JPH04136478A - Air/fuel injection valve device for engine - Google Patents

Air/fuel injection valve device for engine

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Publication number
JPH04136478A
JPH04136478A JP25732990A JP25732990A JPH04136478A JP H04136478 A JPH04136478 A JP H04136478A JP 25732990 A JP25732990 A JP 25732990A JP 25732990 A JP25732990 A JP 25732990A JP H04136478 A JPH04136478 A JP H04136478A
Authority
JP
Japan
Prior art keywords
fuel
valve
air
fuel injection
injection 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
JP25732990A
Other languages
Japanese (ja)
Inventor
Takeshi Motoyama
本山 雄
Junichi Kako
淳一 加来
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.)
Yamaha Motor Co Ltd
Original Assignee
Yamaha 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 Yamaha Motor Co Ltd filed Critical Yamaha Motor Co Ltd
Priority to JP25732990A priority Critical patent/JPH04136478A/en
Publication of JPH04136478A publication Critical patent/JPH04136478A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To greatly broaden the control range for the fuel injection quantity by installing a subfuel feeding system for continuously feeding fuel to the upstream side of a main valve and an electromagnetic opening/closing valve for operating the subfuel feeding system in the prescribed operation region of the engine. CONSTITUTION:An air/fuel injection valve 28 is equipped with at least an electromagnetic type fuel injection valve 32. Further, the air used in the injection valve 28 is introduced into an air passage 72 by an air pump 70. Further, gasoline fuel is introduced into the fuel passage 76 of the fuel injection valve 32 from a fuel tank 80 by a fuel pump 78. In this case, the discharge side of the fuel pump 78 and the fuel injection valve 32 are allowed to communicate through a fuel pipe 90 which forms a subfuel feeding system, and an electromagnetic opening/closing valve 92 is interposed midway in the pipe 90. The electromagnetic opening/closing valve 92 is opened by a controller 94 under the prescribed operation condition such as in high loading on the basis of the data which shows the operation state, and fuel is added from the subfuel feeding system 90.

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は、液体あるいは気体燃料と空気とを予め混合し
てエンジンの燃焼室内に噴射する空気・燃料噴射弁装置
に関するものである。
DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention relates to an air/fuel injection valve device for pre-mixing liquid or gaseous fuel and air and injecting the mixture into a combustion chamber of an engine.

(発明の背景) 近年2サイクルエンジンの混合気の吹き抜けを防止する
ため、燃焼室内に直接燃料を噴射する筒内噴射方式が研
究されている。ここに燃料の微粒化を図るために空気と
燃料とを予め混合して筒内に噴射する空気・燃料噴射方
式が提案されている。ここに従来の燃料噴射弁は、少量
の噴射量を制御できるように噴射口を小径に設定すると
、噴射量を十分に増加させることができず、反対に噴射
量を大きくするために噴射口を大径にすると少噴射量の
制御が高精度にできなくなるという問題があった。この
ため燃料噴射量の制御範囲が狭(なるという問題があっ
た。
(Background of the Invention) In recent years, in order to prevent the air-fuel mixture from blowing through in two-cycle engines, research has been conducted on in-cylinder injection methods in which fuel is directly injected into the combustion chamber. In order to atomize the fuel, an air/fuel injection method has been proposed in which air and fuel are mixed in advance and injected into the cylinder. In conventional fuel injection valves, if the injection port is set to a small diameter to control a small amount of injection, the injection amount cannot be increased sufficiently. When the diameter is made large, there is a problem that it becomes impossible to control the small injection amount with high precision. For this reason, there was a problem that the control range of the fuel injection amount became narrow.

(発明の目的) 本発明はこのような事情に鑑みなされたものであり、燃
料噴射量の制御範囲を大幅に拡大することができるエン
ジンの空気・燃料噴射弁装置を提供することを目的とす
るものである。
(Object of the Invention) The present invention has been made in view of the above circumstances, and an object thereof is to provide an air/fuel injection valve device for an engine that can significantly expand the control range of the fuel injection amount. It is something.

