JPS5857059A - Carburetor - Google Patents

Carburetor

Info

Publication number
JPS5857059A
JPS5857059A JP15536081A JP15536081A JPS5857059A JP S5857059 A JPS5857059 A JP S5857059A JP 15536081 A JP15536081 A JP 15536081A JP 15536081 A JP15536081 A JP 15536081A JP S5857059 A JPS5857059 A JP S5857059A
Authority
JP
Japan
Prior art keywords
fuel
throttle valve
suction
negative pressure
outlet
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
JP15536081A
Other languages
Japanese (ja)
Inventor
Takao Shindo
新藤 孝男
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.)
Nippon Carburetor Co Ltd
Original Assignee
Nippon Carburetor 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 Nippon Carburetor Co Ltd filed Critical Nippon Carburetor Co Ltd
Priority to JP15536081A priority Critical patent/JPS5857059A/en
Publication of JPS5857059A publication Critical patent/JPS5857059A/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
    • F02M3/00Idling devices for carburettors
    • F02M3/08Other details of idling devices
    • F02M3/12Passageway systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of The Air-Fuel Ratio Of Carburetors (AREA)

Abstract

PURPOSE:To prevent the main fuel from being fed too late by providing an auxiliary fuel passage with its inlet directly opened to a constant oil level chamber and with its outlet opened to the portion between a venturi and throttle valve of a suction path in a carburetor with a main channel and low speed channel in a common form. CONSTITUTION:During the fuel feed, when the aperture of a throttle valve 3 is something like idling, the low speed fuel is sucked into a suction path 1 through the slow port 12 and idle port 13 of a low speed channel 6. When the aperture of the throttle valve 3 is increased and the outlet 19b of the auxiliary fuel passage 19 is located downstream the throttle valve 3, the fuel is fed from the inlet 19a opened to the constant oil level chamber 4 at a suction quantity corresponding to the suction negative pressure and the aperture area of the outlet 19b downstream the throttle valve 3. When the aperture of the throttle valve 3 is further increased and the venturi negative pressure is larger than the suction negative pressure, the fuel is gradually sucked into the suction path 1 through a main nozzle 8, and the negative pressure downstream the throttle valve 3 is made comparatively low, thereby the suction quantity from the outlet 19b is decreased.

Description

【発明の詳細な説明】 本発明は主燃料出始めの時期において要求燃料流量を正
確に供給することができる気化器に関するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a carburetor that can accurately supply the required fuel flow rate at the beginning of main fuel output.

気化器の燃料系統は周知のように、主ジェツトの下流に
おいて主系統の燃料通路から低速系統の燃料通路を分岐
させた共通形のものと、恒油面室へ低速系統の燃料通路
を1a接接続させた独立形のものとがある。
As is well known, the carburetor fuel system is of a common type, in which the low-speed system fuel passage is branched from the main system fuel passage downstream of the main jet, and the low-speed system fuel passage is connected to the constant oil level chamber at 1a. There are connected and independent types.

現在の自動車エンジンの気化器の殆んどは共通形の燃料
系統を採用して居り、主ジェツトを通過した燃料は両系
統の燃料通路に作用する負圧の高低に応じて低速燃料と
主燃料とに分配される。そして、共通形のものでは両系
統は圧力バランスを保ち燃料の制御が容易に行われると
いう利点を具えている反面、主燃料の出始めにおいて低
速系統の負圧力が強いと出遅れる傾向があり、特に吸入
空気量に対してベンチュリ径が大きい気化器では主系統
の燃料通路に作用する負圧が吸入空気量に対応して高く
ならないので主燃料の出遅れが著しく、このため一時的
な燃料不足を生じる。
Most of the carburetors of current automobile engines use a common fuel system, and the fuel that has passed through the main jet is switched between low-speed fuel and main fuel depending on the level of negative pressure acting on the fuel passages of both systems. distributed to In the common type, both systems have the advantage of maintaining pressure balance and making fuel control easy, but on the other hand, if the negative pressure in the low-speed system is strong at the beginning of the main fuel flow, there is a tendency to lag, especially when the main fuel starts to flow. In a carburetor whose venturi diameter is large relative to the amount of intake air, the negative pressure acting on the fuel passage in the main system does not increase in proportion to the amount of intake air, so there is a significant delay in the main fuel supply, resulting in a temporary fuel shortage. .

この不足分を低速系統で補うようにすると低速系統の負
圧力゛′がそれだけ強く作用するようになり、主燃料が
史に出遅れるという悪循環を招く。
If this shortage is compensated for by the low-speed system, the negative pressure '' of the low-speed system will act more strongly, leading to a vicious cycle in which the main fuel will fall behind.

本発明は、主系統と低速系統とが共通形の気化器がもっ
ているこれらの問題点を解決し。
The present invention solves these problems of a carburetor in which the main system and the low speed system are common.

エンジンが要求する燃料流量が正確に得られる気化器を
提供することを目的とするもので。
The purpose is to provide a carburetor that can accurately obtain the fuel flow rate required by the engine.

