JPH04334755A - Inlet manifold fuel supply assembly - Google Patents
Inlet manifold fuel supply assemblyInfo
- Publication number
- JPH04334755A JPH04334755A JP3328892A JP3328892A JPH04334755A JP H04334755 A JPH04334755 A JP H04334755A JP 3328892 A JP3328892 A JP 3328892A JP 3328892 A JP3328892 A JP 3328892A JP H04334755 A JPH04334755 A JP H04334755A
- Authority
- JP
- Japan
- Prior art keywords
- fuel
- manifold
- seat structure
- injector
- assembly
- 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
Links
- 239000000446 fuel Substances 0.000 title claims abstract description 56
- 238000002485 combustion reaction Methods 0.000 claims description 6
- 238000005266 casting Methods 0.000 abstract description 14
- 230000015572 biosynthetic process Effects 0.000 abstract 3
- 238000005755 formation reaction Methods 0.000 abstract 3
- 239000002828 fuel tank Substances 0.000 description 5
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
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
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/10—Air intakes; Induction systems
- F02M35/1034—Manufacturing and assembling intake systems
- F02M35/10354—Joining multiple sections together
-
- 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
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/10—Air intakes; Induction systems
- F02M35/10209—Fluid connections to the air intake system; their arrangement of pipes, valves or the like
- F02M35/10216—Fuel injectors; Fuel pipes or rails; Fuel pumps or pressure regulators
-
- 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
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/10—Air intakes; Induction systems
- F02M35/1034—Manufacturing and assembling intake systems
- F02M35/10347—Moulding, casting or the like
-
- 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
- F02M51/00—Fuel-injection apparatus characterised by being operated electrically
- F02M51/005—Arrangement of electrical wires and connections, e.g. wire harness, sockets, plugs; Arrangement of electronic control circuits in or on fuel injection apparatus
-
- 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
- F02M61/168—Assembling; Disassembling; Manufacturing; Adjusting
-
- 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
- F02M69/00—Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
- F02M69/04—Injectors peculiar thereto
- F02M69/042—Positioning of injectors with respect to engine, e.g. in the air intake conduit
- F02M69/044—Positioning of injectors with respect to engine, e.g. in the air intake conduit for injecting into the intake conduit downstream of an air throttle valve
-
- 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
- F02M69/00—Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
- F02M69/46—Details, component parts or accessories not provided for in, or of interest apart from, the apparatus covered by groups F02M69/02 - F02M69/44
- F02M69/462—Arrangement of fuel conduits, e.g. with valves for maintaining pressure in the pipes after the engine being shut-down
- F02M69/465—Arrangement of fuel conduits, e.g. with valves for maintaining pressure in the pipes after the engine being shut-down of fuel rails
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2225/00—Synthetic polymers, e.g. plastics; Rubber
- F05C2225/08—Thermoplastics
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Fuel-Injection Apparatus (AREA)
Abstract
Description
【0001】0001
【産業上の利用分野】本発明は、共通のマニホールドを
有し単一列の複数のシリンダを組込む燃料噴射内燃機関
の組合わされる入口マニホールド燃料供給組立体に関す
る。TECHNICAL FIELD This invention relates to a combined inlet manifold fuel supply assembly for a fuel injected internal combustion engine incorporating a single row of cylinders having a common manifold.
【0002】0002
【従来の技術】内燃機関の代表的な入口マニホールド燃
料供給組立体は、各シリンダに通じる別個の空気入口と
、所要の際に該入口へ制量される量の燃料を噴射する様
に配置される各空気入口に対して別個の燃料噴射器とを
組込む。燃料噴射器を設置する周知の一方法は、燃料レ
ールに該噴射器を装着した後、燃料レールおよび噴射器
を単一ユニットとしてマニホールドに装着することであ
る。BACKGROUND OF THE INVENTION A typical inlet manifold fuel supply assembly for an internal combustion engine has a separate air inlet leading to each cylinder and is arranged to inject a metered amount of fuel into the inlet when required. a separate fuel injector for each air inlet. One known method of installing a fuel injector is to install the injector in a fuel rail and then install the fuel rail and injector as a single unit in a manifold.
【0003】該燃料レールは、代表的に、ポンプを経て
燃料タンクから通じる入口と、圧力調整器を経て燃料タ
ンクへ送給する戻りと、マニホールド内の噴射器への個
々の継手とを有している。The fuel rail typically has an inlet leading from the fuel tank via a pump, a return feeding the fuel tank via a pressure regulator, and individual fittings to the injectors in the manifold. ing.
