JPS5996464A - Carburetor - Google Patents

Carburetor

Info

Publication number
JPS5996464A
JPS5996464A JP57205130A JP20513082A JPS5996464A JP S5996464 A JPS5996464 A JP S5996464A JP 57205130 A JP57205130 A JP 57205130A JP 20513082 A JP20513082 A JP 20513082A JP S5996464 A JPS5996464 A JP S5996464A
Authority
JP
Japan
Prior art keywords
air
passage
air bleed
path
fuel
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
JP57205130A
Other languages
Japanese (ja)
Inventor
Toshiharu Ushiro
卯城 敏治
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.)
Honda Motor Co Ltd
Original Assignee
Honda 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 Honda Motor Co Ltd filed Critical Honda Motor Co Ltd
Priority to JP57205130A priority Critical patent/JPS5996464A/en
Publication of JPS5996464A publication Critical patent/JPS5996464A/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
    • F02M7/00Carburettors with means for influencing, e.g. enriching or keeping constant, fuel/air ratio of charge under varying conditions
    • F02M7/10Other installations, without moving parts, for influencing fuel/air ratio, e.g. electrical means
    • F02M7/103Other installations, without moving parts, for influencing fuel/air ratio, e.g. electrical means with self-acting equaliser jets
    • 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
    • F02M7/00Carburettors with means for influencing, e.g. enriching or keeping constant, fuel/air ratio of charge under varying conditions
    • F02M7/23Fuel aerating devices

Abstract

PURPOSE:To correct to make the air/fuel ratio rich by communicating the negative pressure lead-in path opening to a suction path at the upper straem than a throttle valve with an air bleed path while releasing a portion of bleed air to the suction path under heavy load high speed running. CONSTITUTION:Under heavy load high speed running where a throttle valve 7 will be high opening, secondary throttle valve 10 will open to inject fuel through secondary fuel nozzle 28 into small Venturi 9 in secondary suction path 3. Here negative pressure in large Venturi 4 in main suction path 2 is relatively high to flow a portion of air from an air bleed path 19 through negative pressure lead-in path 40 into large Venturi tube 4 thus to reduce the amount of air to be injected through an air jet 20 into an air bleed tube 12 and to increase the fuel injection by that amount to make rich. When providing an atmosphere responsive valve at the down stream from the coupling position of negative pressure lead-in path 40 and air bleed path 19, air-fuel ratio is prevented from going excessively rich.

Description

【発明の詳細な説明】 本発明は、気化器に関し、特に吸気道の途中に上流から
順にベンチュリおよび絞り弁を配設し、前記ベンチュリ
に開口した燃料ノズルを空気ブリード管を介して燃料室
に連通するとともに、前記空気ブリード管を空気ブリー
ド通路を介して前記吸気道の入口部に連通した気化器に
関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a carburetor, and in particular, a venturi and a throttle valve are disposed in the middle of an intake passage in order from upstream, and a fuel nozzle opened in the venturi is connected to a fuel chamber through an air bleed pipe. The present invention relates to a carburetor in which the air bleed pipe is communicated with the inlet portion of the intake passage through an air bleed passage.

従来のかかる気化器では、ブリード管の形状、ブリード
孔の位置およびその孔径を選択することにより、混合気
の空燃比特性を定めている。ところがこのような従来の
方法では、空燃比特性の傾きを変化させ\\Xs\〜對
畜動〜ることは容易であるが、絞り弁が高開度に開かれ
る内燃機関の高負荷、高速運転時のみに空燃比を小すな
わち混合気の燃料濃度を犬とするように補正することは
困難である。
In such a conventional carburetor, the air-fuel ratio characteristics of the air-fuel mixture are determined by selecting the shape of the bleed pipe, the position of the bleed hole, and the hole diameter. However, with such conventional methods, it is easy to change the slope of the air-fuel ratio characteristic, but it is difficult to change the slope of the air-fuel ratio characteristic at high loads and high speeds of internal combustion engines in which the throttle valve is opened at a high opening. It is difficult to correct the air-fuel ratio to a small value, that is, to reduce the fuel concentration of the air-fuel mixture only during operation.

