JPS6147299B2 - - Google Patents

Info

Publication number
JPS6147299B2
JPS6147299B2 JP6257480A JP6257480A JPS6147299B2 JP S6147299 B2 JPS6147299 B2 JP S6147299B2 JP 6257480 A JP6257480 A JP 6257480A JP 6257480 A JP6257480 A JP 6257480A JP S6147299 B2 JPS6147299 B2 JP S6147299B2
Authority
JP
Japan
Prior art keywords
fuel
passage
valve
starting
air
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.)
Expired
Application number
JP6257480A
Other languages
Japanese (ja)
Other versions
JPS56159541A (en
Inventor
Toshikatsu Nozaki
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Yamaha Motor Co Ltd
Original Assignee
Yamaha Motor Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Yamaha Motor Co Ltd filed Critical Yamaha Motor Co Ltd
Priority to JP6257480A priority Critical patent/JPS56159541A/en
Publication of JPS56159541A publication Critical patent/JPS56159541A/en
Publication of JPS6147299B2 publication Critical patent/JPS6147299B2/ja
Granted legal-status Critical Current

Links

Description

【発明の詳細な説明】 この発明はエンジンの冷間始動時における混合
気の空燃比を濃厚にする始動装置に関するもの
で、その構造を簡単にすると共に常温から氷点下
の極低温に至る広い温度範囲に渉つてエンジンの
始動性を向上させることを目的とするものであ
る。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a starting device that enriches the air-fuel ratio of the air-fuel mixture during a cold start of an engine.It has a simple structure and can be used over a wide temperature range from room temperature to extremely low temperatures below freezing. The purpose of this is to improve engine startability over time.

従来、気化器の低温始動装置として絞り弁を側
路する始動用空気通路を設け、これに低温時に開
く始動弁と始動用燃料噴口とを付設した、いわゆ
るバイスタータ方式が知られている。
BACKGROUND ART Conventionally, a so-called bi-starter system has been known as a low-temperature starting device for a carburetor, in which a starting air passage bypassing a throttle valve is provided, and a starting valve that opens at low temperatures and a starting fuel injection port are attached to the starting air passage.

この発明は冷間始動時に、従来の気化器に設け
られるエアブリード付の低速燃料噴口から供給さ
れる低速燃料を増量することにより、吸入される
混合気の空燃比を濃厚にすると共に、始動用の燃
料噴口を特設してクランキングから完爆に至る間
のみ更に燃料を増量し、低温始動性を向上させた
ものである。
This invention increases the amount of low-speed fuel supplied from the low-speed fuel nozzle with air bleed provided in a conventional carburetor during cold starting, enriches the air-fuel ratio of the air-fuel mixture taken in, and improves the starting temperature. A special fuel nozzle was installed to further increase the amount of fuel from cranking to complete explosion, improving low-temperature startability.