【0004】0004
【発明の要約】本発明の目的は、単純化される入口マニ
ホールド燃料供給組立体を提供することである。SUMMARY OF THE INVENTION It is an object of the present invention to provide a simplified inlet manifold fuel supply assembly.
【0005】本発明によると、シリンダの列に対する共
通の入口マニホールドを有し単一列の複数のシリンダを
組込む燃料噴射内燃機関の入口マニホールド燃料供給組
立体が提供され、該組立体は、該マニホールドが、シリ
ンダの列の長手方向へ延びる界面に沿って結合される2
つの部分で形成され、該マニホールドの1つの部分が、
複数の座構造を限定し、該各座構造が、燃料噴射器を収
容する様に構成され、該座構造が、関連する入口通路へ
一端において開口し、各座構造に対応する閉鎖構造が、
それ等の座構造およびマニホールド内の共通燃料通路の
中に燃料噴射器を保持する様にマニホールドの他の部分
に設けられ、該共通燃料通路が、燃料を燃料噴射器へ供
給する様に各座構造に連通することを特徴とする。In accordance with the present invention, there is provided an inlet manifold fuel supply assembly for a fuel-injected internal combustion engine incorporating a plurality of cylinders in a single row having a common inlet manifold for the rows of cylinders; , 2 connected along longitudinally extending interfaces of the rows of cylinders
formed of two parts, one part of the manifold comprising:
defining a plurality of seat structures, each seat structure configured to house a fuel injector, the seat structure opening at one end to an associated inlet passageway, and a closure structure corresponding to each seat structure;
A seat structure is provided in the other portion of the manifold to retain the fuel injectors within a common fuel passage within the manifold, the common fuel passage being provided at each seat for supplying fuel to the fuel injectors. It is characterized by communicating with the structure.
【0006】この様にして、別個の燃料レールは、も早
や必要ではなく、従って、組立体の構成要素の数と、別
個の燃料継手の数とを低減する。一般に、構成要素の数
の低減は、費用を低減して信頼性を改善することを可能
にする。[0006] In this way, a separate fuel rail is no longer necessary, thus reducing the number of assembly components and the number of separate fuel couplings. Generally, reducing the number of components allows reducing costs and improving reliability.
【0007】好ましくは、電気的コネクタレールは、マ
ニホールドの組立ての際に噴射器への所要の電気的結合
を自動的に行う様にマニホールド内に設けられる。これ
は、燃料レールおよび/またはマニホールドに対する別
個の外部配線の要件を取り除く。Preferably, electrical connector rails are provided within the manifold to automatically make the necessary electrical connections to the injectors during assembly of the manifold. This eliminates the requirement for separate external wiring to the fuel rail and/or manifold.
【0008】また、好ましくは、圧力リリーフ弁は、マ
ニホールドの2つの部分によって限定されるチャンバ内
に設けられる。[0008] Also preferably, the pressure relief valve is provided within a chamber defined by two portions of the manifold.
【0009】以下、添付図面を参照して例としてのみ本
発明の一実施例を説明する。An embodiment of the invention will now be described, by way of example only, with reference to the accompanying drawings, in which:
【0010】0010
【実施例】図1は、4シリンダの一列を有する火花点火
4シリンダ往復動内燃機関の配置の非常に概略な図であ
る。燃料供給系統を別にして、機関自体は、共通の列の
4つのシリンダ12を有するシリンダブロック、ヘッド
11によって示される。入口マニホールド13は、燃焼
のためにシリンダに空燃混合物を与える様に配置される
。DESCRIPTION OF THE PREFERRED EMBODIMENTS FIG. 1 is a highly schematic representation of the arrangement of a spark-ignited four-cylinder reciprocating internal combustion engine with a row of four cylinders. Apart from the fuel supply system, the engine itself is represented by a cylinder block, head 11, with four cylinders 12 in a common row. Inlet manifold 13 is arranged to provide an air-fuel mixture to the cylinder for combustion.