本発明の第1の目的はかかる従来の技術的課題を解決し
、内燃機関の高負荷、高速運転時にのみ空気ブリード量
を減少して混合気の燃料濃度を大としうるようにした気
化器を提供することである。
The first object of the present invention is to solve such conventional technical problems, and to provide a carburetor that can increase the fuel concentration of the air-fuel mixture by reducing the amount of air bleed only during high-load, high-speed operation of an internal combustion engine. It is to provide.

ここで、上述のように内燃機関の高負荷、高速運転時に
空気ブリード量を低減するようにすると、高部などの大
気圧の低い場所においては、前記高負荷、高速運転時に
燃料濃度が必要以上に大となってしまうおそれがある。
As mentioned above, if the amount of air bleed is reduced during high load and high speed operation of the internal combustion engine, in places with low atmospheric pressure such as high altitudes, the fuel concentration will be higher than necessary during high load and high speed operation. There is a risk that it will become large.

そこで本発明の第2の目的は、大気圧の変動に拘らず、
内燃機関の高負荷、高速運転時の空燃比を適切に小とな
るように補正しうるようにした気化器を提供することで
ある。
Therefore, the second object of the present invention is to
An object of the present invention is to provide a carburetor that can appropriately correct the air-fuel ratio during high-load, high-speed operation of an internal combustion engine.

以下、図面により本発明の実施例について説明すると、
先ず第1図において、この気化器は複合型気化器であり
、気化器本体1には、主吸気道2および2次吸気道3が
並行して内設される。主吸気道2の途中には、大ベンチ
ユリ4が形成されるとともに、その大ベンチユリ4の上
流寄りに小ベンチユリ5が配設される。また気化器本体
1には、小ベンチユリ5の上流側でチョーク弁6が軸支
され、大ベンチユリ4の下流側で絞り弁7が軸支される
。一方、2次吸気道3の途中には大ベンチユリ8が形成
されるとともに、その大ベンチユリ8の上流寄りに小ベ
ンチユリ9が配設される。大ベンチユリ8の下流には、
機関の所定の高負荷、高速運転時に従来周知の負圧作動
器(図示せず)によって開放駆動される2次絞り弁10
が軸支される。
Hereinafter, embodiments of the present invention will be explained with reference to the drawings.
First, in FIG. 1, this carburetor is a composite type carburetor, and a main intake passage 2 and a secondary intake passage 3 are installed in a carburetor body 1 in parallel. A large bench lily 4 is formed in the middle of the main intake passage 2, and a small bench lily 5 is disposed upstream of the large bench lily 4. Further, in the carburetor body 1, a choke valve 6 is pivotally supported on the upstream side of the small bench lily 5, and a throttle valve 7 is pivotally supported on the downstream side of the large bench lily 4. On the other hand, a large bench lily 8 is formed in the middle of the secondary intake passage 3, and a small bench lily 9 is disposed upstream of the large bench lily 8. Downstream of large bench lily 8,
A secondary throttle valve 10 is driven to open by a conventionally well-known negative pressure actuator (not shown) during predetermined high-load, high-speed operation of the engine.
is pivoted.

主吸気道2における小ベンチユリ5には主燃料ノズル1
1が開口され、この主燃料ノズル11は空気ブリード管
12を外周する環状室13に連通ずる。環状室13は主
燃料ジェット14を介して燃料通路15に連通しておh
2燃料通路15はフロート16が収納された燃料室とし
てのフロート 5− 室17の燃料油面下に連通ずる。なお、主燃料ノズル1
1には、燃料噴出量を調節するための針状の燃料調節部
材18が挿入されている。
The main fuel nozzle 1 is installed in the small bench lily 5 in the main intake passage 2.
1 is open, and this main fuel nozzle 11 communicates with an annular chamber 13 surrounding an air bleed pipe 12 . The annular chamber 13 communicates with a fuel passage 15 via a main fuel jet 14.
The two fuel passages 15 communicate with the surface of a float chamber 17, which serves as a fuel chamber in which a float 16 is housed, below the fuel oil level. In addition, main fuel nozzle 1
1 has a needle-shaped fuel adjustment member 18 inserted therein for adjusting the amount of fuel jetted.

