JP2001027154A - Carburetor for general purpose engine - Google Patents

Carburetor for general purpose engine

Info

Publication number
JP2001027154A
JP2001027154A JP11202471A JP20247199A JP2001027154A JP 2001027154 A JP2001027154 A JP 2001027154A JP 11202471 A JP11202471 A JP 11202471A JP 20247199 A JP20247199 A JP 20247199A JP 2001027154 A JP2001027154 A JP 2001027154A
Authority
JP
Japan
Prior art keywords
fuel
passage
flange
carburetor
columnar portion
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.)
Granted
Application number
JP11202471A
Other languages
Japanese (ja)
Other versions
JP3836635B2 (en
Inventor
Masaaki Omi
雅明 尾見
Ko Takahashi
航 高橋
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 JP20247199A priority Critical patent/JP3836635B2/en
Priority to US09/616,497 priority patent/US6435482B1/en
Publication of JP2001027154A publication Critical patent/JP2001027154A/en
Application granted granted Critical
Publication of JP3836635B2 publication Critical patent/JP3836635B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Landscapes

  • Fuel-Injection Apparatus (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)

Abstract

PROBLEM TO BE SOLVED: To ensure air and liquid tightness at a mating face between a metallic body and a columnar part of a carburetor improved in high temperature restarting performance wherein a constant fuel chamber is provided at a lower part of the metallic body comprising a horizontal intake passage and the columnar part having a fuel reservoir in a fuel passage formed is made of synthetic resin and suspended in the constant fuel chamber. SOLUTION: This carburetor has a flange 12 integrally formed with a columnar part 11 at an upper end thereof and an outer side peripheral part of the flange 12 is put between a body 1 and a fuel vessel 15 while a lower end of the columnar part 11 is contacted to a bottom wall 15b of the fuel vessel 15, and the body 1 is connected with the fuel vessel 15 on an outside of the flange 12 by a screw 18. A mating face 19 can be thereby in close-adhered condition.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は汎用エンジンの燃料
供給に用いられる気化器、詳しくは高温始動性にすぐれ
ており、且つ簡単容易に形成されるとともに漏れの心配
のない燃料或いはブリード空気の通路を具えた汎用エン
ジン用気化器に関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a carburetor used for supplying fuel to a general-purpose engine, and more particularly, to a fuel or bleed air passage which is excellent in high-temperature startability, is easily and easily formed, and has no fear of leakage. And a vaporizer for a general-purpose engine.

【0002】[0002]

【従来の技術】近年のエンジンはエミッション規制に対
応するため混合気を希薄化しており、そのために燃焼温
度が従前よりも高くなっている。また、低騒音化のため
に多く採用されるようになったエンジンを防音壁で囲ん
だものは、放熱しにくい構造であるためにエンジンを停
止したとき長い時間に亘って高温状態が続くことを避け
られない。
2. Description of the Related Art In recent engines, the air-fuel mixture is diluted to comply with emission regulations, and as a result, the combustion temperature is higher than before. In addition, since the engine that has been widely adopted for noise reduction is surrounded by a soundproof wall, it is difficult to dissipate heat, so that when the engine is stopped, the high temperature state will continue for a long time. Inevitable.

【0003】一方、気化器の胴体は金属、一般にはアル
ミニウムのダイカスト鋳造品であって吸気マニホルドに
接続されるため、エンジンの高い燃焼温度によって容易
に全体が高温状態となり、殊に防音構造のエンジンにあ
ってはエンジン停止後も高温状態が長い時間継続する。
このため、エンジンを停止したとき主燃料通路の燃料溜
り内の燃料が蒸発してしまい、特にジーゼリング対策の
ため燃料通路の入口をエンジン停止時に閉止する手段を
設けたものにおいては、燃料通路に燃料がない状態で再
始動を開始することとなる。加えて、再始動を高温状態
で行なう場合は、燃料溜りに燃料が導入されても直ちに
蒸発してしまい、このことが高温再始動を困難にする原
因となっている。
[0003] On the other hand, the body of the carburetor is a die-cast product of metal, generally aluminum, and is connected to the intake manifold. Therefore, the entire body is easily brought to a high temperature state by the high combustion temperature of the engine. In this case, the high temperature state continues for a long time even after the engine is stopped.
For this reason, when the engine is stopped, the fuel in the fuel reservoir in the main fuel passage evaporates.In particular, in a device provided with a means for closing the entrance of the fuel passage when the engine is stopped to prevent dieseling, the fuel passage is provided in the fuel passage. The restart will be started in the absence of any. In addition, when the restart is performed in a high temperature state, even if the fuel is introduced into the fuel reservoir, the fuel evaporates immediately, which makes the high temperature restart difficult.

【0004】その対策として、胴体と吸気マニホルドと
の間に断熱性のガスケットを挟み込むという手段が慣用
されているが、断熱性ガスケットはエンジンから吸気マ
ニホルドを経て胴体に伝導する熱の遮断には有効であっ
ても、防音構造のエンジンにおいては高温の輻射熱が胴
体に直接作用するのを防ぐことはできず、高温再始動の
困難は解消されない。
As a countermeasure, it has been customary to insert a heat insulating gasket between the fuselage and the intake manifold. However, the heat insulating gasket is effective for blocking heat conducted from the engine to the fuselage through the intake manifold to the engine. However, in a soundproof engine, high-temperature radiant heat cannot be prevented from directly acting on the fuselage, and the difficulty of restarting at a high temperature cannot be solved.

【0005】別の対策として、汎用エンジン向けの気化
器において吸気通路および燃料供給に必要な通路を設け
た胴体と定燃料室を形成する燃料容器とを、金属よりも
熱伝導度が低い材料である合成樹脂で作ることが知られ
ている(実公昭49−39710号公報参照)。
As another countermeasure, in a carburetor for a general-purpose engine, a body provided with an intake passage and a passage required for fuel supply and a fuel container forming a constant fuel chamber are made of a material having lower thermal conductivity than metal. It is known that it is made of a certain synthetic resin (see JP-B-49-39710).