以下、図示の実施例によつて本発明を説明す
る。気化器は吸気胴1に形成した吸気通路2と、
人為操作により吸気通路2内へ進退するピストン
形の絞り弁3を有する。4は絞り弁に支持された
針弁、5は針弁4と共働して開口面積を変ずる主
噴口、6は低速燃料噴口である。7は吸気胴1の
下面に設けられた浮子室で、内部の燃料は主燃料
通路8を通して主噴口5と、エマルジヨンチユー
ブ9を有する低速燃料通路10を通して低速燃料
噴口6とへ供給される。11はスローエア通路で
あり、その一端が低速燃料通路10に、また他端
がエアジエツト12を介して大気中にそれぞれ通
じている。13はパイロツトエアスクリユでスロ
ーエア通路を流れるエアブリード量を大小に変
え、空燃比を希薄、濃厚に調節する。14は始動
用空気通路で、スローエア通路11と絞り弁3下
流の吸気通路2内との間に設けられている。15
はその途中に設けられた始動弁である。始動弁1
5は空気通路14中に設けられ、オリフイス状に
絞られた弁座16と、これに対応する円錐状の弁
体17とからなつている。弁体17は背面の案内
筒18によつて弁箱19内を摺動自在に支持され
ており、後端部の外周溝21にはバイメタル22
が係合して、エンジン低温時には弁体17を弁座
16から引離すようになつている。バイメタル2
2の基端はボルト23で弁箱に固着されており、
遊端が前記外周溝21内を軸方向の隙間aの範囲
で移動できる。24はばねでバイメタル22を外
周溝の下端へ押圧している。25はリーク通路
で、弁座16より上流側の始動空気通路14と弁
体17の背面の弁室とを連通して、弁体17の前
面に作用する空気通路14内負圧が上昇(圧力が
低下)するとき、弁座16との間に形成される通
気面積が減じるようにして始動弁15を感圧弁と
して構成してある。
The present invention will be explained below with reference to illustrated embodiments. The carburetor includes an intake passage 2 formed in an intake body 1,
It has a piston-shaped throttle valve 3 that moves forward and backward into the intake passage 2 by manual operation. 4 is a needle valve supported by a throttle valve; 5 is a main nozzle port that cooperates with the needle valve 4 to change the opening area; and 6 is a low-speed fuel nozzle port. Reference numeral 7 denotes a float chamber provided on the lower surface of the intake shell 1, and fuel therein is supplied to the main nozzle 5 through a main fuel passage 8 and to the low-speed fuel nozzle 6 through a low-speed fuel passage 10 having an emulsion tube 9. 11 is a slow air passage, one end of which communicates with the low speed fuel passage 10, and the other end of which communicates with the atmosphere via an air jet 12. 13 is a pilot air screw that changes the amount of air bleed flowing through the slow air passage to adjust the air-fuel ratio to lean or rich. A starting air passage 14 is provided between the slow air passage 11 and the intake passage 2 downstream of the throttle valve 3. 15
is a starting valve installed in the middle. Starting valve 1
5 is provided in the air passage 14 and consists of an orifice-shaped valve seat 16 and a corresponding conical valve body 17. The valve body 17 is supported slidably within the valve box 19 by a guide cylinder 18 on the back side, and a bimetal 22 is provided in an outer circumferential groove 21 at the rear end.
is engaged to pull the valve body 17 away from the valve seat 16 when the engine temperature is low. Bimetal 2
The base end of 2 is fixed to the valve box with bolt 23,
The free end can move within the outer circumferential groove 21 within an axial clearance a. A spring 24 presses the bimetal 22 toward the lower end of the outer circumferential groove. A leak passage 25 communicates the starting air passage 14 on the upstream side of the valve seat 16 with the valve chamber on the back side of the valve body 17, so that the negative pressure inside the air passage 14 acting on the front side of the valve body 17 increases (pressure The starting valve 15 is configured as a pressure sensitive valve so that when the starting valve 15 decreases, the ventilation area formed between the starting valve 15 and the valve seat 16 decreases.

26はエンジンのクランキングから完爆に至る
間の燃料増量のため設けられた始動燃料噴口であ
り、始動弁15の下流の始動用空気通路14から
吸気通路2内に至るいづこかに設けられる。噴口
26は通路27を介して浮子室7内に通じてお
り、通路27にはそれを連通遮断する負圧作動式
の燃料弁28が設けられている。通路27は浮子
室7内においてエマルジヨン管29及び計量管3
1とで略U字形に形成されており、計量管31の
上端はジエツト32を介して浮子室上方に開口し
ている。浮子室7内の燃料は計量管31の側面に
開口した小孔33を通じて通路27内へ入り、エ
ンジン停止時は浮子室7と同レベルを保つてい
る。34は始動燃料ジエツトである。
A starting fuel nozzle 26 is provided to increase the amount of fuel during the period from engine cranking to complete explosion, and is provided anywhere from the starting air passage 14 downstream of the starting valve 15 to the intake passage 2. . The nozzle 26 communicates with the inside of the float chamber 7 via a passage 27, and the passage 27 is provided with a negative pressure operated fuel valve 28 for communicating and cutting off communication therebetween. The passage 27 is connected to the emulsion pipe 29 and the metering pipe 3 in the float chamber 7.
The upper end of the metering tube 31 opens above the float chamber through a jet 32. The fuel in the float chamber 7 enters the passage 27 through a small hole 33 opened on the side of the metering tube 31, and is maintained at the same level as the float chamber 7 when the engine is stopped. 34 is a starting fuel jet.