入口な恒油面室に直接開口すると共に出口を吸気路のベ
ンチエリと絞り弁との間の部分に開口した補助燃料通路
を設けたことを特徴とするものである。
The present invention is characterized in that an auxiliary fuel passage is provided, which opens directly into the constant oil level chamber as an inlet, and whose outlet opens in a portion of the intake passage between the bench area and the throttle valve.

以下本発明の実施例を図面に就いて説明すると、第1図
においてlは下向きの吸気路。
Embodiments of the present invention will be described below with reference to the drawings. In FIG. 1, l represents a downward air intake path.

2はベンチュリ、3は絞り弁、4は恒油面室。2 is a venturi, 3 is a throttle valve, and 4 is a constant oil level chamber.

5は主系統、6は低速系統であって、主系統5は主ジェ
ツト7から主ノズル8へ至る燃料通路9に主空気ブリー
ドジエツ)10およびエマルジョン管11を設けて構成
されている。また、低速系統6は主系統5の主ジェツト
7の下流において燃料通路9から分岐してスローボート
12.アイドルボー)13へ至る燃料通路14に低速ジ
エツ) 15.第一低速空気ブリードジェット16.エ
コノマイザ17.第二低速空気ブリードジエツ)18を
設けて構成されている。
Reference numeral 5 indicates a main system, and 6 indicates a low speed system. Further, the low-speed system 6 branches from the fuel passage 9 downstream of the main jet 7 of the main system 5, and is branched from the slow boat 12. Low speed jets in the fuel passage 14 leading to the idle board) 13) 15. First low speed air bleed jet 16. Economizer 17. A second low-velocity air bleed jet 18 is provided.

前記燃料系統とは別個に補助燃料通路19が設けられ、
その人口19aは恒油面室4に直接開口していると共に
出口19bは吸気路lのベンチュリ2と絞り弁3との間
の部分に開口し。
An auxiliary fuel passage 19 is provided separately from the fuel system,
The port 19a opens directly into the constant oil level chamber 4, and the outlet 19b opens into a portion of the intake path 1 between the venturi 2 and the throttle valve 3.

またこの通路19は燃料ジェット20.第一の空気ブリ
ードジェット21.エコノマイザ22.第二の空気ブリ
ードジェット23を具えている。
This passage 19 also has a fuel jet 20. First air bleed jet 21. Economizer 22. A second air bleed jet 23 is provided.

出°口19bはエンジンの要求燃料流量に対応して主燃
料が出始めるべきときに開口の一部が絞り弁3の下流側
となる位置に設けるのがよ〈、また二段二連気化器など
のように二段側気化器を具えているときは二段側絞り弁
開き始めにおいて開口の全部が絞り弁3の下流側となる
位置とする。
The outlet 19b is preferably provided at a position where a part of the opening is downstream of the throttle valve 3 when the main fuel starts to come out in accordance with the fuel flow rate required by the engine. When a second-stage vaporizer is provided, such as in the case of a second-stage throttle valve, the opening is all located downstream of the throttle valve 3 when the second-stage throttle valve begins to open.

このように構成した本実施列は、絞り弁3が例えばアイ
ドリンク開度程度の小さい開度であって吸入空気量が少
なく且つ吸入負圧が高い低速回転域においては低速系統
6のスローボート12.アイドルポート13から低速燃
料が供給され、これより絞り弁3の開度が次第に大きく
なり補助燃料通路19の出口19bが絞り弁3の下流側
へ開口するようになると恒油面室4から送られる燃料が
吸出されるようになり、この吸出し旨は吸入負圧、、出
口19bの絞り弁下流側の開口面積によって決定されろ
In this embodiment array configured in this way, the slow boat 12 of the low speed system 6 is used when the throttle valve 3 is at a small opening, such as the idle link opening, and the intake air amount is small and the intake negative pressure is high in the low speed rotation range. .. Low-speed fuel is supplied from the idle port 13, and when the opening degree of the throttle valve 3 gradually increases and the outlet 19b of the auxiliary fuel passage 19 opens downstream of the throttle valve 3, it is sent from the constant oil level chamber 4. Fuel is now being sucked out, and this suction is determined by the suction negative pressure and the opening area of the outlet 19b on the downstream side of the throttle valve.

絞り弁3の開度が更に大きくなり吸入負圧よりもベンチ
ュリ負圧の方が高くなると吸気路lKは主に主燃料が吸
出されるようになり。
When the opening degree of the throttle valve 3 becomes larger and the venturi negative pressure becomes higher than the suction negative pressure, the main fuel will mainly be sucked out from the intake passage lK.

このとき吸気路lの絞り弁下流側の負圧は絞り弁開度が
小さいときに比べ低ぐflっているので補助燃料通路1
9からの吸出し量は主燃料吸出し始めの頃よりも減少し
ている。
At this time, the negative pressure on the downstream side of the throttle valve in the intake passage 1 is lower than when the opening degree of the throttle valve is small, so the auxiliary fuel passage 1
The amount of suction from No. 9 has decreased compared to when the main fuel suction started.