【0006】前記の熱対策とは別に、金属または合成樹
脂で作られた胴体の内部に設けられる燃料更にはブリー
ド空気の通路の多くは途中で屈折している。このような
通路は多方向からのドリル加工により形成されるもので
あり、それらの端面を球栓などの閉止部材で個別に閉止
処理しなければならず、加工工数が多い、部品点数が多
い、燃料或いはブリード空気の漏れの心配を完全に払拭
できない、という問題がある。
Apart from the above-mentioned heat countermeasures, many of the passages for fuel and bleed air provided inside the body made of metal or synthetic resin are bent in the middle. Such a passage is formed by drilling from multiple directions, and their end faces must be individually closed with a closing member such as a ball plug, and the number of processing steps is large, the number of parts is large, There is a problem that the fear of leakage of fuel or bleed air cannot be completely eliminated.

【0007】加えて、金属製の胴体は形状がかなり複雑
であるため鋳巣が散在していることが多く、ドリル加工
で作られた通路が互いに接近しているとこれらが鋳巣に
よって短絡することがある。殊に、汎用エンジン向けの
気化器は小形であり、この種の気化器に多く採用されて
いる横向き吸気通路を有する胴体の下方に燃料容器を取
り付けてその中心部分に胴体から垂下した柱状部分に燃
料通路を設けた構造のものにあっては、柱状部分内で通
路が互いにきわめて接近しているため鋳巣による短絡の
機会が多く、製品の歩留まりを低くする原因となってい
る。合成樹脂製の胴体は鋳巣が存在しないので通路を互
いにきわめて接近させて形成しても短絡の心配がない
が、機械的強度に劣るため吸気マニホルドへの接続の際
に変形や破損を生じさせないように補強手段が必要であ
るばかりか、機能部品である金属製の絞り弁、ジェット
などを安定よく取り付け保持されるのが困難である。
[0007] In addition, metal hulls are fairly complex in shape and are often interspersed with cavities, which short-circuit due to the cavities when the drilled passages are close together. Sometimes. In particular, carburetors for general-purpose engines are small, and a fuel container is attached below the fuselage having a horizontal intake passage, which is often used in this type of carburetor, and a central portion of the fuel container is formed in a columnar portion hanging down from the fuselage. In the structure having the fuel passage, since the passages are extremely close to each other in the columnar portion, there are many chances of short-circuiting due to a cavity, which causes a reduction in product yield. The body made of synthetic resin has no cavities, so there is no danger of short-circuiting even if the passages are formed very close to each other.However, the mechanical strength is inferior, so there is no deformation or breakage when connecting to the intake manifold In addition to the need for reinforcing means, it is difficult to stably mount and hold a metal throttle valve, jet, or the like, which is a functional component.

【0008】[0008]

【発明が解決しようとする課題】本発明は特に汎用エン
ジン向けの気化器について、前述の問題点である胴体を
金属で作ったものがもっている高温再始動が困難である
という点、およびこの困難を避けるため胴体を合成樹脂
で作ったものがもっている機械的強度に劣るという点、
更にこれらに加えて燃料やブリード空気の通路の加工が
面倒であるとともに短絡や漏れの心配が残るという点を
伴わないものとすることを課題としてなされたものであ
る。
SUMMARY OF THE INVENTION The present invention relates to a carburetor for a general-purpose engine, in particular, it is difficult to perform a high-temperature restart due to the fact that a fuselage made of metal is difficult. The point that the body made of synthetic resin is inferior in mechanical strength to avoid
Further, in addition to the above, it has been made to make the processing of the passage for the fuel and the bleed air troublesome and to avoid the problem of remaining short circuit and leakage.

【0009】[0009]

【課題を解決するための手段】横向きの吸気通路を有す
る胴体の下に定燃料室を形成する燃料容器が取り付けら
れているとともに、その内部に胴体の下方に延びる柱状
部分が差込まれており、定燃料室の燃料を吸気通路に送
る燃料通路が柱状部分から胴体に亘って形成されている
汎用エンジン用気化器について、前述の問題が伴なわな
いものとするために、本発明は先ず胴体と柱状部分とを
別体として胴体を金属で作るとともに柱状部分を合成樹
脂で作り、燃料通路の燃料溜りが合成樹脂部分に形成さ
れているものとした。
A fuel container forming a constant fuel chamber is mounted below a body having a lateral intake passage, and a columnar portion extending below the body is inserted into the inside of the fuel container. In order to avoid the above-mentioned problems, a carburetor for a general-purpose engine, in which a fuel passage for feeding fuel in a constant fuel chamber to an intake passage extends from a columnar portion to a fuselage, the present invention relates to a fuselage. The main body is made of metal and the columnar part is made of synthetic resin, and the fuel reservoir of the fuel passage is formed in the synthetic resin part.

【0010】このように、金属よりも熱伝導度が低い材
料である合成樹脂で作った柱状部分の内部に燃料溜りが
形成され、且つこの柱状部分は燃料容器に差込まれて燃
料に下半部が浸漬していることにより、エンジン停止後
の高温の熱が燃料溜りに伝わりにくく、従って燃料の蒸
発が少量にとどめられるか、または大量に蒸発すること
があっても再始動時に導入された燃料の蒸発が抑制され
て高温再始動を容易確実なものとすることが可能とな
る。
As described above, a fuel reservoir is formed inside a columnar portion made of a synthetic resin, which is a material having a lower thermal conductivity than metal, and this columnar portion is inserted into a fuel container to lower the fuel. Due to the immersion of the part, the high-temperature heat after the engine is stopped is difficult to be transmitted to the fuel pool, and therefore, the fuel evaporation is introduced at the restart even if the evaporation of the fuel is small or large. Evaporation of fuel is suppressed, and high-temperature restart can be easily and reliably performed.

【0011】また、吸気マニホルドに接続される胴体は
金属製であるため充分な機械的強度を有しており、変形
しないとともに絞り弁などの機能部品を安定よく取り付
けることができる。
Further, since the body connected to the intake manifold is made of metal, it has a sufficient mechanical strength, does not deform, and can stably mount a functional part such as a throttle valve.