空気ブリード管12内に連通して空気ブリード通路19
が形成され、この空気ブリード通路19は主吸気道20
入口部、図示例ではチョーク弁6に近接しかつ該弁6の
閉弁時にその下流側となる個所で主吸気道2に開口する
。また空気ブリード通路19の途中で空気ブリード管1
2に近接した位置には、空気ブリード管12内へのブリ
ード空気の噴大量を規制するための空気ジェン)20が
配設される。さらに、空気ブリード通路19の主吸気道
2への開口位置付近には空気ブリード通路19への空気
の最大流入量を制限する空気ジェッート21が配設され
る。
An air bleed passage 19 communicates with the air bleed pipe 12.
is formed, and this air bleed passage 19 is connected to the main intake passage 20.
The inlet portion, in the illustrated example, opens into the main intake path 2 at a location close to the choke valve 6 and downstream of the choke valve 6 when the valve 6 is closed. Also, in the middle of the air bleed passage 19, the air bleed pipe 1
An air generator 20 for regulating the amount of bleed air jetted into the air bleed pipe 12 is disposed near the air bleed pipe 12 . Further, an air jet 21 is arranged near the opening position of the air bleed passage 19 to the main intake passage 2 to limit the maximum amount of air flowing into the air bleed passage 19.

前記燃料通路15はまた補助燃料ジェット22を介して
、空気ブリード管23を外周する環状室 6− 24に連通しており、この環状室24は大ベンチユリ4
よりも下流側の絞り弁7付近で主吸気道2に開口した低
速ノズル25に連通ずる。空気ブリード管23内は、空
気ジェット26および空気ブリード通路27を介して、
小ベンチユリ5よりも上流側で主吸気道2に連通ずる。
The fuel passage 15 also communicates via an auxiliary fuel jet 22 with an annular chamber 6-24 surrounding the air bleed pipe 23, which is connected to the large bench lily 4.
It communicates with a low-speed nozzle 25 that opens into the main intake path 2 near the throttle valve 7 on the downstream side. Inside the air bleed pipe 23, via an air jet 26 and an air bleed passage 27,
It communicates with the main intake path 2 on the upstream side of the small bench lily 5.

2次吸気道3に関しても上述の主吸気道2と同様に、小
ベンチユリ9に2次燃料ノズル28が開口し、この2次
燃料ノズル28は空気ブリード管29を外囲する環状室
30に連通ずる。また環状室30は燃料通路31および
2次燃料ジェット32を介してフロート室11の底部に
連通ずる。さらに空気ブリード管29内は空気ブリード
通路33および2次空気ジェット34を介して2次吸気
道3の上流端に連通ずる。さらに2次吸気道3の小ベン
チユリ9より下流の絞り弁10付近には、低速ノズル3
5が開口し、この低速ノズル35は通路36および空気
ジェット31を介して2次吸気道3の上流端に連通する
。この通路36の途中に臨んで補助燃料ジェット38が
配設されており、この補助燃料ジェット38は燃料通路
39を介してフロート室1γの燃料油面下に連通する。
As for the secondary intake passage 3, similarly to the above-mentioned main intake passage 2, a secondary fuel nozzle 28 opens in the small bench lily 9, and this secondary fuel nozzle 28 communicates with an annular chamber 30 surrounding an air bleed pipe 29. It goes through. The annular chamber 30 also communicates with the bottom of the float chamber 11 via a fuel passage 31 and a secondary fuel jet 32. Further, the inside of the air bleed pipe 29 communicates with the upstream end of the secondary intake passage 3 via an air bleed passage 33 and a secondary air jet 34. Furthermore, a low-speed nozzle 3 is located near the throttle valve 10 downstream of the small bench lily 9 of the secondary intake path 3.
5 is open, and this low-velocity nozzle 35 communicates with the upstream end of the secondary intake passage 3 via a passage 36 and an air jet 31. An auxiliary fuel jet 38 is disposed facing the middle of this passage 36, and this auxiliary fuel jet 38 communicates with the surface of the fuel oil in the float chamber 1γ via a fuel passage 39.

