JPH0835448A - Membrane carburetor fuel passage structure - Google Patents
Membrane carburetor fuel passage structureInfo
- Publication number
- JPH0835448A JPH0835448A JP19188294A JP19188294A JPH0835448A JP H0835448 A JPH0835448 A JP H0835448A JP 19188294 A JP19188294 A JP 19188294A JP 19188294 A JP19188294 A JP 19188294A JP H0835448 A JPH0835448 A JP H0835448A
- Authority
- JP
- Japan
- Prior art keywords
- fuel
- speed
- passage
- injection hole
- low
- 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
Landscapes
- Control Of The Air-Fuel Ratio Of Carburetors (AREA)
Abstract
(57)【要約】
【目的】 高速燃料噴孔の吸気負圧が低速燃料系統へ作
用するのを弱めることにより、機関の中速運転域で燃料
量が不足するのを防止する。
【構成】 一端が定圧燃料室25に連通し他端が高速燃
料噴孔51を経て吸気通路16に開口する通路を気化器
本体15に備える。高速燃料噴孔51の定圧燃料室25
に隣接する上流側端部に固定ジエツト46を設け、固定
ジエツト46の下流側通路を第1、第2の燃料系統に分
岐する。第1の燃料系統は固定ジエツト46で計量され
た燃料の一部を、低速燃料通路36を経て低速燃料噴孔
20から吸気通路16へ噴出する。第2の燃料系統は固
定ジエツト46で計量された燃料の残部を、絞り43を
経て高速燃料噴孔51から吸気通路16のベンチユリ部
16aへ噴出する。絞り43は固定ジエツト46とほぼ
同径にする。
(57) [Abstract] [Purpose] To prevent the intake negative pressure of the high-speed fuel injection hole from acting on the low-speed fuel system to prevent the fuel amount from becoming insufficient in the medium-speed operation range of the engine. A carburetor main body 15 is provided with a passageway, one end of which communicates with the constant pressure fuel chamber 25 and the other end of which opens into the intake passage 16 through the high-speed fuel injection hole 51. Constant-pressure fuel chamber 25 of high-speed fuel injection hole 51
A fixed jet 46 is provided at an upstream end portion adjacent to, and a downstream passage of the fixed jet 46 is branched into a first fuel system and a second fuel system. The first fuel system ejects a part of the fuel measured by the fixed jet 46 from the low-speed fuel injection hole 20 to the intake passage 16 via the low-speed fuel passage 36. The second fuel system injects the rest of the fuel measured by the fixed jet 46 from the high-speed fuel injection hole 51 through the throttle 43 to the bench lily portion 16a of the intake passage 16. The diaphragm 43 has substantially the same diameter as the fixed jet 46.
Description
【0001】[0001]
【産業上の利用分野】本発明は膜型気化器の同系統式燃
料通路構造、特に機関の低速運転域と高速運転域との中
間の運転域、つまり低速運転域から高速運転域へ移る中
速運転域で燃料量が相対的に少くなる(薄くなる)のを
防止する、膜型気化器の同系統式燃料通路構造に関する
ものである。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a fuel passage structure of the same system of a membrane carburetor, and more particularly, to an operating range intermediate between the low speed operating range and the high speed operating range of an engine, that is, from the low speed operating range to the high speed operating range. The present invention relates to the same type fuel passage structure of a membrane carburetor, which prevents the fuel amount from becoming relatively small (thinner) in a high speed operation range.
【0002】[0002]
【従来の技術】低速燃料調整機構と高速燃料調整機構を
備える膜型気化器には、定圧燃料室から低速燃料室へ至
る通路と、定圧燃料室から高速燃料室へ至る通路とが別
になつている別系統式燃料通路のものと、定圧燃料室か
らの通路が高速燃料調整機構を経て高速燃料室へ連通
し、さらに高速燃料調整機構から低速燃料調整機構を経
て低速燃料室へ連通する同系統式燃料通路のものとがあ
り、2行程機関ではピストンポート型、リードバルブ
型、ロータリバルブ型などの吸気・燃料系統の特性に応
じた使い分けをしている。2. Description of the Related Art In a membrane carburetor having a low speed fuel adjusting mechanism and a high speed fuel adjusting mechanism, a passage from a constant pressure fuel chamber to a low speed fuel chamber and a passage from a constant pressure fuel chamber to a high speed fuel chamber are separately provided. Another system type fuel passage and a passage from the constant pressure fuel chamber communicate with the high speed fuel chamber through the high speed fuel adjustment mechanism, and further communicate with the low speed fuel chamber through the high speed fuel adjustment mechanism through the low speed fuel adjustment mechanism. There is a type of fuel passage, and in a two-stroke engine, a piston port type, a reed valve type, a rotary valve type, etc. are used properly according to the characteristics of the intake / fuel system.