【0012】そして、本発明は前記のようにしたうえ
で、第一に柱状部分の上端にフランジを一体に設け、フ
ランジの外側周縁部を胴体と燃料容器との間に挟み込む
とともに柱状部分の下端を燃料容器の底壁に接触させ、
胴体と燃料容器とをフランジの外側方においてねじによ
り結合することによって、胴体の下面と柱状部分および
フランジの上面とを互いに全面密着状態で重ね合わせ
た。
In the present invention, as described above, first, a flange is integrally provided at the upper end of the columnar portion, the outer peripheral edge of the flange is sandwiched between the body and the fuel container, and the lower end of the columnar portion is provided. Contact the bottom wall of the fuel container,
By connecting the body and the fuel container by screws on the outside of the flange, the lower surface of the body and the columnar portion and the upper surface of the flange were overlapped with each other in a state of being in close contact with each other.

【0013】このように、フランジの外側周縁部とその
中心部に位置する柱状部分とがねじの締付け力を燃料容
器を介して間接的に受けて胴体に押し付けられるものと
したことにより、ねじによる強い圧縮応力を直接受けて
変形、破損するという心配がなくなるとともに、胴体の
下面に全面で均等な荷重で重ね合わせられることによ
り、この合わせ面を通る燃料通路が気・液密であって漏
れの心配がないものとされる。
As described above, the outer peripheral portion of the flange and the columnar portion located at the center thereof are indirectly subjected to the tightening force of the screw via the fuel container and are pressed against the body, whereby the screw is used. There is no need to worry about deformation and breakage due to direct compression stress, and the entire lower surface of the fuselage is superimposed with an even load. Don't worry.

【0014】次に、第二に前記第一のものにおいて、合
わせ面の外側周縁部分およびこの合わせ面を通る燃料通
路のそれぞれを囲んでシール部片を設置した。
Secondly, in the first embodiment, a seal piece is provided so as to surround the outer peripheral portion of the mating surface and each of the fuel passages passing through the mating surface.

【0015】このシール部片は合わせ面自身および燃料
通路の気密性、液密性を更に向上させることが可能とな
る。
The sealing piece can further improve the air-tightness and liquid-tightness of the mating surface itself and the fuel passage.

【0016】更に、第三に前記第一のものにおいて燃料
通路の内で低速燃料通路の一部、或いは第四に前記第三
のものに加えて燃料を定燃料室に送る燃料供給通路の一
部を合わせ面に形成し、そしてこの合わせ面と主燃料通
路の合わせ面貫通個所と溝通路とをそれぞれシール部片
で囲んだ。
Further, thirdly, a part of the low-speed fuel passage in the fuel passage of the first fuel supply passage, or fourthly, a fuel supply passage for feeding fuel to the constant fuel chamber in addition to the third fuel passage. A part was formed in the mating surface, and the mating surface, the mating surface penetration of the main fuel passage and the groove passage were each surrounded by a sealing piece.

【0017】このように、胴体と柱状部分およびフラン
ジとの合わせ面を利用して溝を作り、これを燃料が流れ
る通路の一部としたことにより、多方向からのドリル加
工数が大幅に減少し、加えて燃料通路が互いに接近して
いる柱状部分が合成樹脂製であることとシール部片で囲
んだこととが相俟って短絡、漏れの心配が全くない信頼
性あるものとすることができる。
As described above, a groove is formed by using the mating surface of the body, the columnar portion, and the flange, and the groove is formed as a part of the passage through which the fuel flows, thereby greatly reducing the number of drilling operations from multiple directions. In addition, since the columnar portions where the fuel passages are close to each other are made of synthetic resin and surrounded by a sealing piece, there is no need to worry about short-circuiting and leakage, and reliability should be ensured. Can be.

【0018】[0018]

【発明の実施の形態】図面を参照して本発明の実施の形
態を説明すると、金属、一般にはアルミニウムのダイカ
スト鋳造品である胴体1は前後に貫通した横向きの吸気
通路2を有しており、この吸気通路2には入口から出口
に向かって順にチョーク弁3,ベンチュリ4,絞り弁5
が設けられている。チョーク弁3および絞り弁5の各弁
軸3a,5aは胴体1に形成した軸受孔に嵌装支持され
ており、これらの軸端に団結したチョーク弁レバー6,
絞り弁レバー7によってチョーク弁3,絞り弁5が開閉
動作することは通常の気化器と同じである。また、胴体
1には吸気通路2の通路長を直径とする円形の平面から
なる下面8が形成されている。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Referring to the drawings, an embodiment of the present invention will be described. A body 1, which is a die-cast product of metal, generally aluminum, has a lateral intake passage 2 penetrating front and rear. The choke valve 3, the venturi 4, and the throttle valve 5 are arranged in this intake passage 2 in order from the inlet to the outlet.
Is provided. The valve shafts 3a, 5a of the choke valve 3 and the throttle valve 5 are fitted and supported in bearing holes formed in the body 1, and the choke valve levers 6, 6,
The opening and closing of the choke valve 3 and the throttle valve 5 by the throttle valve lever 7 is the same as in a normal carburetor. Further, a lower surface 8 formed of a circular flat surface whose diameter is the passage length of the intake passage 2 is formed on the body 1.

【0019】柱状部分11は上端に下面8よりも少し小
径の円板状のフランジ12を一体に有しており、これら
は硬質合成樹脂の成形品である。また、柱状部分11と
フランジ12の上面13は円形の平面に形成されてい
る。
The columnar portion 11 integrally has a disk-shaped flange 12 slightly smaller in diameter than the lower surface 8 at the upper end, and these are molded products of a hard synthetic resin. The columnar portion 11 and the upper surface 13 of the flange 12 are formed in a circular plane.