第2図は吸入負圧を一定(−4sogH7)としたとき
の共通形の燃料系統からの、燃料流量(8曲1)、補助
燃料通路19からの燃料流量(C曲線)および総合燃料
流量(A曲線)の吸入空気量に対する変化の状況を示゛
した図であって、共通形のものが一時的な燃料不足を生
じるときこれを補助燃料が補うことが示されている。こ
の場合、A曲線から判るように燃料流量は心壁以上に増
大するので主ジェツト7の径を従来よりも小さくして正
規の燃料系統を通る燃料流量を減少させ、A曲線をエン
ジン要求燃料流量(曲線D)とほぼ一致させることがで
きる。また、補助燃料が出始めたとき主燃料が同時に吸
出され混合気を過濃とすることがないように吸入空気量
に対してベンチュリ径を大きくシ、または低速系統6を
吸入負圧が強く作用する構成とし、主燃料出始め時期を
故意に遅れさせることによって補助燃料の効果を高める
ことができる。
Figure 2 shows the fuel flow from the common fuel system (8 tracks 1), the fuel flow from the auxiliary fuel passage 19 (C curve), and the total fuel flow ( FIG. 3 is a diagram showing how the intake air amount changes in curve A), and shows that when the common type suffers from a temporary fuel shortage, auxiliary fuel compensates for this. In this case, as can be seen from curve A, the fuel flow rate increases beyond the core wall, so the diameter of the main jet 7 is made smaller than before to reduce the fuel flow rate passing through the regular fuel system, and curve A is changed to the engine required fuel flow rate. (curve D). Also, in order to prevent the main fuel from being sucked out at the same time when the auxiliary fuel starts to come out, making the mixture too rich, the venturi diameter should be made large relative to the amount of intake air, or the intake negative pressure should strongly act on the low speed system 6. The effect of the auxiliary fuel can be increased by deliberately delaying the start of the main fuel.

このように本発明によると、従来の独立形低速系統と同
様の構成をもつ補助燃料通路を共通形の燃料系統とは全
く別個に設け、この通路の出口を吸気路のベンチュリと
絞り弁との間の部分に開口したことによって、主燃料の
出遅れを補助燃料通路からの燃料で補いエンジンが要求
する燃料流量が正確に得られるものである。
As described above, according to the present invention, an auxiliary fuel passage having the same configuration as a conventional independent low-speed system is provided completely separately from the common type fuel system, and the outlet of this passage is connected to the venturi of the intake passage and the throttle valve. By opening in the area between the two, the delay in the main fuel flow can be compensated for by the fuel from the auxiliary fuel passage, and the fuel flow rate required by the engine can be accurately obtained.

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

第1図は本発明の実施例を示す縦断面図。 第2図は吸入空気量と燃料流量との関係を示す図である
。 l・・・・・・吸気路、2・・・・・・ベンチュリ、3
・・・・・・絞り弁、4・・・・・・恒油面室、5・・
・・・・主系統、6・・・・・・低速系統、19・・・
・・・補助燃料通路、 19m・・・・・・人口、19
b・・・・・・出口、20・・・・・・燃料ジェット。 21.2390.10.空気ブリードジェット、22・
・・・・・エコノマイザ。 代理人野沢睦秋
FIG. 1 is a longitudinal sectional view showing an embodiment of the present invention. FIG. 2 is a diagram showing the relationship between intake air amount and fuel flow rate. l...Intake path, 2...Venturi, 3
... Throttle valve, 4... Constant oil level chamber, 5...
...Main system, 6...Low speed system, 19...
...Auxiliary fuel passage, 19m ...Population, 19
b...Exit, 20...Fuel jet. 21.2390.10. Air bleed jet, 22・
...Economizer. Agent Mutsuaki Nozawa

Claims (1)

【特許請求の範囲】[Claims] 主系統と低速系統とが共通形の気化器において、入口が
恒油面室に直接開口し出口が吸気路のベンチュリと絞り
升との間の部分に開口した補助燃料通路を具えたことを
特徴とする気化器。
A carburetor in which the main system and low-speed system are common, characterized by having an auxiliary fuel passage whose inlet opens directly into the constant oil level chamber and whose outlet opens in the portion of the intake path between the venturi and the throttle box. vaporizer.
JP15536081A 1981-09-30 1981-09-30 Carburetor Pending JPS5857059A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP15536081A JPS5857059A (en) 1981-09-30 1981-09-30 Carburetor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP15536081A JPS5857059A (en) 1981-09-30 1981-09-30 Carburetor

Publications (1)

Publication Number Publication Date
JPS5857059A true JPS5857059A (en) 1983-04-05

Family

ID=15604202

Family Applications (1)

Application Number Title Priority Date Filing Date
JP15536081A Pending JPS5857059A (en) 1981-09-30 1981-09-30 Carburetor

Country Status (1)

Country Link
JP (1) JPS5857059A (en)

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