【0003】ところで、動力鋸や刈払機などの携帯作業
機にも排ガス規制が適用されることになると、寒冷地、
高地などの運転環境に応じて低速燃料調整機構を再調整
する必要がある携帯作業機では、排ガス規制の対応が難
しくなる。別系統式燃料通路の気化器では、低速燃料調
整機構の通路と高速燃料調整機構の通路が独立している
ので、図4に破線で示す通常の調整位置から、例えば高
地運転のために、低速燃料調整機構を調整して燃料量を
多くすると、高速燃料調整機構が影響を受け、図4に実
線で示すように、機関の高速運転での燃料量も増加す
る。By the way, when exhaust gas regulations are applied to portable working machines such as power saws and brush cutters,
It is difficult to comply with exhaust gas regulations for portable work machines that require readjustment of the low-speed fuel adjustment mechanism according to the driving environment such as in highlands. In the carburetor of the separate system fuel passage, the passage of the low speed fuel adjustment mechanism and the passage of the high speed fuel adjustment mechanism are independent, so that the low speed fuel adjustment mechanism is operated at a low speed from a normal adjustment position shown by a broken line in FIG. When the fuel adjustment mechanism is adjusted to increase the fuel amount, the high-speed fuel adjustment mechanism is affected, and as shown by the solid line in FIG. 4, the fuel amount during high-speed operation of the engine also increases.
【0004】一方、同系統式燃料通路の気化器では、低
速燃料調整機構を調整しても、機関の高速運転での燃料
量には影響しないが、図5に示すように、機関の低速運
転域と高速運転域との中間の運転域で、燃料量が少くな
ることがある。つまり、上述した機関の中速運転域で
は、高速燃料系統と低速燃料系統にそれぞれ作用する吸
気負圧が互いに引き合いを始め、吸気負圧が打ち消しあ
うために燃料量が不足する。On the other hand, in the carburetor of the same system type fuel passage, even if the low speed fuel adjusting mechanism is adjusted, it does not affect the fuel amount in the high speed operation of the engine, but as shown in FIG. The amount of fuel may be low in the operating range intermediate between the high speed operating range and the high speed operating range. That is, in the above-described medium speed operation range of the engine, the intake negative pressures acting on the high-speed fuel system and the low-speed fuel system start to attract each other, and the intake negative pressures cancel each other, so that the fuel amount becomes insufficient.
【0005】本出願人の出願による実願平5-24974 号に
係る膜型気化器の同系統式燃料通路構造では、同出願図
面の符号を引用して説明すると、機関の高速運転域でベ
ンチユリ部で絞られた高速燃料噴孔19の吸気負圧が、
低速燃料噴孔20のそれよりも強くなるために、連続し
て高速運転すると、吸気通路の空気が低速燃料噴孔2
0、低速燃料室21、低速燃料調整針弁23、低速燃料
通路36b、高速燃料室18を経て高速燃料噴孔19へ
逆流し、燃料が稀薄になつたり、燃料噴出が不規則にな
り、機関の不調や排ガス成分の悪化を来すことがある。In the same-system fuel passage structure of the membrane carburetor according to Japanese Patent Application No. 5-24974 filed by the applicant of the present invention, a description will be given by referring to the reference numerals in the drawings of the same application. The intake negative pressure of the high-speed fuel injection hole 19 throttled by
Since it becomes stronger than that of the low-speed fuel injection hole 20, the air in the intake passage will be discharged by the low-speed fuel injection hole 2 when continuously operating at high speed.
0, the low-speed fuel chamber 21, the low-speed fuel adjusting needle valve 23, the low-speed fuel passage 36b, the high-speed fuel chamber 18 and the reverse flow into the high-speed fuel injection hole 19, and the fuel is diluted or the fuel injection becomes irregular. May result in deterioration of exhaust gas components.
【0006】上述の問題は低速燃料通路36bの内部に
逆止弁を配設することにより解決できるが、燃料の流れ
が少ない低速燃料通路36bの内部に逆止弁を設ける
と、逆止弁の弁室に燃料蒸気や空気が溜つたり、弁体
(普通には薄いゴム製の板が用いられる)が弁座に付着
したままになつたりし、かえつて低速燃料の流れが不安
定になることがある。また、小型の膜型気化器では逆止
弁を設けるスペースが制限され、設計上の自由度も制限
される。The above-mentioned problem can be solved by disposing a check valve inside the low speed fuel passage 36b. However, if the check valve is provided inside the low speed fuel passage 36b where the flow of fuel is small, the check valve will be closed. Fuel vapor or air accumulates in the valve chamber, or the valve body (usually a thin rubber plate) remains attached to the valve seat, which in turn makes the low-speed fuel flow unstable. Sometimes. Further, in a small membrane vaporizer, the space for providing the check valve is limited, and the degree of freedom in design is also limited.