【0020】燃料容器15は上端に外径が下面8と同一
径の取付フランジ16を有する椀形であって、周側壁1
5aから取付フランジ16に移行する上端内側周面部分
にフランジ12の厚さとほぼ同一高さであってこれより
も僅かに大径の段部17が形成されており、一般には金
属板の深絞り成形品である。
The fuel container 15 is bowl-shaped and has a mounting flange 16 having an outer diameter equal to that of the lower surface 8 at the upper end.
A step portion 17 having a height substantially equal to the thickness of the flange 12 and slightly larger than the thickness of the flange 12 is formed on the inner peripheral surface of the upper end transitioning from 5 a to the mounting flange 16. It is a molded product.

【0021】そして、柱状部分11の下端を燃料容器1
5の底壁15bの中心部に接触させ且つフランジ12の
外側周縁部を段部17に嵌装した状態で下面8と上面1
3とを重ねるとともに、下面8のフランジ12外側方に
露出した部分に取付フランジ16を重ね、フランジ12
の外側方において取付フランジ16から胴体1にねじ1
8をねじ込むことによって燃料容器15が胴体1に結合
されている。
Then, the lower end of the columnar portion 11 is
5 and the upper surface 1 and the lower surface 1 in a state where the outer peripheral edge of the flange 12 is fitted to the step portion 17 while being in contact with the center of the bottom wall 15b.
3 and the mounting flange 16 is overlapped with the portion of the lower surface 8 exposed to the outside of the flange 12,
Screw 1 from the mounting flange 16 to the fuselage 1
The fuel container 15 is connected to the fuselage 1 by screwing 8.

【0022】下面8と上面13とは互いに密着して合わ
せ面19を形成し、この合わせ面19はねじ18のねじ
込みによってフランジ12の周縁部分が段部17で押さ
れると同時に中心部分の柱状部分11が底壁15bで押
されることによって、全面でほぼ均等な密着状態とな
る。また、フランジ12はねじ18の締付け力を直接受
けることなく間接的に受け、且つ段部17の内部で逃げ
ることができるので変形、破損を生じる心配なく組付け
られるばかりか、高温と低温が繰返されても強い応力作
用部分がないため変形を生じることがなく、合わせ面1
9の全面密着性が確保されるものである。
The lower surface 8 and the upper surface 13 are in close contact with each other to form a mating surface 19, and the mating surface 19 is pushed by the screw 18 so that the peripheral portion of the flange 12 is pushed by the step 17, and at the same time, a columnar portion at the center is formed. 11 is pressed by the bottom wall 15b, so that an almost uniform contact state is achieved over the entire surface. Further, the flange 12 can be indirectly received without directly receiving the tightening force of the screw 18 and can escape inside the stepped portion 17, so that not only there is no fear of deformation and breakage, but also high and low temperatures are repeated. No deformation occurs because there is no strong stress acting part.
No. 9 ensures the overall adhesion.

【0023】燃料容器15の内部は定燃料室20を形成
しており、その中心部分に柱状部分11が差込まれてい
る。定燃料室20にはピン21に片持ち式に支持させた
浮子22が装入されており、この浮子22に取付けた燃
料弁23がフランジ12に固着した弁座体24に嵌め込
まれている。
The interior of the fuel container 15 forms a constant fuel chamber 20, into which a columnar portion 11 is inserted. The fixed fuel chamber 20 is provided with a float 22 supported by a pin 21 in a cantilever manner, and a fuel valve 23 attached to the float 22 is fitted into a valve seat 24 fixed to the flange 12.

【0024】図示しない燃料タンクより燃料ポンプを経
て送られてくる燃料は、胴体1の一側方に突出させた接
手管26a,胴体1の孔通路26b,下面8に下向きに
開放して形成された溝通路26c,フランジ12の孔通
路26dからなる燃料供給通路26によって弁座体24
の入口に達し、定燃料室20の油面変化に伴って上下動
する燃料弁23の開閉動作に応じて定燃料室20に供給
される。このことにより、定燃料室20に一定量の燃料
が保有されることは通常の浮子式気化器と同じである。
Fuel supplied from a fuel tank (not shown) via a fuel pump is formed by opening downwardly to a joint pipe 26a protruding to one side of the body 1, a hole passage 26b of the body 1 and the lower surface 8. The fuel supply passage 26, which is formed by the groove passage 26c and the hole passage 26d of the flange 12, forms a valve seat 24.
And is supplied to the constant fuel chamber 20 according to the opening / closing operation of the fuel valve 23 which moves up and down in accordance with a change in the oil level of the constant fuel chamber 20. As a result, a constant amount of fuel is held in the constant fuel chamber 20 in the same manner as a normal float type carburetor.

【0025】燃料容器15の底壁15bの中心部には電
磁駆動の燃料遮断弁28が取付けられており、その弁体
29は柱状部分11の下端部に形成した弁室30に突出
して燃料通路33の入口に設けた主ジェット32の入口
端をエンジン停止時に閉止し、エンジン運転時に開放し
て定燃料室20から弁室30に入った燃料を主ジェット
32で計量して燃料通路33に送入させる。
An electromagnetically driven fuel cutoff valve 28 is mounted at the center of the bottom wall 15b of the fuel container 15, and its valve body 29 projects into a valve chamber 30 formed at the lower end of the columnar portion 11 to protrude into the fuel passage. The inlet end of the main jet 32 provided at the inlet of the engine 33 is closed when the engine is stopped, and is opened during operation of the engine, and the fuel that has entered the valve chamber 30 from the constant fuel chamber 20 is measured by the main jet 32 and sent to the fuel passage 33. To enter.

【0026】燃料通路33は主ジェット32から上方へ
延び柱状部分11,胴体1を通ってベンチュリ4の最狭
部分に達する直線状の主燃料通路34と、主ジェット3
2の出口端で主燃料通路34から分岐して絞り弁5の側
方にスローポート46を開口させているスローポート室
45に達する低速燃料通路42との二系統によって構成
されている。
The fuel passage 33 extends upward from the main jet 32 and extends through the columnar portion 11 and the body 1 to reach the narrowest portion of the venturi 4.
2 and a low-speed fuel passage 42 that branches off from the main fuel passage 34 and reaches a slow port chamber 45 that opens a slow port 46 to the side of the throttle valve 5.