【0011】図2は、マニホールド13が界面16に沿
って2つの部分14,15に分割されることを示す。代
表的に、双方の部分14,15は、界面の機械加工面と
、所要の個所のその他の機械加工個所とを有するアルミ
ニウム鋳物である。該マニホールドは、1つが各シリン
ダに達する4つの別個の入口通路17を備えている。
代りに、樹脂塑造品がマニホールドに使用されてもよい
。これ等の通路を限る材料は、共通の鋳物の部分を形成
する様にウェブ18によって結合されてもよい。1つが
各入口通路17に対応する4つの座構造19は、燃料噴
射器21を収容する様にマニホールド13の下側部分1
4に設けられる。座構造19は、関連する入口通路17
に一端において開口する。噴射器21は、界面16に隣
接して座構造19の端部に形成されるスピゴット23に
係合するフランジ22によって座構造19内の所定の位
置に配置される。マニホールド13の部分15は、各閉
鎖構造20が1つの座構造19に対応する4つの閉鎖構
造20を限定し、従って、マニホールド13の2つの部
分14,15が一体にボルト止めされるとき、閉鎖構造
20は、座構造19内に噴射器21を保持する様にスピ
ゴット23内にフランジ22を締付ける。これにより、
噴射器21は、マニホールド13内に完全に閉鎖される
。FIG. 2 shows that the manifold 13 is divided into two parts 14, 15 along an interface 16. Typically, both parts 14, 15 are aluminum castings with interfacial machined surfaces and other machined areas as required. The manifold includes four separate inlet passages 17, one to each cylinder. Alternatively, resin moldings may be used for the manifold. These passage-defining materials may be joined by webs 18 to form part of a common casting. Four seat structures 19, one for each inlet passageway 17, are provided in the lower portion 1 of the manifold 13 to accommodate the fuel injectors 21.
4. The seat structure 19 has an associated inlet passage 17
It opens at one end. Injector 21 is placed in position within seat structure 19 by a flange 22 that engages a spigot 23 formed at the end of seat structure 19 adjacent interface 16 . Portion 15 of manifold 13 defines four closure structures 20, each closure structure 20 corresponding to one seat structure 19, so that when the two sections 14, 15 of manifold 13 are bolted together, the closure Structure 20 clamps flange 22 within spigot 23 to retain injector 21 within seat structure 19. This results in
Injector 21 is completely enclosed within manifold 13.
【0012】該噴射器は、各閉鎖構造20に対して開口
する鋳物15の長手方向溝に固定される電気的コネクタ
レール24によって各噴射器に別個に供給される信号に
よって電気的に制御される。コネクタレール24は、マ
ニホールド13の2つの部分14,15の組立ての際に
、噴射器に自動的に所要の結合をなす様に配置される。
電気的コネクタレール24は、噴射器21を操作するた
めに電気信号を供給する多重ピンコネクタ30において
終る。The injectors are electrically controlled by signals supplied to each injector separately by an electrical connector rail 24 fixed in a longitudinal groove of the casting 15 opening to each closure structure 20. . The connector rail 24 is arranged so as to automatically make the required connection to the injector during assembly of the two parts 14, 15 of the manifold 13. Electrical connector rail 24 terminates in a multi-pin connector 30 that provides electrical signals to operate injector 21.
【0013】長手方向の燃料通路25は、鋳物14内の
總ての4つの座構造19に連通し、従って、總ての4つ
の噴射器に対する燃料レールへ等しい共通の燃料供給を
与える。燃料は、入口29に対してポンプ(図示せず)
を経て燃料タンクから通路25へ供給される。図1に示
す様に、チャンバ26は、2つの隣接する座構造19お
よびこれ等の関連する噴射器21の間にマニホールド1
3の部分14,15によって形成され、該チャンバは、
圧力リリーフ弁27を装着する。戻り管28は、チャン
バ26の下流領域から燃料タンクへ通じる。燃料は、各
噴射器21の2つのシール33と、圧力リリーフ弁27
の同様なシールとによってレール内に保持される。別の
シール34は、界面16を密封する。The longitudinal fuel passages 25 communicate with all four seat structures 19 in the casting 14, thus providing an equal common fuel supply to the fuel rails for all four injectors. Fuel is pumped (not shown) to inlet 29.
The fuel is supplied from the fuel tank to the passage 25 via the fuel tank. As shown in FIG.
3, the chamber is formed by parts 14, 15 of 3;
Install the pressure relief valve 27. A return pipe 28 leads from the downstream region of the chamber 26 to the fuel tank. The fuel is supplied to the two seals 33 of each injector 21 and the pressure relief valve 27.
is retained within the rail by a similar seal. Another seal 34 seals the interface 16.