(発明の構成) 本発明によればこの目的は、燃料噴射弁から間欠的に噴
射される燃料と所定圧の空気との混合流を、主弁の開閉
によって燃焼室内に間欠的に噴射する空気・燃料噴射弁
装置において、前記主弁の上流側に燃料を連続的に供給
する副燃料供給系と、この副燃料供給系をエンジンの所
定運転領域で作動させる電磁開閉弁とを備えることを特
徴とするエンジンの空気・燃料噴射弁装置、により達成
される。
(Structure of the Invention) According to the present invention, the object is to inject a mixed flow of fuel intermittently injected from a fuel injection valve and air at a predetermined pressure into a combustion chamber intermittently by opening and closing a main valve. - The fuel injection valve device is characterized by comprising a sub-fuel supply system that continuously supplies fuel to the upstream side of the main valve, and an electromagnetic on-off valve that operates the sub-fuel supply system in a predetermined operating range of the engine. This is achieved by the engine's air/fuel injection valve system.

(作用) エンジンの高負荷運点時などの所定運転領域では電磁開
閉弁が開き、副燃料供給系が作動状態になる。この状態
では副燃料供給系は主弁の上流側に燃料を連続的に供給
する。従ってこの運転領域では燃料噴射弁とこの副燃料
供給系との両方から燃料が供給されることになる。また
この所定運転領域外の例えば低・中負荷運転時には、こ
のif電磁開閉弁閉じて副燃料供給系は不作動となる。
(Operation) In a predetermined operating range such as when the engine is operating under high load, the electromagnetic on-off valve opens and the auxiliary fuel supply system becomes operational. In this state, the auxiliary fuel supply system continuously supplies fuel to the upstream side of the main valve. Therefore, in this operating range, fuel is supplied from both the fuel injection valve and this auxiliary fuel supply system. Further, during low/medium load operation outside the predetermined operation range, for example, the if electromagnetic on-off valve closes and the auxiliary fuel supply system becomes inoperable.

このため燃料噴射弁だけから燃料が供給されることにな
る。
Therefore, fuel is supplied only from the fuel injection valve.

(実施例) 第1図は本発明の一実施例の全体図、第2図はその噴射
特性図、第3図は他の実施例の全体図、第4図はその噴
射特性図、第5図は空気・燃料噴射弁の断面図、第6図
と第7図はその主弁付近の異なる実施例を示す断面図で
ある。
(Example) Fig. 1 is an overall view of one embodiment of the present invention, Fig. 2 is an injection characteristic diagram thereof, Fig. 3 is an overall view of another embodiment, Fig. 4 is an injection characteristic diagram thereof, and Fig. 5 is an overview diagram of an embodiment of the present invention. The figure is a cross-sectional view of the air/fuel injection valve, and FIGS. 6 and 7 are cross-sectional views showing different embodiments near the main valve.

第1.3図において、符号10は2サイクルエンジン、
12はクランク軸、14はピストン、16はシリンダで
ある。吸気はエアフローメータ18、スロットル弁20
、リード弁22を介してクランク室24に吸入される。
In Fig. 1.3, numeral 10 is a two-stroke engine;
12 is a crankshaft, 14 is a piston, and 16 is a cylinder. Intake air flow meter 18, throttle valve 20
, is sucked into the crank chamber 24 via the reed valve 22.

燃焼室26の頂部には第5図で説明する空気・燃料噴射
弁28が取付けられ、ここから所定タイミングで燃料と
空気との混合流が燃焼室26内に間欠的に噴射される。
An air/fuel injection valve 28 described in FIG. 5 is attached to the top of the combustion chamber 26, from which a mixed flow of fuel and air is intermittently injected into the combustion chamber 26 at predetermined timings.

30は点火栓である。30 is a spark plug.

空気・燃料噴射弁28は、第5図に示すよづに公知の電
磁式燃料噴射弁32と、混合流の流出を断続するための
電磁ソレノイド34とを有する。
The air/fuel injection valve 28 includes a known electromagnetic fuel injection valve 32 shown in FIG. 5, and an electromagnetic solenoid 34 for cutting off and on the outflow of the mixed flow.

すなわちこの電磁ソレノイド34の可動片36はケース
38内にダイヤフラム40で横方向の移動が規制される
一方、復帰ばね42により上方への復帰習性が付与され
ている。この可動片36には弁軸44の上端が固定され
ている。
That is, the movable piece 36 of the electromagnetic solenoid 34 is restricted from moving in the lateral direction by a diaphragm 40 inside the case 38, and is given the tendency to return upward by a return spring 42. The upper end of the valve shaft 44 is fixed to the movable piece 36.

