発熱体30の面には径方向
に対向する2つの隆起部54が形成され、その隆
起部の高さは接点板56,58の厚さに相当する
ことを特徴とする特許請求の範囲第9項に記載の
燃焼室に燃料を噴射する装置。
[Claims] 1. Comprising an injection nozzle and a heating element disposed behind the injection nozzle and on the combustion chamber side of the injection nozzle,
The heating element is formed with a passage surrounded by a heating wall through which the injected fuel flow passes and partially vaporizes the injected fuel flow.
In an apparatus for injecting fuel into a combustion chamber, in particular a combustion chamber of a diesel engine, the shape and position of the inner walls of the heating elements 30, 82 surrounding the passage with respect to the nozzle axis, and the fuel flow 22, 78 emerging from the injection nozzle.
The parameters that determine the cone angle a or the injection angle c are set such that at least a part of the injected fuel flow 22, 78 hits the inner wall of the heating element 30, 82 in a predetermined drive region of the internal combustion engine and is vaporized, The apparatus for injecting fuel into a combustion chamber is characterized in that the heating elements 30 and 82 are made of ceramics and support a heating element 42 forming a metal film laminated on the surface of the ceramics. 2. The heating elements 30, 82 have conically expanding passages 40, 80 at the ends on the side of the combustion chamber, and at least a portion of the fuel flows 22, 78 pass through the conically expanding passages in the driving region. 2. A device for injecting fuel into a combustion chamber according to claim 1, characterized in that the parameters are selected such that the fuel injects into the combustion chamber so as to hit the wall surfaces of the sections 40, 80. 3 The injection nozzle has a valve needle with an injection axis needle passing through the injection opening, the fuel flow injected through this injection axis needle has a conical shape, the cone angle of the fuel flow is equal to the cone of the heating element 30. The passage section 4 expands into
A device for injecting fuel into a combustion chamber according to claim 2, characterized in that the cone angle b is greater than zero. 4. The injection nozzle has at least one injection opening 76 having a predetermined angle with respect to the nozzle axis, and the injection angle c of the injection opening with respect to the nozzle axis corresponds to the conical passage portion 80 of the heating element 82 that expands conically. 3. Device for injecting fuel into a combustion chamber according to claim 2, characterized in that the angle b is greater than half of the angle b. 5 The injection nozzle has at least one injection opening having a predetermined angle with respect to the nozzle axis, and the injection angle c of the injection opening with respect to the nozzle axis is less than half of the cone angle b of the conical passage portion 80 of the heating element. is also slightly smaller and this conical passage 80 is offset outwardly in its axial extent with respect to the injection opening 76 so that the injected fuel flow is directed to the inlet area 8 of the conical passage 80.
4. The device for injecting fuel into a combustion chamber according to claim 2, wherein the fuel injects into the combustion chamber. 6. The device for injecting fuel into a combustion chamber according to claim 4 or 5, wherein the injection nozzle is formed with an injection hole 76 through which the injected fuel flow swirls. 7. The combustion chamber according to any one of claims 1 to 6, wherein the heating element 42 is formed on the wall surface of the conical passage portion 40, 80 of the heating element 30, 82. A device that injects fuel into 8 The end of the metal coating layer forming the heating element 42 extends to the heating element surface 48 facing the nozzle body 10, and the heating element 30 is connected to the contact plates 56, 58 and the insulating plate 6.
0. Claim 7, characterized in that it is attached to the nozzle body 10 via a dish-shaped spring 70.
A device for injecting fuel into the combustion chamber described in paragraph 1. 9. Claims characterized in that the contact plates 58, 58 are fixed to an insulating plate 60 and connected to connecting wires 66, 68, and the connecting wires are guided to the outside via the insulating plate 60 and the nozzle body 10. A device for injecting fuel into the combustion chamber according to item 8. 10 The insulating plate 60 is an annular sector-shaped contact plate 5
6, 58, and two radially opposing ridges 54 are formed on the surface of the heating element 30, and the height of the ridges corresponds to the thickness of the contact plates 56, 58. An apparatus for injecting fuel into a combustion chamber according to claim 9.
JP2528284A 1983-03-04 1984-02-15 Device for injecting fuel into combustion chamber Granted JPS59162358A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19833307666 DE3307666A1 (en) 1983-03-04 1983-03-04 Device for the injection of fuel into combustion chambers, especially combustion chambers of diesel engines
DE3307666.9 1983-03-04

Publications (2)

Publication Number Publication Date
JPS59162358A JPS59162358A (en) 1984-09-13
JPH0451664B2 true JPH0451664B2 (en) 1992-08-19

Family

ID=6192500

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2528284A Granted JPS59162358A (en) 1983-03-04 1984-02-15 Device for injecting fuel into combustion chamber

Country Status (2)

Country Link
JP (1) JPS59162358A (en)
DE (1) DE3307666A1 (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3502109A1 (en) * 1985-01-23 1986-07-24 Robert Bosch Gmbh, 7000 Stuttgart FUEL INJECTION NOZZLE FOR INTERNAL COMBUSTION ENGINES
DE3609749A1 (en) * 1986-03-22 1987-09-24 Bosch Gmbh Robert DEVICE FOR INJECTING FUEL IN THE COMBUSTION ROOM OF INTERNAL COMBUSTION ENGINES
DE3614226A1 (en) * 1986-04-26 1987-10-29 Bosch Gmbh Robert DEVICE FOR INJECTING FUEL IN THE COMBUSTION ROOM OF INTERNAL COMBUSTION ENGINES
DE3615634A1 (en) * 1986-05-09 1987-11-12 Bosch Gmbh Robert DEVICE FOR INJECTING FUEL INTO THE COMBUSTION CHAMBER OF AN INTERNAL COMBUSTION ENGINE
US4760818A (en) * 1986-12-16 1988-08-02 Allied Corporation Vapor phase injector
JPS6432064A (en) * 1987-07-28 1989-02-02 Nippon Denso Co Electromagnetic fuel injection valve
JPH0733815B2 (en) * 1987-09-02 1995-04-12 株式会社日立製作所 Fuel supply device
IT223984Z2 (en) * 1990-01-17 1995-10-05 Weber Srl VALVE OF A POWER SUPPLY OF AN INTERNAL COMBUSTION ENGINE
DE4224344A1 (en) * 1992-07-23 1994-01-27 Bayerische Motoren Werke Ag Fuel injection nozzle incorporating glow plug for diesel engine - has e.g. three loops of resistance wire mounted in heat-resistant ceramic end of socket and connected electrically in parallel
DE19546851A1 (en) * 1995-12-15 1997-06-19 Bosch Gmbh Robert Fuel injection device for an internal combustion engine
US9790906B2 (en) * 2014-08-15 2017-10-17 Continental Automotive Systems, Inc. High pressure gasoline injector seat to reduce particle emissions

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS51151837U (en) * 1975-05-29 1976-12-04
DE2715943C2 (en) * 1977-04-09 1986-08-14 Robert Bosch Gmbh, 7000 Stuttgart Internal combustion engine with at least one main combustion chamber and an ignition chamber
US4245589A (en) * 1978-07-18 1981-01-20 Ryan Joseph C Exothermic injector adapter
US4300497A (en) * 1980-06-30 1981-11-17 Rockwell International Corporation Prevaporizing diesel precombustion chamber

Also Published As

Publication number Publication date
JPS59162358A (en) 1984-09-13
DE3307666A1 (en) 1984-09-06

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