【0027】主燃料通路34は柱状部分11および胴体
1に連続して設けた縦方向に延びる取付孔35に挿入し
たエマルジョン管36と、その上方部分に一体形成され
て胴体1の取付孔35部分に圧接状態で嵌め込まれた主
ノズル37とを有しており、エマルジョン管36の下端
に主ジェット32の出口端に接してこれを取付孔35の
底に定着させている。
The main fuel passage 34 has an emulsion pipe 36 inserted into a vertically extending mounting hole 35 provided continuously with the columnar portion 11 and the body 1, and is integrally formed at an upper portion thereof with a portion of the mounting hole 35 of the body 1. And a main nozzle 37 fitted in a pressure contact state with the outlet end of the main jet 32 at the lower end of the emulsion tube 36 and fixing it to the bottom of the mounting hole 35.

【0028】また、胴体1の吸気通路2上流側端面に入
口端の空気ジェット39を開口させた主ブリード空気通
路40が取付孔35に接続されており、これより取付孔
35に入った空気はエマルジョン管33に入った燃料と
混合し、主ノズル37から吸気通路2に送出される。こ
の主ブリード空気通路40は胴体1の前後方向の孔通路
40a,縦方向の孔通路40b,下面8に形成した溝通
路40cからなり、溝通路40cが取付孔35に連通し
ている。
A main bleed air passage 40 having an air jet 39 at the inlet end is connected to the mounting hole 35 at the upstream end face of the air intake passage 2 of the body 1 so that the air entering the mounting hole 35 is The fuel is mixed with the fuel contained in the emulsion pipe 33 and sent out from the main nozzle 37 to the intake passage 2. The main bleed air passage 40 includes a hole passage 40 a in the front-rear direction of the body 1, a hole passage 40 b in the vertical direction, and a groove passage 40 c formed in the lower surface 8, and the groove passage 40 c communicates with the mounting hole 35.

【0029】低速燃料通路42は主ジェット32の出口
端である取付孔35の底部から横方向へ分岐して延びる
横通路42a,柱状部分11の内部を取付孔35と平行
に上方へ延びる孔通路42b,下面8に形成した溝通路
42c,胴体1の吸気通路2側方を上方へ延びる孔通路
42d,胴体1の前後方向へ延びる孔通路42eからな
り、孔通路42dは低速ジェット43を嵌め込み装着し
ているとともに孔通路42eはスローポート室45に連
通している。
The low-speed fuel passage 42 is a lateral passage 42a extending laterally from the bottom of the mounting hole 35, which is the outlet end of the main jet 32, and a hole passage extending upward inside the columnar portion 11 in parallel with the mounting hole 35. 42b, a groove passage 42c formed in the lower surface 8, a hole passage 42d extending upward on the side of the intake passage 2 of the body 1, and a hole passage 42e extending in the front-rear direction of the body 1. The hole passage 42d is fitted with the low-speed jet 43. The hole passage 42e communicates with the slow port chamber 45.

【0030】主ジェット32からエマルジョン管36に
入った燃料の一部は直ちに取付孔35の底部から低速燃
料通路42に流入し、低速ジェット43で計量されてス
ローポート46から吸気通路2に送出される。孔通路4
2eのスローポート室45と反対側の延長上には、胴体
1の吸気通路2上流側端面に入口端の空気ジェット48
を開口させた低速ブリード空気通路49が設けられてお
り、低速ジェット43で計量された燃料にブリード空気
が混入する。
A part of the fuel that has entered the emulsion pipe 36 from the main jet 32 immediately flows into the low-speed fuel passage 42 from the bottom of the mounting hole 35, is measured by the low-speed jet 43, and is sent out from the slow port 46 to the intake passage 2. You. Hole passage 4
On the extension of 2e opposite to the slow port chamber 45, an air jet 48 at the inlet end is provided on the upstream end surface of the intake passage 2 of the body 1.
A low-speed bleed air passage 49 having an opening is provided, and bleed air mixes with the fuel measured by the low-speed jet 43.

【0031】この実施の形態によると、主燃料通路34
のエマルジョン管36の部分、低速燃料通路42の横通
路42aと孔通路42bの下半部分とがそれぞれ形成す
る燃料溜り38,44は合成樹脂で作られた柱状部分1
1の内部に設けられており、且つ柱状部分11は下半部
が定燃料室20の燃料に浸漬されていることにより、エ
ンジンを停止したときエンジン自身およびその周辺が高
温度であっても蒸発が少量にとどめられる。また胴体1
から主ノズル管37,エマルジョン管36が受ける熱に
よって大量に蒸発することがあっても、再始動時に導入
された燃料の蒸発はごく少量に押さえられて高温再始動
を容易確実なものとすることができる。
According to this embodiment, the main fuel passage 34
The fuel reservoirs 38 and 44 formed by the portion of the emulsion pipe 36, the lateral passage 42a of the low-speed fuel passage 42, and the lower half of the hole passage 42b are columnar portions 1 made of synthetic resin.
1, and the lower half of the columnar portion 11 is immersed in the fuel in the constant fuel chamber 20, so that when the engine is stopped, even if the engine itself and its surroundings are at a high temperature, the columnar portion 11 evaporates. Are kept in small quantities. Also body 1
Therefore, even if a large amount of fuel is evaporated by the heat received by the main nozzle pipe 37 and the emulsion pipe 36, the evaporation of the fuel introduced at the time of restarting is suppressed to a very small amount, and high-temperature restarting can be easily and reliably performed. Can be.

【0032】また、吸気マニホルドに接続される胴体1
は金属製であるために充分な機械的強度を有していると
ともに、チョーク弁3,絞り弁5,主ノズル37を安定
よく取り付けることができる。一方、機械的強度に劣る
合成樹脂で作られている柱状部分11は、胴体1の下面
8と燃料容器15の底壁15bとに挟み込まれているこ
とと、胴体1に固定された主ノズル37,エマルジョン
管36を補強部材としていることによって、変形するこ
となく所定の形状に保持される。そしてまた、このこと
により、柱状部分11の内部の主ジェット32も安定よ
く取り付けられる。
The body 1 connected to the intake manifold
Since it is made of metal, it has a sufficient mechanical strength and can stably mount the choke valve 3, the throttle valve 5, and the main nozzle 37. On the other hand, the columnar portion 11 made of a synthetic resin having poor mechanical strength is sandwiched between the lower surface 8 of the body 1 and the bottom wall 15b of the fuel container 15, and the main nozzle 37 fixed to the body 1 By using the emulsion tube 36 as a reinforcing member, the emulsion tube 36 is maintained in a predetermined shape without deformation. This also allows the main jet 32 inside the columnar portion 11 to be stably attached.