負圧作動式の燃料弁28は弁体35を背面のば
ね36で押圧して常時通路27を閉じるように作
用する常閉形であり、弁体35の後端には弾膜3
7が連結されている。弾膜37の一側には浮子室
上面に連らなる大気室38が、また、他側には始
動弁15より上流のスローエア通路11に連らな
る負圧室39が形成されている。
The negative pressure operated fuel valve 28 is a normally closed type that presses a valve body 35 with a spring 36 on the back side and acts to close the passage 27 at all times.
7 are connected. An atmospheric chamber 38 connected to the upper surface of the float chamber is formed on one side of the elastic membrane 37, and a negative pressure chamber 39 connected to the slow air passage 11 upstream of the starter valve 15 is formed on the other side.

いま、エンジンあるいは外気が所定の温度以下
になるとバイメタル22は図中上方へ反曲して弁
体17を引上げ、始動用空気通路14を全通す
る。この状態でクランキングすると、空気通路1
4を通してスローエア通路11に絞り弁3下流の
吸気負圧が作用し、パイロツトエアスクリユ13
を経て低速燃料通路10内へ流入する空気流が減
少する。よつてエアブリード、即ち、低速燃料噴
口6からの燃料に混入される空気が減少すること
から、吸気通路2内へ噴出する燃料が増す。よつ
て空気通路14を経て大気が導入されたとして
も、供給される混合気の空燃比は濃厚となるもの
で、吸気量の増量に伴つて自動的に濃厚化が行わ
れる。更に、始動弁15の開度が大きい極低温始
動時、たとえば氷点下の始動では始動用空気通路
14内に波及する負圧が大きいので、その作用を
受けて燃料弁28も開かれる。そこで、エマルジ
ヨン管29および計量管31内に溜つている燃料
はジエツト32を通して作用する大気圧の作用で
噴口26を通して吸気通路2内へ短時間のうちに
噴出し、始動時に吸入される混合気をエンリツチ
してエンジンの始動性を一層向上させる。
Now, when the temperature of the engine or the outside air falls below a predetermined temperature, the bimetal 22 bends upward in the figure, pulls up the valve body 17, and completely passes through the starting air passage 14. When cranking in this condition, air passage 1
Intake negative pressure downstream of the throttle valve 3 acts on the slow air passage 11 through the pilot air screw 13.
The airflow flowing into the low speed fuel passage 10 through the lower speed fuel passage 10 is reduced. Therefore, air bleed, that is, air mixed into the fuel from the low-velocity fuel nozzle 6 is reduced, so that the amount of fuel injected into the intake passage 2 is increased. Therefore, even if the atmosphere is introduced through the air passage 14, the air-fuel ratio of the supplied air-fuel mixture will be rich, and the air-fuel ratio will be enriched automatically as the amount of intake air increases. Furthermore, when starting at a cryogenic temperature where the opening degree of the starting valve 15 is large, for example when starting at sub-zero temperatures, the negative pressure that spreads within the starting air passage 14 is large, so the fuel valve 28 is also opened under the influence of the negative pressure. Therefore, the fuel accumulated in the emulsion pipe 29 and the metering pipe 31 is injected into the intake passage 2 through the jet nozzle 26 in a short time due to the atmospheric pressure acting through the jet 32, and the air-fuel mixture taken in at the time of startup is Enriches to further improve engine startability.