ケース38の下面には内筒46および外筒48が固定さ
れている。内筒46は外筒48内に同軸に挿入され、両
筒46.48の間に燃料流路50を形成する。前記弁軸
44はこの内筒46内を通って下降し、この弁軸44の
下端に設けた傘型の弁体52は、内筒46の弁座54に
下から当接して主弁56を形成する(第6.7図)。
An inner tube 46 and an outer tube 48 are fixed to the lower surface of the case 38. The inner cylinder 46 is coaxially inserted into the outer cylinder 48, forming a fuel passage 50 between the two cylinders 46,48. The valve shaft 44 descends through the inner cylinder 46, and the umbrella-shaped valve body 52 provided at the lower end of the valve shaft 44 contacts the valve seat 54 of the inner cylinder 46 from below to open the main valve 56. form (Figure 6.7).

第6図の実施例における弁軸44には、弁体52の上方
に所定間隔をもって円板58が形成され、また第7図の
実施例では弁体52に連続して円柱58Aが形成されて
いる。これらの円板58および円柱58Aの上方には放
射状の4本の爪60が形成されている。円板58および
円柱58Aは、内筒46の内壁との間に一定間隔の円環
状の絞り62.62A(第6.7図参照)を形成する。
In the embodiment shown in FIG. 6, a disk 58 is formed on the valve shaft 44 at a predetermined interval above the valve body 52, and in the embodiment shown in FIG. There is. Four radial claws 60 are formed above the disk 58 and the cylinder 58A. The disk 58 and the cylinder 58A form an annular diaphragm 62.62A (see FIG. 6.7) with a constant interval between the disk 58 and the inner wall of the inner cylinder 46.

4本の爪60は内筒46の内壁を摺動して弁軸44の径
方向の移動を規制する。そしてこの爪60と円板58あ
るいは円柱58Aとの間に混合室64が形成される。前
記の絞り62.62Aは主弁56の開閉に伴う混合室6
4.64Aの圧力変化を抑制し、燃料の噴射量を安定化
させる機能を有するものである。前記燃料通路50の下
端はオリフィス66によってこの混合室64.64Aに
連通している。
The four claws 60 slide on the inner wall of the inner cylinder 46 to restrict movement of the valve shaft 44 in the radial direction. A mixing chamber 64 is formed between the claw 60 and the disk 58 or cylinder 58A. The aforementioned throttle 62.62A opens and closes the mixing chamber 6 as the main valve 56 opens and closes.
It has the function of suppressing pressure changes of 4.64 A and stabilizing the fuel injection amount. The lower end of the fuel passage 50 communicates with this mixing chamber 64.64A by an orifice 66.

この噴射弁28に使用される空気は第1.3図に示す空
気ポンプ70により加圧され、第5図に示す空気通路7
2からケース38内の空気通路74に常時導かれ、内筒
46と弁軸44との間の混合室64.64A(第6.7
図)に入る。第1.3図で76は空気圧を一定(例えば
5.0Kg/cm2)に保つリリーフ弁である。
The air used in this injection valve 28 is pressurized by an air pump 70 shown in FIG. 1.3, and the air passage 70 shown in FIG.
2 to the mixing chamber 64.64A (No. 6.7) between the inner cylinder 46 and the valve shaft 44.
Figure). In Fig. 1.3, 76 is a relief valve that keeps the air pressure constant (for example, 5.0 kg/cm2).

燃料噴射弁32はケース38に取付けられ、前記空気圧
よりやや高い圧力(例えば5.5Kg/cm2)の燃料
が燃料通路76に供給されている。
The fuel injection valve 32 is attached to the case 38, and fuel is supplied to the fuel passage 76 at a pressure slightly higher than the air pressure (for example, 5.5 kg/cm2).