【0007】[0007]
【発明が解決しようとする課題】本発明の目的は上述の
問題に鑑み、高速燃料噴孔の吸気負圧が低速燃料系統へ
作用するのを弱めることにより、機関の中速運転域で燃
料量が不足するのを防止する、膜型気化器の同系統式燃
料通路構造を提供することにある。SUMMARY OF THE INVENTION In view of the above problems, the object of the present invention is to reduce the influence of the intake negative pressure of the high-speed fuel injection hole on the low-speed fuel system, so that the fuel amount in the medium-speed operation range of the engine is reduced. It is an object of the present invention to provide a systematic fuel passage structure for a membrane carburetor, which prevents shortage of fuel.
【0008】[0008]
【課題を解決するための手段】上記目的を達成するため
に、本発明の構成は一端が定圧燃料室に連通し他端が高
速燃料噴孔を経て吸気通路に開口する高速燃料通路を備
えた膜式気化器の同系統式燃料通路構造において、高速
燃料噴孔の定圧燃料室に隣接する上流側端部に固定ジエ
ツトを設け、固定ジエツトの下流側通路を第1、第2の
燃料系統に分岐し、第1の燃料系統は固定ジエツトで計
量された燃料の一部を低速燃料通路を経て低速燃料噴孔
から吸気通路へ噴出し、第2の燃料系統は固定ジエツト
で計量された燃料の残部を絞りを経て高速燃料噴孔から
吸気通路のベンチユリ部へ噴出し、前記絞りは固定ジエ
ツトとほぼ同径にしたものである。In order to achieve the above object, the structure of the present invention comprises a high speed fuel passage, one end of which communicates with the constant pressure fuel chamber and the other end of which opens into the intake passage through the high speed fuel injection hole. In the same type fuel passage structure of the membrane carburetor, a fixed jet is provided at the upstream end adjacent to the constant pressure fuel chamber of the high-speed fuel injection hole, and the downstream passage of the fixed jet is used as the first and second fuel systems. The first fuel system branches and a part of the fuel measured by the fixed jet is ejected from the low speed fuel injection hole to the intake passage through the low speed fuel passage, and the second fuel system is divided into the fixed fuel measured by the fixed jet. The remaining portion is jetted from the high-speed fuel injection hole to the bench lily portion of the intake passage through the throttle, and the throttle has approximately the same diameter as the fixed jet.
【0009】[0009]
【作用】高速燃料噴孔に隣接して高速燃料噴孔の上流側
に絞りを配設することにより、高速燃料噴孔から低速燃
料系統へ作用する吸気負圧を弱め、低速燃料系統の燃料
が少くなるのを防止する。By arranging a throttle adjacent to the high-speed fuel injection hole and upstream of the high-speed fuel injection hole, the intake negative pressure acting on the low-speed fuel system from the high-speed fuel injection hole is weakened, and the fuel of the low-speed fuel system is reduced. Prevent it from running low.
【0010】同系統式燃料通路構造であるから、低速燃
料系統の燃料量を調整しても、機関の高速運転(絞り弁
が全開)での燃料量には影響せず、排ガス成分の悪化を
防止できる。Since the fuel passage structure is of the same system, even if the fuel amount of the low speed fuel system is adjusted, it does not affect the fuel amount in the high speed operation of the engine (the throttle valve is fully open), and the exhaust gas component is deteriorated. It can be prevented.