【0014】個々の仕上げられた構成要素によって完全
な入口マニホールド燃料供給組立体を組立てるため、コ
ネクタレール組立体24は、多重ピンコネクタ30と共
に鋳物15に最初に挿入される。次に、個々の噴射器2
1は、座構造19に挿入され、それ等のフランジ22に
よってスピゴット23内の所要の位置に配置される。圧
力リリーフ弁27は、チャンバ26内に同様に設置され
る。次に、上側鋳物15は、下側鋳物14に係合する様
にもたらされ、次に、噴射器21への電気的な結合は、
自動的になされる。2つの鋳物14,15は位置決めピ
ンまたはスピゴットの様な装置によって共に位置決めさ
れ、一連のスタッドまたはボルトによって一緒に保持さ
れる。ガスケットまたはシール用コンパウンドは、組立
て操作の際に所要によって使用される。次に、燃料供給
管路および戻り管路の任意の所要の継手は、装着される
。Connector rail assembly 24 is first inserted into casting 15 along with multi-pin connector 30 to assemble a complete inlet manifold fuel supply assembly with individual finished components. Next, the individual injectors 2
1 are inserted into the seat structure 19 and placed in position within the spigot 23 by their flanges 22. A pressure relief valve 27 is similarly installed within the chamber 26. The upper casting 15 is then brought into engagement with the lower casting 14 and the electrical connection to the injector 21 is then made.
done automatically. The two castings 14, 15 are positioned together by devices such as locating pins or spigots and held together by a series of studs or bolts. Gaskets or sealing compounds are optionally used during assembly operations. Any required fittings of the fuel supply and return lines are then fitted.
【0015】次に、完成されたマニホールド組立体は、
通路17が入口弁32を経てシリンダ12に結合する入
口ポート31に整合する様に、通常の態様で機関11に
装架される。機関の使用の際、入口マニホールド13と
、その燃料供給装置とは、通常の様に作用する。Next, the completed manifold assembly is
The engine 11 is mounted in a conventional manner such that the passageway 17 is aligned with an inlet port 31 that connects to the cylinder 12 via an inlet valve 32. During use of the engine, the inlet manifold 13 and its fuel supply function in a normal manner.
【0016】全体の入口マニホールド13燃料供給組立
体は、簡単な組立て操作へ導き非常に高い信頼性の可能
性を与える比較的少い数の構成要素から成るユニットで
ある。The entire inlet manifold 13 fuel supply assembly is a unit consisting of a relatively small number of components leading to a simple assembly operation and providing the potential for very high reliability.
【0017】本発明は、特に、火花点火往復動機関に適
用可能であるが、他の型式の機関、例えば多シリンダ回
転式機関に使用されてもよい。同様に、V形6シリンダ
またはV形8シリンダまたはV形12シリンダの機関は
、本発明に適用される概念を持ってもよい。Although the invention is particularly applicable to spark ignition reciprocating engines, it may also be used in other types of engines, such as multi-cylinder rotary engines. Similarly, V6-cylinder or V8-cylinder or V12-cylinder engines may have the concept applied to the present invention.
【図1】理解し易くするために変更された幾つかの部分
の相対的な位置によりマニホールドの一部を組込む機関
の一部の概略の平面図。FIG. 1 is a schematic plan view of a part of an engine incorporating part of a manifold, with the relative positions of the several parts modified for clarity;
【図2】付加的な構成要素を示す1つのシリンダおよび
関連する噴射器の拡大断面図。FIG. 2 is an enlarged cross-sectional view of one cylinder and associated injector showing additional components.