すなわち第1.3図に示す燃料ポンプ78は、燃料タン
ク80からガソリン燃料を吸い上げて加圧し吐出するが
、この吐出側にはリリーフ弁82が接続され、吐出圧が
一定(例えば5 、5 Kg/cm2)に維持される。
That is, the fuel pump 78 shown in FIG. 1.3 sucks up gasoline fuel from the fuel tank 80, pressurizes it, and then discharges it. A relief valve 82 is connected to the discharge side of the fuel pump 78, so that the discharge pressure is constant (for example, 5.5 kg). /cm2).

そしてこの一定圧の燃料が燃料噴射弁32の燃料通路7
6に導かれる。燃料噴射弁32から噴射されたガソリン
燃料はケース38および外筒48に形成され燃料通路8
4(第5図)を通って内・外筒46.48間の前記燃料
通路50に導かれる。この燃料はさらにオリフィス66
から混合室64.64Aに流入する。
This constant pressure fuel flows into the fuel passage 7 of the fuel injection valve 32.
6. Gasoline fuel injected from the fuel injection valve 32 is formed in the case 38 and the outer cylinder 48 and flows through the fuel passage 8.
4 (FIG. 5) and is led to the fuel passage 50 between the inner and outer cylinders 46 and 48. This fuel is further fed to the orifice 66.
and flows into the mixing chamber 64.64A.

第1図において符号90は副燃料供給系を形成する燃料
バイブであり、このバイブ90は燃料ポンプ78の吐出
側と燃料通路84とを連通ずる。
In FIG. 1, reference numeral 90 is a fuel vibrator forming an auxiliary fuel supply system, and this vibrator 90 communicates the discharge side of the fuel pump 78 with the fuel passage 84.

このバイブ90の途中には電磁開閉弁92が介在し、非
励磁時にはこのバイブ90を閉路し励磁時に開路する。
An electromagnetic on-off valve 92 is interposed in the middle of this vibrator 90, which closes the vibrator 90 when it is not energized and opens it when it is energized.

また第3図の実施例ではリリーフ弁82の下流側にさら
に別のリリーフ弁82Aが接続されている。このリリー
フ弁82Aは、リリーフ弁82よりも低くかつ空気圧に
ほぼ等しい圧力(例えば5 、 0 Kg/cm2)で
開き燃料をタンク80に戻す。
Further, in the embodiment shown in FIG. 3, another relief valve 82A is connected downstream of the relief valve 82. This relief valve 82A opens at a pressure lower than that of the relief valve 82 and approximately equal to air pressure (for example, 5.0 Kg/cm2) to return the fuel to the tank 80.

そしてこの実施例で副燃料供給系となる燃料バイブ90
Aは、両リリーフ弁82.82A間から電磁開閉弁92
を介して燃料を燃料通路84に導く。
In this embodiment, a fuel vibrator 90 serves as an auxiliary fuel supply system.
A is the electromagnetic on-off valve 92 from between both relief valves 82 and 82A.
The fuel is introduced into the fuel passage 84 through the fuel passageway 84 .

第1.3図において94はCPUやメモリなどからなる
制御装置であり、電磁開閉弁92、燃料噴射弁32、電
磁ソレノイド34などを制御するものである。すなわち
エアフローメータ18から検出した吸気流量Q、スロッ
トル弁20の開度θ、クランク軸12の回転速度Nなど
の運転状態を示すデータがこの制御装置94に入力され
ると、この制御装置92はこの運転条件に適する燃料噴
射量をメモリから読出し、電磁ソレノイド34と燃料噴
射弁32との開弁時間τを求める。
In FIG. 1.3, 94 is a control device consisting of a CPU, memory, etc., and controls the electromagnetic on-off valve 92, the fuel injection valve 32, the electromagnetic solenoid 34, etc. That is, when data indicating the operating state such as the intake flow rate Q detected from the air flow meter 18, the opening degree θ of the throttle valve 20, and the rotational speed N of the crankshaft 12 is input to this control device 94, this control device 92 The fuel injection amount suitable for the operating conditions is read from the memory, and the opening time τ of the electromagnetic solenoid 34 and the fuel injection valve 32 is determined.

また高負荷時などの所定運転条件下では電磁開閉弁92
を開き、副燃料供給系から燃料の追加を行う。
Also, under certain operating conditions such as during high loads, the solenoid on-off valve 92
Open it and add fuel from the auxiliary fuel supply system.