【0011】[0011]
【実施例】図1は本発明に係る同系統式燃料通路構造を
備えた膜型気化器の側面断面図である。気化器の本体1
5はベンチユリ部16aを有する吸気通路16を備えて
おり、吸気通路16の上流側端壁15aは空気清浄器を
結合され、下流側端壁15bは機関の吸気ポートへ結合
される。吸気通路16の上流側に軸4によりチヨーク弁
5が、下流側に軸17aにより絞り弁17がそれぞれ回
動可能に配設される。本体15の上壁部は膜10により
仕切られる脈動圧室8およびポンプ室9と、逆止弁1
2,7とからなる燃料ポンプ11を構成される。2行程
機関のクランク室の脈動圧が通路14から脈動圧室8へ
導入されると、図示してない燃料槽の燃料が通路13、
逆止弁12を経てポンプ室9へ吸い込まれ、逆止弁7、
ストレーナ6、通路3、流入弁2を経て定圧燃料室25
へ吐き出される。DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS FIG. 1 is a side sectional view of a membrane type carburetor equipped with the same type fuel passage structure according to the present invention. Main body of vaporizer 1
5 includes an intake passage 16 having a bench lily portion 16a. An upstream end wall 15a of the intake passage 16 is connected to an air purifier and a downstream end wall 15b is connected to an intake port of the engine. The chuck yoke valve 5 is disposed on the upstream side of the intake passage 16 by the shaft 4 and the throttle valve 17 is rotatable on the downstream side by the shaft 17a. The upper wall portion of the main body 15 is partitioned by the membrane 10, and the pulsating pressure chamber 8 and the pump chamber 9, and the check valve 1
A fuel pump 11 including 2 and 7 is configured. When the pulsating pressure in the crank chamber of the two-stroke engine is introduced into the pulsating pressure chamber 8 from the passage 14, fuel in a fuel tank (not shown) is passed through the passage 13,
The check valve 7 is sucked into the pump chamber 9 through the check valve 12,
Through the strainer 6, the passage 3 and the inflow valve 2, the constant pressure fuel chamber 25
Is exhaled to.
【0012】定圧燃料室25は本体15の下壁にカバー
31と一緒に結合した膜29の上側に区画され、膜29
の下側は大気室30とされる。定圧燃料室25に支軸2
7により回動可能に支持したレバー28は、左端を流入
弁2に係合され、右端を膜29に係合される。レバー2
8はばね24の力により時計方向へ回転付勢され、流入
弁2を閉じる。定圧燃料室25の燃料が少くなると、大
気圧を受ける膜29が押し上げられ、レバー28がばね
24の力に抗して反時計方向へ回動し、流入弁2を開
く。定圧燃料室25は燃料ポンプ11から燃料を補給さ
れる。The constant-pressure fuel chamber 25 is defined on the lower wall of the main body 15 and above the membrane 29 joined together with the cover 31.
The lower side is an atmosphere chamber 30. Support shaft 2 in constant pressure fuel chamber 25
The lever 28 rotatably supported by 7 has its left end engaged with the inflow valve 2 and its right end engaged with the membrane 29. Lever 2
8 is urged to rotate in the clockwise direction by the force of the spring 24 to close the inflow valve 2. When the amount of fuel in the constant pressure fuel chamber 25 is low, the membrane 29 that receives the atmospheric pressure is pushed up, the lever 28 rotates counterclockwise against the force of the spring 24, and the inflow valve 2 opens. The constant pressure fuel chamber 25 is replenished with fuel from the fuel pump 11.
【0013】本発明によれば、定圧燃料室25とベンチ
ユリ部16aとを結ぶ円筒部47に組立体Aが嵌装され
る。図2に示すように、組立体Aは円柱状の本体50
に、上から円筒状の高速燃料噴孔51、弁室52、絞り
43、通路54、円筒部55を順に形成される。高速燃
料噴孔51はベンチユリ部16aへ突出される。ゴム製
の弁板からなる逆止弁42が弁室52へ収容され、絞り
43の圧力が低くなると、逆止弁42は弁座53へ吸着
され、絞り43を閉じるが、高速燃料噴孔51に作用す
る吸気負圧が強くなると吸い上げられ、高速燃料噴孔5
1に嵌装した座板41から下方へ湾曲して突出する複数
の脚片41aに当り、弁室52と吸気通路16との間の
連通を維持する。円筒部55に通路46aを有する固定
ジエツト46が嵌合される。通路54は径方向通路45
を経て本体50の外周面に形成した環状溝44へ連通さ
れる。According to the present invention, the assembly A is fitted in the cylindrical portion 47 connecting the constant pressure fuel chamber 25 and the bench lily portion 16a. As shown in FIG. 2, the assembly A has a cylindrical main body 50.
A cylindrical high-speed fuel injection hole 51, a valve chamber 52, a throttle 43, a passage 54, and a cylindrical portion 55 are sequentially formed from the top. The high-speed fuel injection hole 51 is projected to the bench lily portion 16a. When the check valve 42 made of a rubber valve plate is housed in the valve chamber 52 and the pressure of the throttle 43 becomes low, the check valve 42 is adsorbed to the valve seat 53 and closes the throttle 43, but the high speed fuel injection hole 51 When the negative pressure of intake air acting on the cylinder becomes strong, it is sucked up, and the high-speed fuel injection hole 5
The plurality of leg pieces 41a that curve downward and project from the seat plate 41 fitted to the first portion 41 maintain the communication between the valve chamber 52 and the intake passage 16. The fixed jet 46 having the passage 46a is fitted into the cylindrical portion 55. The passage 54 is the radial passage 45.