こゝでエンジンが始動し、クランキングからエ
ンジンが自力で運転を連続できるいわゆる完爆に
至るとエンジン速度が急上昇して絞り弁下流の吸
気負圧が急上昇する。
At this point, the engine starts, and when it reaches so-called complete combustion, where the engine can continue to operate on its own from cranking, the engine speed increases rapidly and the intake negative pressure downstream of the throttle valve increases rapidly.

始動弁15の弁体17はばね24に抗して下方
へ移動し、その開度を減じるので(図面はこの状
態を示す)、それより上流側の空気通路14内は
逆に負圧が減じて負圧作動式の燃料弁28が閉弁
すると共に、低速燃料噴口6から供給される燃料
が減量する。なお、外気温が非常に低いため空気
通路14内の負圧の減少(大気圧に近づく)が充
分でないとき、負圧応動弁28は開弁状態に保た
れるが、通路27中に存した燃料が消費される短
時間後には、ジエツト32を通して流入する空気
と小孔33を通して通路27内へ流入する小量の
燃料とのエマルジヨンがジエツト32で計量され
て吸気通路2内へ供給される。
Since the valve element 17 of the starter valve 15 moves downward against the spring 24 and reduces its opening degree (the figure shows this state), the negative pressure in the air passage 14 on the upstream side decreases. As a result, the negative pressure operated fuel valve 28 closes, and the amount of fuel supplied from the low speed fuel nozzle 6 decreases. Note that when the outside temperature is so low that the negative pressure inside the air passage 14 is not sufficiently reduced (approaching atmospheric pressure), the negative pressure responsive valve 28 is kept open, but the negative pressure inside the air passage 27 remains open. After a short time after the fuel has been consumed, an emulsion of air flowing through the jet 32 and a small amount of fuel flowing into the passage 27 through the small hole 33 is metered by the jet 32 into the intake passage 2.

エンジンが暖機運転されて温度が上昇してくる
と、始動弁15の開度が自動的に減少し、遂には
閉弁に至るが、この間低速燃料噴口6から供給さ
れる燃料は徐々に減少してエンジンの低速運転用
の所要の低流量に低下する。
When the engine is warmed up and the temperature rises, the opening degree of the starter valve 15 automatically decreases and finally closes, but during this time the fuel supplied from the low-speed fuel injection port 6 gradually decreases. This reduces the flow rate to the required low flow rate for low speed operation of the engine.

この発明は以上のようにスローエア通路を絞り
弁下流の吸気通路へ連通する空気通路を設け、そ
の途中に、そこへ作用する吸気負圧が上昇したと
き通気面積を減じる感圧弁を設けると共に、絞り
弁下流の吸気通路へ燃料を供給する通路を設け、
そこへ前記空気通路内の負圧が上昇したとき閉じ
る負圧作動式の燃料弁を設けたものである。よつ
て両者が共働してエンジンがクランキングされる
間、低速燃料噴口と始動燃料噴口とから吸気通路
内へ燃料が供給されて、吸入混合気の空燃比が一
層濃厚となり、極低温時の始動を容易にする。エ
ンジンが自力運転可能な出力を生じると感圧弁に
より低速燃料噴口から供給される燃料が減じると
共に燃料弁により始動燃料の供給を停止する。従
つて始動と同時に空燃比が希薄化され、引続く運
転に際して、空燃比過濃による運転の不安定や燃
料の浪費を防止する効果を有する。
As described above, this invention provides an air passage that communicates the slow air passage with the intake passage downstream of the throttle valve, and a pressure-sensitive valve that reduces the ventilation area when the intake negative pressure acting thereon rises in the middle. A passage is provided to supply fuel to the intake passage downstream of the valve,
There is provided a negative pressure operated fuel valve that closes when the negative pressure in the air passage increases. Therefore, while the two work together to crank the engine, fuel is supplied from the low-speed fuel nozzle and the starting fuel nozzle into the intake passage, making the air-fuel ratio of the intake mixture even richer, which increases the Makes starting easier. When the engine produces an output that allows it to run on its own, the pressure-sensitive valve reduces the amount of fuel supplied from the low-speed fuel nozzle, and the fuel valve stops the supply of starting fuel. Therefore, the air-fuel ratio is diluted at the same time as the engine starts, which has the effect of preventing unstable operation and waste of fuel due to an excessively rich air-fuel ratio during subsequent operation.