12 シリンダ 13 入口マニホールド 14 下側部分(鋳物) 15 上側部分(鋳物) 16 界面 17 入口通路 19 座構造 20 閉鎖構造 21 燃料噴射器 24 電気的コネクタレール 25 燃料通路 26 チャンバ 27 圧力リリーフ弁 12 Cylinder 13 Inlet manifold 14 Lower part (casting) 15 Upper part (casting) 16 Interface 17 Entrance passage 19 Seat structure 20 Closed structure 21 Fuel injector 24 Electrical connector rail 25 Fuel passage 26 Chamber 27 Pressure relief valve
Claims (4)
入口マニホールド(13)を有し単一列の複数のシリン
ダ(12)を組込む燃料噴射内燃機関の入口マニホール
ド(13)燃料供給組立体において,前記マニホールド
(13)が、前記シリンダ(12)の列の長手方向へ延
びる界面(16)に沿って結合される2つの部分(14
,15)で形成され,該マニホールド(13)の1つの
部分(14)が、複数の座構造(19)を限定し,該各
座構造(19)が、燃料噴射器(21)を収容する様に
構成され,該座構造(19)が、関連する入口通路(1
7)へ一端において開口し,該各座構造(19)に対応
する閉鎖構造(20)が、それ等の座構造(19)と、
前記マニホールド(13)内の共通燃料通路(25)と
の中に前記燃料噴射器(21)を保持する様に該マニホ
ールド(13)の他の部分(15)に設けられ,該共通
燃料通路(25)が、燃料を該燃料噴射器(21)へ供
給する様に該各座構造(19)に連通することを特徴と
する組立体。1. An inlet manifold (13) fuel supply assembly for a fuel-injected internal combustion engine incorporating a plurality of cylinders (12) in a single row having a common inlet manifold (13) for the rows of cylinders (12); The manifold (13) has two parts (14) joined along a longitudinally extending interface (16) of said row of cylinders (12).
, 15), a portion (14) of the manifold (13) defining a plurality of seat structures (19), each seat structure (19) housing a fuel injector (21). The seat structure (19) is configured in such a way that the seat structure (19)
A closed structure (20) opening at one end to 7) and corresponding to each seat structure (19) is connected to the seat structure (19);
The common fuel passage (25) in the manifold (13) is provided in another part (15) of the manifold (13) so as to hold the fuel injector (21) in the common fuel passage (25). 25) communicates with said seat structure (19) for supplying fuel to said fuel injector (21).
気的コネクタレール(24)が、前記マニホールド(1
3)の組立ての際に前記噴射器(21)への所要の電気
的結合を自動的に行う様に該マニホールド(13)内に
配置されることを特徴とする組立体。2. An assembly according to claim 1, wherein the electrical connector rail (24) is connected to the manifold (1).
3), characterized in that it is arranged in said manifold (13) so as to automatically make the necessary electrical connections to said injector (21) during assembly.
体において,圧力リリーフ弁(27)が、前記マニホー
ルド(13)の2つの部分(14,15)によって限定
されるチャンバ(26)内に設けられることを特徴とす
る組立体。3. An assembly according to claim 1 or claim 2, wherein the pressure relief valve (27) is arranged in a chamber (26) defined by two parts (14, 15) of the manifold (13). An assembly characterized in that it is provided in.
の項に記載の組立体において,前記燃料通路(25)が
、前記マニホールド(13)の第1部分(14)に沿っ
て延び、前記座構造(19)を直接に切り取ることを特
徴とする組立体。4. An assembly according to any one of claims 1 to 3, wherein the fuel passageway (25) extends along a first part (14) of the manifold (13), An assembly characterized in that the seat structure (19) is cut directly.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB91038331 | 1991-02-23 | ||
| GB919103833A GB9103833D0 (en) | 1991-02-23 | 1991-02-23 | Inlet manifold and fuel supply system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH04334755A true JPH04334755A (en) | 1992-11-20 |
Family
ID=10690486
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP3328892A Pending JPH04334755A (en) | 1991-02-23 | 1992-02-20 | Inlet manifold fuel supply assembly |
Country Status (3)
| Country | Link |
|---|---|
| EP (1) | EP0501612A3 (en) |
| JP (1) | JPH04334755A (en) |
| GB (1) | GB9103833D0 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018066168A1 (en) * | 2016-10-07 | 2018-04-12 | 株式会社ミクニ | Fuel injection device |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5465699A (en) * | 1993-06-01 | 1995-11-14 | Volkswagen Ag | Intake pipe arrangement for an internal combustion engine having individual arc-shaped cylinder intake pipes |
| US5353767A (en) * | 1993-12-17 | 1994-10-11 | General Motors Corporation | Fuel and air induction system |
| DE19600378A1 (en) * | 1996-01-08 | 1997-07-10 | Bosch Gmbh Robert | Fuel injection system |
| US5771863A (en) * | 1996-10-11 | 1998-06-30 | Siemens Electric Limited | Integrated intake manifold and fuel rail with enclosed fuel filter |