Through the annular groove 44 formed on the outer peripheral surface of the main body 50.
【0014】図1に示すように、環状溝44は低速燃料
通路36、低速燃料調整針弁23を経て、低速燃料室2
1へ連通される。低速燃料室21は絞り弁17の閉位置
付近に配設され、低速燃料室21から吸気通路16へ、
吸気通路16の軸方向に沿つて複数の低速燃料噴孔20
が開口される。As shown in FIG. 1, the annular groove 44 passes through the low-speed fuel passage 36, the low-speed fuel adjusting needle valve 23, and the low-speed fuel chamber 2.
It is connected to 1. The low-speed fuel chamber 21 is arranged near the closed position of the throttle valve 17, and the low-speed fuel chamber 21 enters the intake passage 16,
A plurality of low speed fuel injection holes 20 are provided along the axial direction of the intake passage 16.
Is opened.
【0015】固定ジエツト46の通路面積は絞り43の
通路面積とほぼ等しく、機関の高速運転で排ガス規制値
を超えないような燃料量を得る値に決定される。固定ジ
エツト46の内径は、機関の出力や機関が搭載される携
帯作業機により異なるが、排気量が20cc程度の2行程
機関では1mm以下とする。The passage area of the fixed jet 46 is substantially equal to the passage area of the throttle 43, and is set to a value that provides a fuel amount that does not exceed the exhaust gas regulation value at high speed operation of the engine. The inner diameter of the fixed jet 46 varies depending on the output of the engine and the portable working machine on which the engine is mounted, but it is 1 mm or less for a two-stroke engine with a displacement of about 20 cc.
【0016】次に、本発明による膜型気化器の同系統式
燃料通路の作用について説明する。機関のアイドルない
し低速運転では、絞り弁17に隣接する低速燃料噴孔2
0に強い吸気負圧が作用するので、定圧燃料室25の燃
料は固定ジエツト46、通路45、環状溝44、低速燃
料通路36、低速燃料調整針弁23、低速燃料室21、
低速燃料噴孔20を経て吸気通路16へ供給される。こ
の時、ベンチユリ部16aから高速燃料噴孔51へ作用
する吸気負圧は弱く、逆止弁42は燃料の粘性により弁
座53に付着し、高速燃料噴孔51から弁室52、絞り
43、通路45、環状溝44、低速燃料通路36、低速
燃料調整針弁23、低速燃料室21、低速燃料噴孔20
への空気の流れを阻止する。Next, the operation of the same type fuel passage of the membrane vaporizer according to the present invention will be described. During idle or low speed operation of the engine, the low speed fuel injection hole 2 adjacent to the throttle valve 17
Since a strong intake negative pressure acts on 0, the fuel in the constant pressure fuel chamber 25 receives the fixed jet 46, the passage 45, the annular groove 44, the low speed fuel passage 36, the low speed fuel adjusting needle valve 23, the low speed fuel chamber 21,
It is supplied to the intake passage 16 through the low-speed fuel injection hole 20. At this time, the intake negative pressure acting from the bench lily portion 16a to the high-speed fuel injection hole 51 is weak, the check valve 42 adheres to the valve seat 53 due to the viscosity of the fuel, and the high-speed fuel injection hole 51 causes the valve chamber 52, the throttle 43, Passage 45, annular groove 44, low speed fuel passage 36, low speed fuel adjusting needle valve 23, low speed fuel chamber 21, low speed fuel injection hole 20
Block the flow of air to.
【0017】機関の高速運転では、ベンチユリ部16a
の高速燃料噴孔51に作用する吸気負圧が強くなり、逆
止弁42が吸い上げられ、定圧燃料室25の燃料は固定
ジエツト46、通路54、絞り43、弁室52、高速燃
料噴孔51を経て吸気通路16へ供給される。In the high speed operation of the engine, the bench lily portion 16a
The intake negative pressure acting on the high-speed fuel injection hole 51 becomes strong, the check valve 42 is sucked up, and the fuel in the constant-pressure fuel chamber 25 is fixed jet 46, passage 54, throttle 43, valve chamber 52, high-speed fuel injection hole 51. And is supplied to the intake passage 16.