【0033】更に、柱状部分11の内部で互いに接近し
て配置される取付孔35と孔通路42bとは、鋳巣に相
当する気泡を散在させることのない合成樹脂成形品に形
成されているので、短絡してそれぞれの機能を損うとい
う心配がない。
Further, since the mounting hole 35 and the hole passage 42b which are arranged close to each other inside the columnar portion 11 are formed in a synthetic resin molded product in which bubbles corresponding to the cavities are not scattered. There is no need to worry about short-circuiting and impairing each function.

【0034】一方、この実施の形態によると、燃料供給
通路26の孔通路26bは胴体1の側面および下面8か
らのドリル加工により、孔通路26dは柱状部分11の
成形用金型の例えばリターンピンを利用することにより
それぞれ形成することができる。また。主燃料通路34
の取付孔35および低速燃料通路42の孔通路42bは
胴体1の鋳型や柱状部分11の成形用金型にピンを設け
ることにより且つ必要がありばドリル加工を施すことに
より形成することができる。更に、主ブリード空気通路
40の孔通路40a,40bは胴体1の前面および下面
8からのドリル加工により、低速燃料通路42の孔通路
42dは下面8からのドリル加工により、孔通路42e
および低速ブリード空気通路49は胴体1の前面からの
ドリル加工により、それぞれ形成することができる。
On the other hand, according to this embodiment, the hole passage 26b of the fuel supply passage 26 is formed by drilling from the side surface and the lower surface 8 of the body 1, and the hole passage 26d is formed by, for example, a return pin of a molding die for the columnar portion 11. Each of them can be formed by utilizing. Also. Main fuel passage 34
The mounting hole 35 and the hole passage 42b of the low-speed fuel passage 42 can be formed by providing pins in a mold of the body 1 or a molding die of the columnar portion 11, and by drilling if necessary. Further, the hole passages 40a and 40b of the main bleed air passage 40 are drilled from the front surface and the lower surface 8 of the body 1, and the hole passage 42d of the low-speed fuel passage 42 is drilled from the lower surface 8 by the hole passage 42e.
The low-speed bleed air passage 49 can be formed by drilling from the front surface of the body 1.

【0035】そして、溝通路26c,40c,42cは
胴体1の鋳型に突起を設けることにより形成することが
できるので、ドリル加工により形成される低速燃料通路
42の横通路42aの端面を閉止処理するのみで、燃料
やブリード空気が流れる全ての通路26,34,40,
42,49を少ない加工工数で漏れの心配がないものに
することができる。
Since the groove passages 26c, 40c and 42c can be formed by providing projections on the mold of the body 1, the end face of the lateral passage 42a of the low-speed fuel passage 42 formed by drilling is closed. All the passages 26, 34, 40,
42 and 49 can be reduced in number of processing steps and without fear of leakage.

【0036】尚、低速燃料通路42の溝通路42cの容
積はきわめて小さいので、エンジン停止時にこの部分の
燃料が蒸発しても再始動時に直ちに補充されて高温再始
動を妨げない。
Since the volume of the groove passage 42c of the low-speed fuel passage 42 is extremely small, even if the fuel in this portion evaporates when the engine is stopped, it is replenished immediately upon restart and does not hinder high-temperature restart.

【0037】更に、合わせ面19は前述のように前面ほ
ぼ均等な密着状態とされ、この部分に存在する取付孔3
5および溝通路26c,40c,42cは互いに気・液
密性を有しているが、本発明ではこのことを更に信頼性
あるものにするため、シール部材51を具えさせた。図
示実施の形態では、前記に加えてチョーク弁軸3a,絞
り弁軸5aの下面8への開放端面の気密性も併せて向上
させるために、シール部材51をこれらをそれぞれ囲む
とともにこれらの外側で合わせ面19のほぼ全体を囲む
ように作られたシール部片を互いに連結して一体品とし
た0リングからなるものとし、下面8に装着して合成樹
脂製の柱状部分11,フランジ12の上面13との密着
状態を更に良好なものとした。
Further, as described above, the mating surface 19 is brought into substantially uniform contact with the front surface.
5 and the groove passages 26c, 40c, 42c are gas- and liquid-tight, but the present invention is provided with a sealing member 51 to make this more reliable. In the illustrated embodiment, in addition to the above, in order to also improve the airtightness of the open end faces of the choke valve shaft 3a and the throttle valve shaft 5a to the lower surface 8, the seal members 51 are respectively surrounded and surrounded outside. A seal piece formed so as to surround almost the entire mating surface 19 is connected to each other to form an integrated O-ring, and is attached to the lower surface 8 and is attached to the lower surface 8 of the columnar portion 11 made of synthetic resin and the upper surface of the flange 12. 13 was further improved.

【0038】即ち、このシール部材51は合わせ面19
の外側周縁部分に配置されてそのほぼ全体を囲む円形の
シール部片51a,溝通路26cを囲むほぼ長円形のシ
ール部片51b,取付孔35と溝通路40cとを囲むほ
ぼ長円形のシール部片51c,溝通路42cを囲むほぼ
長円形のシール部片51d,チョーク弁軸3aと絞り弁
軸5aの開放端面をそれぞれ囲む円形のシール部片51
e,51fを互いに連結して一体品としたものであり、
下面8に設けたシール部材51の形状と合致する溝にそ
のまま嵌め込まれている。このように各シール部片51
a…51fを一体化すると、取扱いが容易で下面8への
装着が一挙に行なえるばかりか、連結部分が気・液密性
の更なる向上に役立つという利点がある。
That is, the sealing member 51 is
And a substantially oval sealing portion 51b surrounding the groove passage 26c, and a substantially oval sealing portion surrounding the mounting hole 35 and the groove passage 40c. Piece 51c, a substantially elliptical seal piece 51d surrounding the groove passage 42c, and a circular seal piece 51 surrounding the open end faces of the choke valve shaft 3a and the throttle valve shaft 5a, respectively.
e, 51f are connected to each other to form an integral product,
It is fitted directly into a groove that matches the shape of the seal member 51 provided on the lower surface 8. Thus, each seal piece 51
When a ... 51f is integrated, there is an advantage that not only the handling is easy and the mounting to the lower surface 8 can be performed at once, but also that the connecting portion helps to further improve the gas-liquid tightness.