| WO2003012279A1 (en) * | 2001-07-31 | 2003-02-13 | Filterwerk Mann & Hummel Gmbh | An air intake and a method for installing an air intake |
| DE10145035A1 (en) | 2001-09-13 | 2003-04-10 | Bosch Gmbh Robert | fuel injection system |
| US6786203B1 (en) * | 2002-04-30 | 2004-09-07 | Siemens Vdo Automotive Corporation | Injector valve for integrated air/fuel module |
| US6769410B2 (en) * | 2002-06-18 | 2004-08-03 | Siemens Vdo Automotive Inc. | Integrated fuel module wire harness and carrier gasket for vehicle intake manifold |
| JP4657177B2 (en) * | 2006-08-29 | 2011-03-23 | 本田技研工業株式会社 | Internal combustion engine |
| FR2909731A1 (en) * | 2006-12-08 | 2008-06-13 | Renault Sas | Internal combustion engine's part manufacturing method for vehicle, involves incorporating part of common fuel supply ramp into injection tubes by injecting synthetic material compatible with that of conduit of air intake splitter |
| GB2465996B (en) * | 2008-12-05 | 2013-07-24 | Gm Global Tech Operations Inc | Injection system and method of cold starting a combustion engine |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3333843A1 (en) * | 1983-09-20 | 1985-04-04 | Dr.Ing.H.C. F. Porsche Ag, 7000 Stuttgart | PIPE SYSTEM FOR AN INTERNAL COMBUSTION ENGINE |
| JPS6288875U (en) * | 1985-11-22 | 1987-06-06 | ||
| GB2195394A (en) * | 1986-09-17 | 1988-04-07 | Ford Motor Co | Fuel injection system component |
| US4966120A (en) * | 1987-07-29 | 1990-10-30 | Aisan Kogyo Kabushiki Kaisha | Fuel injection system assembly |
| DE3739108A1 (en) * | 1987-11-19 | 1989-06-01 | Opel Adam Ag | INTERNAL COMBUSTION ENGINE WITH A FUEL INJECTION SYSTEM |
| US5022371A (en) * | 1989-09-29 | 1991-06-11 | Siemens-Bendix Automotive Electronics L.P. | Molded plastic fuel rail for an internal combustion engine |
-
1991
- 1991-02-23 GB GB919103833A patent/GB9103833D0/en active Pending
-
1992
- 1992-01-29 EP EP19920300769 patent/EP0501612A3/en not_active Withdrawn
- 1992-02-20 JP JP3328892A patent/JPH04334755A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018066168A1 (en) * | 2016-10-07 | 2018-04-12 | 株式会社ミクニ | Fuel injection device |
Also Published As
| Publication number | Publication date |
|---|---|
| EP0501612A2 (en) | 1992-09-02 |
| EP0501612A3 (en) | 1992-10-21 |
| GB9103833D0 (en) | 1991-04-10 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US5657733A (en) | Fuel injector mounting for molded intake manifold with integrated fuel rail | |
| US7296558B2 (en) | Dual-injector fuel injection engine | |
| US5022371A (en) | Molded plastic fuel rail for an internal combustion engine | |
| US5673673A (en) | Method and apparatus for the high Mach injection of a gaseous fuel into an internal combustion engine | |
| JPH04334755A (en) | Inlet manifold fuel supply assembly | |
| WO1999000595A3 (en) | Fuel injection system | |
| EP1304477A3 (en) | Multi-point fuel injection module | |
| US6622700B2 (en) | Integrated fuel system and wiring harness | |
| EP0261855B1 (en) | Fuel injection system component | |
| JP3871016B2 (en) | Fuel injector mounting structure for in-cylinder injection engine | |
| US5146897A (en) | Intake manifold of intake system for multi-cylinder internal combustion engine | |
| ES2004644A6 (en) | Injection valve | |
| US3980058A (en) | Fuel feed control system of internal combustion engine | |
| US2995123A (en) | Fuel injecting means for internal combustion engines of the type compressing a fuel-air mixture | |
| US20190331061A1 (en) | Intake manifold with integrated water injection nozzle | |
| US11268475B2 (en) | Cylinder head for a combustion engine, and a method for supply of prechamber gas in a cylinder head | |
| GB2203487A (en) | A fuel injection system component | |
| JPH029176B2 (en) | ||
| JPH0988761A (en) | Fuel injection device for internal combustion engine | |
| JP7211216B2 (en) | engine fuel supply | |
| JPH0450458Y2 (en) | ||
| JPS6327094Y2 (en) | ||
| JPH03121250A (en) | Mixture supply device for multi-cylinder internal combustion engine | |
| JPH09256928A (en) | Intake device for direct injection gasoline engine | |
| JP3879507B2 (en) | Fuel supply device for internal combustion engine |