【0018】絞り弁17を全開とする機関の高速運転で
は、ベンチユリ部16aの高速燃料噴孔51に作用する
吸気負圧は、低速燃料噴孔20に作用する吸気負圧より
も強くなり、吸気通路16の空気が低速燃料噴孔20、
低速燃料室21、低速燃料調整針弁23、低速燃料通路
36、環状溝44、通路45,54、絞り43、弁室5
2を経て高速燃料噴孔51へ流れようとする。しかし、
高速燃料噴孔51から低速燃料噴孔20に至る通路は、
絞り43と低速燃料調針弁23により2段に絞られるの
で、高速燃料噴孔51から吸気通路16へ供給される燃
料量に悪影響を及ぼさない。During high-speed operation of the engine with the throttle valve 17 fully opened, the negative suction pressure acting on the high-speed fuel injection hole 51 of the bench lily portion 16a becomes stronger than the negative suction pressure acting on the low-speed fuel injection hole 20. The air in the passage 16 is the low-speed fuel injection hole 20,
Low speed fuel chamber 21, low speed fuel adjusting needle valve 23, low speed fuel passage 36, annular groove 44, passages 45 and 54, throttle 43, valve chamber 5
Attempt to flow into the high-speed fuel injection hole 51 via 2. But,
The passage from the high speed fuel injection hole 51 to the low speed fuel injection hole 20 is
Since the throttle 43 and the low-speed fuel adjustment valve 23 restrict the pressure in two stages, the amount of fuel supplied from the high-speed fuel injection hole 51 to the intake passage 16 is not adversely affected.
【0019】機関の中速運転域では、高速燃料噴孔51
と低速燃料噴孔20に作用する吸気負圧はほぼ等しくな
るが、両方の燃料噴孔51,20から吸気通路16へ供
給される燃料量は固定ジエツト46により規定され、か
つ高速燃料噴孔51と低速燃料噴孔20とが、絞り43
と低速燃料調整針弁23とにより2段に絞られているの
で、両方の燃料噴孔51,20での吸気負圧の引き合い
が抑えられ、燃料は両方の燃料噴孔51,20から吸気
通路16へ円滑に供給される。In the medium speed operation range of the engine, the high speed fuel injection holes 51
And the intake negative pressure acting on the low-speed fuel injection hole 20 become substantially equal, but the amount of fuel supplied from both fuel injection holes 51, 20 to the intake passage 16 is defined by the fixed jet 46 and the high-speed fuel injection hole 51. The low-speed fuel injection hole 20 and the throttle 43
And the low-speed fuel adjusting needle valve 23, the intake negative pressure in both fuel injection holes 51, 20 is suppressed, and the fuel flows from both fuel injection holes 51, 20 into the intake passage. 16 is smoothly supplied.
【0020】低速燃料調整針弁23の開度が小さい状態
では、図3に破線で示すように機関回転数に対応して燃
料量が増加する。一方、低速燃料調整針弁23の開度を
大きくすると、図3に実線で示すように両方の燃料噴孔
51,20から吸気通路16へ供給される燃料量は、機
関回転数に対応して増加し、機関の中速運転域で燃料不
足を来たすということはない。つまり、低速燃料調整針
弁23を調整することにより機関の低速運転域での燃料
量を加減しても、機関の高速運転域で両方の燃料噴孔5
1,20から吸気通路16へ供給される燃料量は変化せ
ず、所定の値に保たれるので、排ガス規制に悪影響を及
ぼさない。When the opening degree of the low speed fuel adjusting needle valve 23 is small, the fuel amount increases in accordance with the engine speed as shown by the broken line in FIG. On the other hand, when the opening degree of the low speed fuel adjusting needle valve 23 is increased, the amount of fuel supplied from both fuel injection holes 51, 20 to the intake passage 16 as shown by the solid line in FIG. It will not increase and fuel shortage will not occur in the medium speed operation range of the engine. That is, even if the fuel amount in the low speed operation range of the engine is adjusted by adjusting the low speed fuel adjustment needle valve 23, both fuel injection holes 5 are
The amount of fuel supplied to the intake passage 16 from 1, 20 does not change and is maintained at a predetermined value, so that it does not adversely affect the exhaust gas regulation.