次に第1図の実施例の動作を説明する。制御装置92は
、低・中負荷時などの所定条件下では電磁開閉弁92を
閉じ、主弁56が開いている期間内の燃焼噴射弁32が
開いて燃料噴射弁32だけから燃料を供給する。この時
には第2図にaで示すよう舛こ開弁時間りにほぼ比例し
て噴射量qが増える。高負荷時などの所定条件になると
電磁開閉弁92が開(。すると副燃料供給系であるバイ
ブ9oを介して燃料が燃料通路84に供給される。この
燃料圧(約5 、5 Kg/cm2)は空気圧(約5 
、0 Kg/Cm”)より高いので連続的に燃料は供給
されるが、主弁56の開弁時には混合室64内の圧力が
低下して燃料噴射弁32の燃料供給側と吐出側との差圧
が増えるのでその供給量が増える。
Next, the operation of the embodiment shown in FIG. 1 will be explained. The control device 92 closes the electromagnetic on-off valve 92 under predetermined conditions such as during low/medium load, opens the combustion injection valve 32 during the period when the main valve 56 is open, and supplies fuel only from the fuel injection valve 32. . At this time, as shown by a in FIG. 2, the injection amount q increases approximately in proportion to the valve opening time. When a predetermined condition such as high load is reached, the electromagnetic on-off valve 92 opens (then fuel is supplied to the fuel passage 84 via the vibrator 9o, which is an auxiliary fuel supply system. This fuel pressure (approx. ) is the air pressure (approximately 5
, 0 Kg/Cm"), so fuel is continuously supplied, but when the main valve 56 is opened, the pressure in the mixing chamber 64 decreases and the pressure between the fuel supply side and the discharge side of the fuel injection valve 32 decreases. As the differential pressure increases, the supply amount increases.

このためこの副燃料供給系から供給される燃料量qは第
2図にbで示すように開弁時間ての増加に伴って僅かに
増加する。この結果この時の総燃料量Cは実線で示すよ
うにc=:a+bとなる。
Therefore, the amount of fuel q supplied from the auxiliary fuel supply system increases slightly as the valve opening time increases, as shown by b in FIG. As a result, the total fuel amount C at this time becomes c=:a+b as shown by the solid line.

また第3図の実施例によれば、N磁開閉弁92が閉じた
低・中負荷時の動作は第1図のものと同じである。しか
し電磁開閉弁92が開く高負荷時においては、リリーフ
弁82Aにより決まる燃料圧が空気圧にほぼ等しいので
前記第1図のものと異なる。すなわち電磁開閉弁92が
開いても主弁56が閉じている時にはバイブ9OAから
は燃料が供給されず、主弁56が開いて混合室64Aが
減圧した時だけ燃料の供給が行われる。従ってこの時の
副燃料供給系からの供給量qは第4図にb′で示すよう
に主弁56の開弁時間てにほぼ比例する。この結果、総
供給量C′はc’ =a+b′になる。
Further, according to the embodiment shown in FIG. 3, the operation at low and medium loads when the N-magnetic on-off valve 92 is closed is the same as that shown in FIG. However, when the electromagnetic on-off valve 92 is opened under high load, the fuel pressure determined by the relief valve 82A is approximately equal to the air pressure, which is different from that shown in FIG. 1. That is, even if the electromagnetic on-off valve 92 is open, fuel is not supplied from the vibrator 9OA when the main valve 56 is closed, and fuel is supplied only when the main valve 56 is opened and the pressure in the mixing chamber 64A is reduced. Therefore, the amount q supplied from the auxiliary fuel supply system at this time is approximately proportional to the opening time of the main valve 56, as shown by b' in FIG. As a result, the total supply amount C' becomes c' = a + b'.

以上の実施例では、主弁56の開弁期間内&と燃料噴射
弁32が開弁するものとして説明しているが、本発明は
両者の開弁期間の一部が重なるものや、全く重ならない
ものであってもよい。
In the above embodiments, the fuel injection valve 32 is opened during the opening period of the main valve 56 and the fuel injection valve 32 is opened. It may be something that does not exist.