このような複合型気化器において、本発明に従えば、主
吸気道2で機関の高負荷、高速運転時に負圧が犬となる
部分すなわち絞り弁1よりも上流側の個所に開口して負
圧導入路4oが設けられる。
In such a compound carburetor, according to the present invention, the main intake path 2 is opened at a portion of the main intake path 2 where negative pressure is generated during high-load and high-speed operation of the engine, that is, at a location upstream of the throttle valve 1. A pressure introduction path 4o is provided.

すなわちこの実施例では、大ベンチユリ4の内面に開口
して負圧導入路40が設けられ、この負圧導入路40は
空気ブリード通路19における空気ジェット20よりも
上流側に連結される。また負圧導入路40には、主吸気
道2からの負圧の導入量を規制する空気ジェット41が
配設される。
That is, in this embodiment, a negative pressure introduction path 40 is provided opening on the inner surface of the large bench lily 4, and this negative pressure introduction path 40 is connected to the air bleed passage 19 upstream of the air jet 20. Further, an air jet 41 that regulates the amount of negative pressure introduced from the main intake path 2 is arranged in the negative pressure introduction path 40 .

次にこの実施例の作用を説明すると、絞り弁γの開度が
小さい機関の低負荷運転時には絞り弁7が開放され、空
気ブリード管12のブリード孔42から環状室13内の
燃料に空気がブリードされる。
Next, the operation of this embodiment will be explained. During low load operation of the engine with a small opening degree of the throttle valve γ, the throttle valve 7 is opened, and air flows into the fuel in the annular chamber 13 from the bleed hole 42 of the air bleed pipe 12. be bred.

それによってエマルジョン化した燃料は主燃料ノズル1
1から小ベンチユリ5内に吸引噴出されて混合気が形成
される。なお機関の低負荷運転時には、大ベンチユリ4
の内面付近の負圧は比較的小さい。そのため負圧導入路
40から空気ブリード通路19に作用する負圧は極めて
弱く、したがって空気ジェット20を介してブリードさ
れる空気量は従来と同程度に維持されて所定の空燃比の
混合気が得られる。
The emulsified fuel is then transferred to the main fuel nozzle 1.
1 into the small bench lily 5 to form an air-fuel mixture. In addition, when operating the engine at low load, the large bench lily 4
The negative pressure near the inner surface of is relatively small. Therefore, the negative pressure acting on the air bleed passage 19 from the negative pressure introduction passage 40 is extremely weak, and therefore the amount of air bleed through the air jet 20 is maintained at the same level as before, and a mixture of a predetermined air-fuel ratio is obtained. It will be done.

絞り弁Tが高開度に開かれて機関が高負荷、高速運転状
態に達すると、2次絞り弁10が開放され、それに応じ
て2次燃料ノズル28から2次吸気道3の小ベンチユリ
9内にエマルジョン化した燃料が噴出されることによっ
て、混合気が形成される。したがって、機関には主吸気
道2および29 − 火成気道3から混合気が供給されることになる。
When the throttle valve T is opened to a high opening degree and the engine reaches a high-load, high-speed operating state, the secondary throttle valve 10 is opened, and accordingly, the secondary fuel nozzle 28 is opened to the small bench lily 9 of the secondary intake path 3. An air-fuel mixture is formed by ejecting the emulsified fuel inside. Therefore, the engine is supplied with air-fuel mixture from the main intake duct 2 and the 29-igneous air duct 3.