【0039】尚、溝通路26c,40c,42cは柱状
部分11,フランジ12の上面13に形成すること、或
いは下面8と上面13の両方に浅い溝を向かい合わせに
設けて形成することがある。また、燃料供給通路26は
レイアウトによっては溝通路26cを設けることなく孔
通路26b,26dを直接連通させる場合がある。更
に、主ブリード空気通路40は胴体1に斜め直線状に形
成して溝通路40cを経ることなく取付孔35に接続さ
せる場合がある。更にまた、柱状部分11の下端は燃料
遮断弁28の弁本体に接触させることにより、燃料容器
15の底壁15bに間接的に接触させた構造とすること
がある。
The groove passages 26c, 40c and 42c may be formed on the columnar portion 11 and the upper surface 13 of the flange 12, or may be formed by providing shallow grooves on both the lower surface 8 and the upper surface 13 so as to face each other. The fuel supply passage 26 may directly communicate the hole passages 26b and 26d without providing the groove passage 26c depending on the layout. Further, there is a case where the main bleed air passage 40 is formed obliquely straight in the body 1 and connected to the mounting hole 35 without passing through the groove passage 40c. Further, the lower end of the columnar portion 11 may be in contact with the valve body of the fuel cutoff valve 28 so as to be indirectly in contact with the bottom wall 15b of the fuel container 15.

【0040】[0040]

【発明の効果】以上のように、吸気通路を有する胴体を
金属で作るとともに燃料溜りが形成される柱状部分を合
成樹脂で作ったことにより、機械的強度を損うことがな
いとともに高温再始動性が良好なものとすることができ
る。また、柱状部分と一体のフランジおよび柱状部分自
身を胴体と燃料容器とに挟んでこれらを結合するねじの
締付け力を直接受けさせないものとしたため、強度的に
劣る柱状部分更にはフランジに変形や破損を生じさせる
心配をなくし、胴体と柱状部分およびフランジとの合わ
せ面の全面を密着させて燃料やブリード空気の漏れがな
いものとすることができる。更に、合わせ面を利用して
燃料やブリード空気の通路を少ない加工工数で形成でき
るとともに、この合わせ面にシール部材を設けることに
より、気・液密性にすぐれ漏れの心配がない通路構造と
することができる。
As described above, the body having the intake passage is made of metal, and the columnar portion where the fuel reservoir is formed is made of synthetic resin. The property can be good. In addition, since the flange integrated with the columnar portion and the columnar portion itself are sandwiched between the body and the fuel container and are not directly subjected to the tightening force of the screws connecting them, the columnar portion, which is inferior in strength, and the flange are deformed or damaged. And the entire surface of the mating surface of the body and the columnar portion and the flange is brought into close contact with each other to prevent leakage of fuel and bleed air. Further, the passage for fuel and bleed air can be formed with a small number of processing steps by using the mating surface, and by providing a sealing member on the mating surface, the passage structure is excellent in air / liquid tightness and has no fear of leakage. be able to.

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

【図1】本発明の実施の形態を示す縦断面図。FIG. 1 is a longitudinal sectional view showing an embodiment of the present invention.

【図2】図1のA−A線に沿う断面図。FIG. 2 is a sectional view taken along the line AA in FIG. 1;

【図3】図1のB−B線に沿う断面部分図。FIG. 3 is a partial sectional view taken along the line BB of FIG. 1;

【図4】図1のC−C線に沿う断面部分図。FIG. 4 is a partial sectional view taken along the line CC of FIG. 1;

【図5】図1の横断面図。FIG. 5 is a cross-sectional view of FIG.

【図6】図1の形態における胴体の下面図。FIG. 6 is a bottom view of the body in the embodiment of FIG. 1;

【符号の説明】[Explanation of symbols]

1 胴体,2 吸気通路,8 下面,11 柱状部分,
12 フランジ,13上面,15 燃料容器,18 ね
じ,19 合わせ面,20 定燃料室,26燃料供給通
路,26c,40c,42c 溝通路,28 燃料遮断
弁,33燃料通路,34 主燃料通路,38,44 燃
料溜り,40 主ブリード空気通路,42 低速燃料通
路,51 シール部材,
1 body, 2 intake passage, 8 bottom surface, 11 columnar part,
12 Flange, 13 upper surface, 15 fuel container, 18 screw, 19 mating surface, 20 constant fuel chamber, 26 fuel supply passage, 26c, 40c, 42c groove passage, 28 fuel cutoff valve, 33 fuel passage, 34 main fuel passage, 38 , 44 fuel reservoir, 40 main bleed air passage, 42 low speed fuel passage, 51 seal member,

Claims (5)