またこの実施例では副燃料供給系は燃料通路84に燃料
を供給するが、本発明は主弁56より上流側であれば混
合室64.64Aやその上流側の空気通路内に供給する
ものであってもよい。
Further, in this embodiment, the auxiliary fuel supply system supplies fuel to the fuel passage 84, but in the present invention, as long as it is upstream of the main valve 56, it supplies fuel to the mixing chamber 64.64A and the air passage upstream thereof. There may be.

(発明の効果) 本発明は以上のように、高負荷時などの所定の運転領域
で電磁開閉弁が副燃料供給系を開路するようにしたから
、燃料噴射弁からの燃料供給に加えてこの副燃料供給系
からも燃料が供給される。
(Effects of the Invention) As described above, the present invention allows the electromagnetic on-off valve to open the auxiliary fuel supply system in a predetermined operating range such as during high load. Fuel is also supplied from the auxiliary fuel supply system.

また低・中負荷時などでは電磁開閉弁が副燃料供給系を
閉路するから、燃料噴射弁のみから燃料が供給される。
Furthermore, under low or medium load conditions, the electromagnetic on-off valve closes the auxiliary fuel supply system, so fuel is supplied only from the fuel injection valve.

この結果燃料供給量の制御範囲が拡4゜ 大する。As a result, the control range of fuel supply amount has been expanded by 4°. make it big

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

第1図は本発明の一実施例の全体図、第2図はその噴射
特性図、第3図は他の実施例の全体図、第4図はその噴
射特性図、第5図は空気・燃料噴射弁の断面図、第6図
と第7図はその主弁付近の異なる実施例を示す断面図で
ある。 28・・・空気・燃料噴射弁、 32・・・燃料噴射弁、 34・・・電磁ソレノイド、 56・・・主弁、 70・・・空気ポンプ、 78・・・燃料ポンプ、 90.90A・・・副燃料供給系となる燃料パイプ、 92・・・1ffn開閉弁。 特許出願人 ヤマハ発動機株式会社
Fig. 1 is an overall view of one embodiment of the present invention, Fig. 2 is an injection characteristic diagram thereof, Fig. 3 is an overall view of another embodiment, Fig. 4 is an injection characteristic diagram thereof, and Fig. 5 is an air 6 and 7 are sectional views showing different embodiments of the fuel injection valve in the vicinity of its main valve. 28... Air/fuel injection valve, 32... Fuel injection valve, 34... Electromagnetic solenoid, 56... Main valve, 70... Air pump, 78... Fuel pump, 90.90A. ...Fuel pipe serving as the auxiliary fuel supply system, 92...1ffn on-off valve. Patent applicant Yamaha Motor Co., Ltd.

Claims (1)

【特許請求の範囲】  燃料噴射弁から間欠的に噴射される燃料と所定圧の空
気との混合流を、主弁の開閉によって燃焼室内に間欠的
に噴射する空気・燃料噴射弁装置において、 前記主弁の上流側で燃料を連続的に供給する副燃料供給
系と、この副燃料供給系をエンジンの所定運転領域で作
動させる電磁開閉弁とを備えることを特徴とするエンジ
ンの空気・燃料噴射弁装置。
[Scope of Claims] An air/fuel injection valve device that intermittently injects a mixed flow of fuel intermittently injected from a fuel injection valve and air at a predetermined pressure into a combustion chamber by opening and closing a main valve, comprising: An air/fuel injection system for an engine characterized by comprising a sub-fuel supply system that continuously supplies fuel upstream of the main valve, and an electromagnetic on-off valve that operates the sub-fuel supply system in a predetermined operating range of the engine. Valve device.
JP25732990A 1990-09-28 1990-09-28 Air/fuel injection valve device for engine Pending JPH04136478A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP25732990A JPH04136478A (en) 1990-09-28 1990-09-28 Air/fuel injection valve device for engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP25732990A JPH04136478A (en) 1990-09-28 1990-09-28 Air/fuel injection valve device for engine

Publications (1)

Publication Number Publication Date
JPH04136478A true JPH04136478A (en) 1992-05-11

Family

ID=17304852

Family Applications (1)

Application Number Title Priority Date Filing Date
JP25732990A Pending JPH04136478A (en) 1990-09-28 1990-09-28 Air/fuel injection valve device for engine

Country Status (1)

Country Link
JP (1) JPH04136478A (en)

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