このような高負荷、高速運転時に、主吸気道2における
大ベンチユリ4の内面付近の負圧は比較的太となる。そ
のため、その負圧が負圧導入路40を介して空気ブリー
ド通路19に強く作用し、その結果空気ブリード通路1
9を流れる空気の一部は、負圧導入路40を経て大ベン
チユリ4に流れることになり、空気ジェット20を介し
て空気ブリード管12内に噴入されるブリード空気の量
が減少し、その分だけ燃料の噴出量が大となる。したが
って、機関の高負荷、高速運転時において、混合気の燃
料濃度が大とされ、すなわち空燃比が汁となる方向に補
正されることになる。
During such high-load, high-speed operation, the negative pressure near the inner surface of the large bench lily 4 in the main intake passage 2 becomes relatively large. Therefore, the negative pressure acts strongly on the air bleed passage 19 through the negative pressure introduction passage 40, and as a result, the air bleed passage 19
A part of the air flowing through the air 9 flows into the large bench lily 4 via the negative pressure introduction path 40, and the amount of bleed air injected into the air bleed pipe 12 through the air jet 20 is reduced. The amount of fuel ejected increases accordingly. Therefore, when the engine is operated under high load and at high speed, the fuel concentration of the air-fuel mixture is increased, that is, the air-fuel ratio is corrected to become lean.

次に第2の発明の一実施例について説明すると、第2図
において、空気ブリード通路19における負圧導入路4
0との連結位置43よりも下流側であってかつ空気ジェ
ット20よりも上流側には、10− 大気圧応動弁44が配設される。なお、その他の構成に
ついては、第1図示の実施例と同様であり、対応する部
分には同一の参照符号を付す。
Next, an embodiment of the second invention will be described. In FIG.
An atmospheric pressure responsive valve 44 is disposed downstream of the connection position 43 with the air jet 20 and upstream of the air jet 20. Note that the other configurations are the same as those of the embodiment shown in the first figure, and corresponding parts are given the same reference numerals.

大気圧応動弁44は、透孔45を介して大包に連通した
空間46を形成するケーシング47と、そのケーシング
47の内面に固着され予め一定量の気体が封入された伸
縮自在のベローズ体 48と、とのベローズ体48に該
ベローズ体48の伸縮方向に延びて固着された弁棒49
と、弁棒49に固着され弁孔50の開度を定める弁体5
1とを含む。空間46と空気ブリード通路19との間は
弁棒49の外面に摺接するシール部材52でシールされ
ている。
The atmospheric pressure responsive valve 44 includes a casing 47 that forms a space 46 that communicates with the large package through a through hole 45, and an expandable bellows body 48 that is fixed to the inner surface of the casing 47 and is filled with a certain amount of gas in advance. and a valve stem 49 fixed to the bellows body 48 extending in the direction of expansion and contraction of the bellows body 48.
and a valve body 5 which is fixed to the valve stem 49 and determines the opening degree of the valve hole 50.
1. The space 46 and the air bleed passage 19 are sealed by a sealing member 52 that slides on the outer surface of the valve stem 49.

このような大気圧応動弁44では、大気圧が低下して空
間46の圧力が低下すると、ベローズ体48が、その内
部の圧力と前記空間46の圧力とがバランスするまで、
伸長し、それによって弁孔50の開度が大となる。した
がって、空気プIJ −ド通路19から空気ジェット2
0を介してブリード管12内にブリードされる空気量が
比較的太となる。これとは逆に大気圧が上昇すると、ベ
ローズ体48が収縮して弁孔50の開度が小となり、空
気ジェット20からブリード管12内にブリードされる
空気量が比較的太となる。
In such an atmospheric pressure responsive valve 44, when the atmospheric pressure decreases and the pressure in the space 46 decreases, the bellows body 48 operates until the internal pressure and the pressure in the space 46 are balanced.
The valve hole 50 expands, thereby increasing the opening degree of the valve hole 50. Therefore, the air jet 2 from the air jet passage 19
The amount of air bleed into the bleed pipe 12 through 0 becomes relatively large. Conversely, when the atmospheric pressure increases, the bellows body 48 contracts, the opening degree of the valve hole 50 becomes small, and the amount of air bleed from the air jet 20 into the bleed pipe 12 becomes relatively large.