【特許請求の範囲】[Claims] 【請求項1】 横向きの吸気通路を有する胴体の下に定
燃料室を形成する燃料容器が取り付けられているととも
に、前記燃料容器の内部に前記胴体の下方へ延びる柱状
部分が差し込まれており、前記定燃料室の燃料を前記吸
気通路に送る燃料通路が前記柱状部分から前記胴体に亘
って形成されている汎用エンジン用気化器において、 前記胴体と柱状部分とが別体であって前記胴体は金属で
作られ、前記燃料通路の燃料溜りが存在する前記柱状部
分は合成樹脂で作られていて上端にフランジを一体に有
しており、前記フランジの外側周縁部が前記胴体と燃料
容器との間に挟み込まれるとともに前記柱状部分の下端
が前記燃料容器の底壁に接触した状態で前記胴体と燃料
容器とが前記フランジの外側方においてねじにより結合
されることによって、前記胴体の下面と前記柱状部分お
よびフランジの上面とが互いに全面密着状態で重ね合わ
せられている、 ことを特徴とする汎用エンジン用気化器。
1. A fuel container forming a constant fuel chamber is attached below a body having a lateral intake passage, and a columnar portion extending downward from the body is inserted into the fuel container. In a general-purpose engine carburetor in which a fuel passage that sends fuel from the constant fuel chamber to the intake passage is formed from the columnar portion to the body, the body and the columnar portion are separate bodies, and the body is The columnar portion, which is made of metal and in which the fuel reservoir of the fuel passage is present, is made of synthetic resin and has a flange integrally at an upper end, and an outer peripheral portion of the flange is formed between the body and the fuel container. The body and the fuel container are screwed on the outside of the flange while being sandwiched therebetween and the lower end of the columnar portion is in contact with the bottom wall of the fuel container. Carburetor for general-purpose engines, characterized in that, the upper surface of the columnar portion and the flange and the lower surface of the body are superposed on the entire surface close contact with each other.
【請求項2】 請求項1に記載した汎用エンジン用気化
器において、 前記胴体と前記柱状部分およびフランジとの合わせ面の
外側周縁部分を囲んでシール部片が設けられているとと
もに、前記合わせ面を通る燃料通路を囲んでシール部片
が設けられている、 ことを特徴とする汎用エンジン用気化器。
2. The carburetor for a general-purpose engine according to claim 1, wherein a seal piece is provided around an outer peripheral portion of a mating surface between the body and the columnar portion and the flange, and the mating surface is provided. A seal piece surrounding a fuel passage passing therethrough.
【請求項3】 請求項1に記載した汎用エンジン用気化
器において、 前記燃料通路の内で低速燃料通路の一部が前記胴体と前
記柱状部分およびフランジとの合わせ面に設けた溝通路
によって形成されており、前記合わせ面の外側周縁部分
を囲んでシール部片が設けられているとともに、主燃料
通路の前記合わせ面貫通個所と前記溝通路とをそれぞれ
囲んでシール部片が設けられている、 ことを特徴とする汎用エンジン用気化器。
3. The carburetor for a general-purpose engine according to claim 1, wherein a part of the low-speed fuel passage in the fuel passage is formed by a groove passage provided on a mating surface between the body, the columnar portion, and the flange. And a seal piece surrounding the outer peripheral portion of the mating surface, and a seal piece surrounding the mating surface penetrating portion of the main fuel passage and the groove passage, respectively. A carburetor for a general-purpose engine.
【請求項4】 請求項1に記載した汎用エンジン用気化
器において、 燃料を前記定燃料室に送る燃料供給通路の一部および前
記燃料通路の内で低速燃料通路の一部が前記胴体と前記
柱状部分およびフランジとの合わせ面に設けた溝通路に
よってそれぞれ形成されており、前記合わせ面の外側周
縁部分を囲んでシール部片が設けられているとともに、
主燃料通路の前記合わせ面貫通個所と前記二つの溝通路
とをそれぞれ囲んでシール部片が設けられている、 ことを特徴とする汎用エンジン用気化器。
4. The carburetor for a general-purpose engine according to claim 1, wherein a part of a fuel supply passage for sending fuel to the constant fuel chamber and a part of a low-speed fuel passage in the fuel passage are connected to the body and the body. Each is formed by a groove passage provided on a mating surface with the columnar portion and the flange, and a sealing piece is provided around an outer peripheral portion of the mating surface,
A carburetor for a general-purpose engine, characterized in that a seal piece is provided so as to surround the joint portion of the main fuel passage and the two groove passages.
【請求項5】 前記それぞれの囲みを形成する複数のシ
ール部片は互いに連結され一体品とされている請求項
2,3または4に記載した汎用エンジン用気化器。
5. The carburetor for a general-purpose engine according to claim 2, wherein the plurality of seal pieces forming the respective enclosures are connected to each other to form an integral product.
JP20247199A 1999-07-16 1999-07-16 General-purpose engine carburetor Expired - Lifetime JP3836635B2 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
JP20247199A JP3836635B2 (en) 1999-07-16 1999-07-16 General-purpose engine carburetor
US09/616,497 US6435482B1 (en) 1999-07-16 2000-07-13 Carburetor for a general purpose engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP20247199A JP3836635B2 (en) 1999-07-16 1999-07-16 General-purpose engine carburetor

Publications (2)

Publication Number Publication Date
JP2001027154A true JP2001027154A (en) 2001-01-30
JP3836635B2 JP3836635B2 (en) 2006-10-25

Family

ID=16458081

Family Applications (1)

Application Number Title Priority Date Filing Date
JP20247199A Expired - Lifetime JP3836635B2 (en) 1999-07-16 1999-07-16 General-purpose engine carburetor

Country Status (1)

Country Link
JP (1) JP3836635B2 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007192150A (en) * 2006-01-20 2007-08-02 Nikki Co Ltd Carburetor
JP2012067618A (en) * 2010-09-21 2012-04-05 Nikki Co Ltd Carburetor
US8333366B2 (en) 2010-03-08 2012-12-18 Briggs & Stratton Corporation Carburetor including one-piece fuel-metering insert

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104454243B (en) * 2014-12-04 2017-04-19 苏州圆能动力科技有限公司 Anti-toppling carburetor structure based on external fuel oil container

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007192150A (en) * 2006-01-20 2007-08-02 Nikki Co Ltd Carburetor
US8333366B2 (en) 2010-03-08 2012-12-18 Briggs & Stratton Corporation Carburetor including one-piece fuel-metering insert
US8573567B2 (en) 2010-03-08 2013-11-05 Briggs & Stratton Corporation Carburetor including one-piece fuel-metering insert
JP2012067618A (en) * 2010-09-21 2012-04-05 Nikki Co Ltd Carburetor

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