【0021】[0021]
【発明の効果】本発明は上述のように、一端が定圧燃料
室に連通し他端が高速燃料噴孔を経て吸気通路に開口す
る高速燃料通路を備えた膜式気化器の同系統式燃料通路
構造において、高速燃料噴孔の定圧燃料室に隣接する上
流側端部に固定ジエツトを設け、固定ジエツトの下流側
通路を第1、第2の燃料系統に分岐し、第1の燃料系統
は固定ジエツトで計量された燃料の一部を低速燃料通路
を経て低速燃料噴孔から吸気通路へ噴出し、第2の燃料
系統は固定ジエツトで計量された燃料の残部を絞りを経
て高速燃料噴孔から吸気通路のベンチユリ部へ噴出し、
前記絞りは固定ジエツトとほぼ同径にしたものであるか
ら、部品点数の増加や通路の変更を来さず、加工が容易
であり、限られたスペースに構成できる。As described above, according to the present invention, the same type fuel of the membrane type carburetor having the high speed fuel passage having one end communicating with the constant pressure fuel chamber and the other end opening to the intake passage through the high speed fuel injection hole is provided. In the passage structure, a fixed jet is provided at the upstream end adjacent to the constant-pressure fuel chamber of the high-speed fuel injection hole, and the downstream passage of the fixed jet is branched into the first and second fuel systems. A part of the fuel measured by the fixed jet is ejected from the low speed fuel injection hole to the intake passage through the low speed fuel passage, and the second fuel system is the high speed fuel injection hole after the rest of the fuel measured by the fixed jet is throttled. Spouts from the intake passage to the bench lily part of the intake passage,
Since the diameter of the throttle is approximately the same as that of the fixed jet, it does not increase the number of parts or change the passage, is easy to process, and can be configured in a limited space.
【0022】高速燃料噴孔に隣接して高速燃料噴孔の上
流側に絞りを配設することにより、高速燃料噴孔から低
速燃料系統へ作用する吸気負圧を弱め、低速燃料系統の
燃料量が少くなるのを防止できる。By disposing a throttle adjacent to the high-speed fuel injection hole and upstream of the high-speed fuel injection hole, the intake negative pressure acting on the low-speed fuel system from the high-speed fuel injection hole is weakened, and the fuel amount of the low-speed fuel system is reduced. Can be prevented from decreasing.
【0023】高速燃料噴孔と低速燃料噴孔とを結ぶ通路
が、絞りと低速燃料調整針弁により2段に絞られるの
で、機関の中・高速運転域で、高速燃料噴孔の吸気負圧
が低速燃料噴孔へ及ぼす影響度が弱められ、低速燃料噴
孔から高速燃料噴孔への空気の逆流を防止できる。Since the passage connecting the high-speed fuel injection hole and the low-speed fuel injection hole is throttled in two stages by the throttle and the low-speed fuel adjusting needle valve, the intake negative pressure of the high-speed fuel injection hole in the medium and high-speed operation region of the engine. Influence on the low-speed fuel injection hole is weakened, and backflow of air from the low-speed fuel injection hole to the high-speed fuel injection hole can be prevented.
【0024】同系統式燃料通路構造により、低速燃料系
統の燃料量を調整しても、機関の高速運転(絞り弁が全
開)での燃料量には影響せず、排ガス成分の悪化を防止
できる。Due to the systematic fuel passage structure, even if the fuel amount of the low speed fuel system is adjusted, it does not affect the fuel amount during high speed operation of the engine (throttle valve is fully open), and deterioration of exhaust gas components can be prevented. .
【図1】本発明に係る同系統式燃料通路構造を備えた膜
型気化器の側面断面図である。FIG. 1 is a side cross-sectional view of a membrane type carburetor equipped with the same type fuel passage structure according to the present invention.
【図2】本発明に係る同系統式燃料通路構造の要部を拡
大して示す側面断面図である。FIG. 2 is a side cross-sectional view showing an enlarged main part of the same-system fuel passage structure according to the present invention.
【図3】本発明に係る同系統式燃料通路構造を備えた膜
型気化器の特性線図である。FIG. 3 is a characteristic diagram of a membrane vaporizer provided with the same-system fuel passage structure according to the present invention.
【図4】別系統式燃料通路構造を備えた膜型気化器の特
性線図である。FIG. 4 is a characteristic diagram of a membrane vaporizer having a separate system fuel passage structure.
【図5】従来の同系統式燃料通路構造を備えた膜型気化
器の特性線図である。FIG. 5 is a characteristic diagram of a conventional membrane carburetor having the same system fuel passage structure.