したがってこの実施例によれば、高地などの大気圧が低
い場所で、内燃機関の高負荷、高速運転時にブリード空
気供給量が減少し過ぎて、空燃比が必要以上に小となる
ことが防止される。
Therefore, according to this embodiment, it is possible to prevent the air-fuel ratio from becoming unnecessarily small due to an excessive decrease in the amount of bleed air supplied when the internal combustion engine is operated at high load and high speed in places with low atmospheric pressure such as at high altitudes. Ru.

本発明は、上述の実施例のような複合型気化器だけでな
く単一の吸気道を有する気化器に関連して実施すること
もでき、さらに吸気道の途中に単一のベンチュリを有す
る気化器に関連しても実施することができる。
The present invention can be implemented not only in conjunction with a compound carburetor as in the embodiments described above, but also in connection with a carburetor having a single intake passage, and furthermore, in connection with a carburetor having a single venturi in the middle of the intake passage. It can also be implemented in relation to vessels.

以上のように本発明によれば、空気ブリード通路に、絞
り弁よりも上流側の吸気道に開口した負圧導入路を連結
したので、内燃機関の高負荷、高速運転時にブリード空
気の一部が負圧導入路を介して吸気道に逃されるように
なり、したがって前記高負荷、高速運転時にのみ空燃比
を小すなわち燃料濃度を大とする補正を行なうことがで
きる。
As described above, according to the present invention, the air bleed passage is connected to the negative pressure introduction passage which opens to the intake passage on the upstream side of the throttle valve. is released into the intake passage through the negative pressure introduction path, and therefore, correction can be made to reduce the air-fuel ratio, that is, increase the fuel concentration, only during the high-load, high-speed operation.

また第2の発明によれば、負圧導入路との連結位置より
も下流側における空気ブリード通路の途中に、大気圧が
低下するのに応じて開度が大となる大気圧応動弁を設け
たので、大気圧が低下した場合の内燃機関高負荷、高速
運転時に混合気の燃料濃度が必要以上に濃くなることが
防止される。
Further, according to the second invention, an atmospheric pressure responsive valve is provided in the middle of the air bleed passage on the downstream side of the connection position with the negative pressure introduction passage, the opening degree of which increases as the atmospheric pressure decreases. Therefore, the fuel concentration of the air-fuel mixture is prevented from becoming richer than necessary when the internal combustion engine is operated under high load and at high speed when the atmospheric pressure decreases.

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

図面は本発明の実施例を示すものであり、第1図は本発
明の一実施例の縦断正面図、第2図は第2発明の一実施
例の要部のみの縦断正面図である。 2・・・主吸気道、4・・・大ベンチユリ、5・・・小
ペン13− チュリ、7・・・絞゛り弁、11・・・主燃料ノズル、
12・・・空気ブリード管、13・・・環状室、15・
・・燃料通路、17・・・フロート室、19・・・空気
ブリード通路、40・・・負圧導入路、43・・・連結
位置、44・・・大気圧応動弁 特許出願人 本田技研工業株式会社 14−
The drawings show embodiments of the present invention, and FIG. 1 is a longitudinal sectional front view of one embodiment of the invention, and FIG. 2 is a longitudinal sectional front view of only essential parts of an embodiment of the second invention. 2...Main intake duct, 4...Large bench lily, 5...Small pen 13-churi, 7...Throttle valve, 11...Main fuel nozzle,
12... Air bleed pipe, 13... Annular chamber, 15...
...Fuel passage, 17...Float chamber, 19...Air bleed passage, 40...Negative pressure introduction path, 43...Connection position, 44...Atmospheric pressure responsive valve patent applicant Honda Motor Co., Ltd. Co., Ltd. 14-