なお、始動燃料噴口は吸気通路内に直接開口す
るものに限らず、空気通路内に設けてもよい。
Note that the starting fuel nozzle is not limited to one that opens directly into the intake passage, but may be provided within the air passage.

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

図面は本発明実施の一例を示す気化器の構成図
である。 2……吸気通路、3……絞り弁、6……低速燃
料噴口、14……始動用空気通路、15……始動
弁、26……始動燃料噴口、28………負圧作動
弁。
The drawing is a configuration diagram of a vaporizer showing an example of carrying out the present invention. 2...Intake passage, 3...Throttle valve, 6...Low speed fuel nozzle, 14...Starting air passage, 15...Starting valve, 26...Starting fuel injection port, 28...Negative pressure operating valve.

Claims (1)

【特許請求の範囲】[Claims] 1 絞り弁下流の吸気通路に低速燃料通路を開口
させ、この低速燃料通路にスローエア通路を介し
て大気を導入するようにした気化器において、前
記スローエア通路と絞り弁下流の吸気通路とを始
動用空気通路で接続し、この始動用空気通路に、
この通路に作用する吸気負圧が上昇したとき通気
面積を減じかつ低温時に通気面積を開く方向へ付
勢する感温部材を備えた始動弁を設けると共に、
この始動弁下流の空気通路または絞り弁下流の吸
気通路に燃料噴口を開口させ、この燃料噴口に接
続された燃料通路に、前記始動弁とスローエア通
路間の負圧に応動する負圧作動式の燃料弁を設け
てなる気化器の始動装置。
1. In a carburetor in which a low-speed fuel passage is opened in the intake passage downstream of the throttle valve and atmospheric air is introduced into the low-speed fuel passage through the slow air passage, the slow air passage and the intake passage downstream of the throttle valve are used for starting. Connected with an air passage, and connected to this starting air passage,
Providing a starter valve equipped with a temperature-sensitive member that reduces the ventilation area when the intake negative pressure acting on this passage increases and biases the ventilation area in the direction of opening it at low temperatures,
A fuel nozzle is opened in the air passage downstream of the starting valve or the intake passage downstream of the throttle valve, and a negative pressure-operated type that responds to the negative pressure between the starting valve and the slow air passage is connected to the fuel passage connected to the fuel nozzle. A carburetor starting device equipped with a fuel valve.
JP6257480A 1980-05-12 1980-05-12 Starting device for carburettor Granted JPS56159541A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP6257480A JPS56159541A (en) 1980-05-12 1980-05-12 Starting device for carburettor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP6257480A JPS56159541A (en) 1980-05-12 1980-05-12 Starting device for carburettor

Publications (2)

Publication Number Publication Date
JPS56159541A JPS56159541A (en) 1981-12-08
JPS6147299B2 true JPS6147299B2 (en) 1986-10-18

Family

ID=13204202

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6257480A Granted JPS56159541A (en) 1980-05-12 1980-05-12 Starting device for carburettor

Country Status (1)

Country Link
JP (1) JPS56159541A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0137438Y2 (en) * 1987-06-09 1989-11-10
JPH0424463U (en) * 1990-06-22 1992-02-27

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0137438Y2 (en) * 1987-06-09 1989-11-10
JPH0424463U (en) * 1990-06-22 1992-02-27

Also Published As

Publication number Publication date
JPS56159541A (en) 1981-12-08

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