15:気化器本体 16:吸気通路 16a:ベンチユ
リ部 20:低速燃料噴孔 21:低速燃料室 23:
低速燃料調整針弁 25:定圧燃料室 36:低速燃料
通路 43:絞り 46:固定ジエツト 51:高速燃
料噴孔 54:通路15: Vaporizer main body 16: Intake passage 16a: Bench lily part 20: Low speed fuel injection hole 21: Low speed fuel chamber 23:
Low speed fuel adjusting needle valve 25: Constant pressure fuel chamber 36: Low speed fuel passage 43: Throttling 46: Fixed jet 51: High speed fuel injection hole 54: Passage
Claims (2)
噴孔を経て吸気通路に開口する高速燃料通路を備えた膜
式気化器の同系統式燃料通路構造において、高速燃料噴
孔の定圧燃料室に隣接する上流側端部に固定ジエツトを
設け、固定ジエツトの下流側通路を第1、第2の燃料系
統に分岐し、第1の燃料系統は固定ジエツトで計量され
た燃料の一部を低速燃料通路を経て低速燃料噴孔から吸
気通路へ噴出し、第2の燃料系統は固定ジエツトで計量
された燃料の残部を絞りを経て高速燃料噴孔から吸気通
路のベンチユリ部へ噴出し、前記絞りは固定ジエツトと
ほぼ同径にしたことを特徴とする、膜型気化器の同系統
式燃料通路構造。1. A high-speed fuel injection hole in a system fuel passage structure of a membrane carburetor having a high-speed fuel passage, one end of which communicates with a constant-pressure fuel chamber and the other end of which opens through a high-speed fuel injection hole into an intake passage. A fixed jet is provided at the upstream end adjacent to the constant pressure fuel chamber, and the downstream passage of the fixed jet is branched into the first and second fuel systems, and the first fuel system is provided with the fuel measured by the fixed jet. Part of the fuel is ejected from the low-speed fuel injection hole to the intake passage through the low-speed fuel passage, and the second fuel system is ejected from the high-speed fuel injection hole to the bench lily portion of the intake passage through the rest of the fuel measured by the fixed jet. The diaphragm has the same diameter as that of the fixed jet, and the same-system fuel passage structure of the membrane carburetor is characterized.
設した、請求項1に記載の膜型気化器の同系統式燃料通
路構造。2. The same-system fuel passage structure for a membrane carburetor according to claim 1, wherein a low-speed fuel adjusting needle valve is arranged in the low-speed fuel passage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP19188294A JPH0835448A (en) | 1994-07-22 | 1994-07-22 | Membrane carburetor fuel passage structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP19188294A JPH0835448A (en) | 1994-07-22 | 1994-07-22 | Membrane carburetor fuel passage structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0835448A true JPH0835448A (en) | 1996-02-06 |
Family
ID=16282036
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP19188294A Pending JPH0835448A (en) | 1994-07-22 | 1994-07-22 | Membrane carburetor fuel passage structure |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0835448A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111550329A (en) * | 2020-06-23 | 2020-08-18 | 福建省大立通用机电制造有限公司 | Novel leak protection oil regulation device |
-
1994
- 1994-07-22 JP JP19188294A patent/JPH0835448A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111550329A (en) * | 2020-06-23 | 2020-08-18 | 福建省大立通用机电制造有限公司 | Novel leak protection oil regulation device |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JPS6029828B2 (en) | Rotary throttle valve type carburetor | |
| JP2000220527A (en) | Vaporizer accelerator | |
| US6676114B2 (en) | Carburetor arrangement having an accelerator pump | |
| JPH0835448A (en) | Membrane carburetor fuel passage structure | |
| JP3292279B2 (en) | Membrane vaporizer for 4-stroke internal combustion engine | |
| JP2580790Y2 (en) | Diaphragm type vaporizer | |
| US5394840A (en) | Fuel supply system | |
| JP2007211772A (en) | Diaphragm vaporizer | |
| JPH10331718A (en) | High-speed fuel passage structure of membrane carburetor | |
| JP2573620Y2 (en) | Diaphragm carburetor with the same system fuel passage | |
| JP2599233Y2 (en) | Diaphragm type vaporizer | |
| US20070052116A1 (en) | Accelerator apparatus for diaphragm carburetors | |
| US20230204005A1 (en) | Carburettor assembly | |
| JP2002155805A (en) | Two-stroke stratified scavenging internal combustion engine | |
| US6234457B1 (en) | Method of operating a diaphragm-type carburetor | |
| JP3409949B2 (en) | Starter fuel supply for carburetor | |
| JP3899609B2 (en) | Fuel supply device | |
| JPS6060028B2 (en) | carburetor fuel control device | |
| JPH0816442B2 (en) | Hydraulic oil supply mechanism for internal combustion engine with hydraulic lifter | |
| JPH084593A (en) | Low-speed fuel passage structure of carburetor | |
| JP2000265906A (en) | Acceleration device for evaporator | |
| JPH0680844U (en) | Diaphragm carburetor same-system fuel passage structure | |
| JPH0953515A (en) | Membrane carburetor fuel passage structure | |
| JP4036908B2 (en) | Fuel adjustment mechanism of rotary throttle carburetor | |
| JPH0650213A (en) | Diaphragm type carburetor |