Claims (1)

【特許請求の範囲】 (])吸気道の途中に」二流から順にベンチュリおよび
絞り弁を配設し、前記ベンチュリに開口した燃料ノズル
を空気ブリード管を介して燃料室に連通するとともに、
前記空気ブリード管を空気ブリード通路を介して前記吸
気道の入口部に連通した気化器において、前記絞り弁よ
り上流の前記吸気道に開口し、かつ前記空気ブリード通
路に連結される負圧導入路が設けられることを特徴とす
る気化器。 (2)吸気道の途中に上流側から順にベンチュリおよび
絞り弁を配設し、前記ベンチュリに開口した燃料ノズル
を空気ブリード管を介して燃料室に連通ずるとともに、
前記空気ブリード管を空気ブリード通路を介して前記吸
気道の入口部に連通した気化器において、前記絞り弁よ
り上流の前記吸気道に開口し、かつ前記空気ブリード通
路に連結される負圧導入路が設けられ、前記負圧導入路
との連結位置よりも下流側における空気ブリード通路に
は、大気圧が小となるのに応じて開度が大となる大気圧
応動弁が配設されることを特徴とする気化器。
[Scope of Claims] (]) A venturi and a throttle valve are disposed in order from the second flow in the middle of the intake passage, and a fuel nozzle opened in the venturi is communicated with the fuel chamber via an air bleed pipe,
In a carburetor in which the air bleed pipe is communicated with an inlet of the intake passage through an air bleed passage, a negative pressure introduction passage opens into the intake passage upstream from the throttle valve and is connected to the air bleed passage. A vaporizer characterized by being provided with. (2) A venturi and a throttle valve are disposed in order from the upstream side in the middle of the intake passage, and the fuel nozzle opened in the venturi is communicated with the fuel chamber via an air bleed pipe,
In a carburetor in which the air bleed pipe is communicated with an inlet of the intake passage through an air bleed passage, a negative pressure introduction passage opens into the intake passage upstream from the throttle valve and is connected to the air bleed passage. The air bleed passage downstream of the connection position with the negative pressure introduction passage is provided with an atmospheric pressure responsive valve whose opening degree increases as the atmospheric pressure decreases. A vaporizer featuring:
JP57205130A 1982-11-22 1982-11-22 Carburetor Pending JPS5996464A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP57205130A JPS5996464A (en) 1982-11-22 1982-11-22 Carburetor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP57205130A JPS5996464A (en) 1982-11-22 1982-11-22 Carburetor

Publications (1)

Publication Number Publication Date
JPS5996464A true JPS5996464A (en) 1984-06-02

Family

ID=16501924

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57205130A Pending JPS5996464A (en) 1982-11-22 1982-11-22 Carburetor

Country Status (1)

Country Link
JP (1) JPS5996464A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2023034365A1 (en) * 2021-09-01 2023-03-09 American CNG, LLC Supplemental fuel system for compression-ignition engine

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS55101751A (en) * 1979-01-26 1980-08-04 Hitachi Ltd Atmospheric pressure adjusting device for carburetor

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS55101751A (en) * 1979-01-26 1980-08-04 Hitachi Ltd Atmospheric pressure adjusting device for carburetor

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2023034365A1 (en) * 2021-09-01 2023-03-09 American CNG, LLC Supplemental fuel system for compression-ignition engine
US11739716B2 (en) 2021-09-01 2023-08-29 American CNG, LLC Supplemental fuel system for compression-ignition engine
US11767811B2 (en) 2021-09-01 2023-09-26 American CNG, LLC Supplemental fuel system for compression-ignition engine
US11808221B2 (en) 2021-09-01 2023-11-07 American CNG, LLC Supplemental fuel system for compression-ignition engine
US11835016B2 (en) 2021-09-01 2023-12-05 American CNG, LLC Supplemental fuel system for compression-ignition engine

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