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JPS6132118Y2 - - Google Patents

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Publication number
JPS6132118Y2
JPS6132118Y2 JP1981126789U JP12678981U JPS6132118Y2 JP S6132118 Y2 JPS6132118 Y2 JP S6132118Y2 JP 1981126789 U JP1981126789 U JP 1981126789U JP 12678981 U JP12678981 U JP 12678981U JP S6132118 Y2 JPS6132118 Y2 JP S6132118Y2
Authority
JP
Japan
Prior art keywords
valve
atmosphere
fuel
engine
pressure
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
JP1981126789U
Other languages
Japanese (ja)
Other versions
JPS5832155U (en
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 filed Critical
Priority to JP12678981U priority Critical patent/JPS5832155U/en
Publication of JPS5832155U publication Critical patent/JPS5832155U/en
Application granted granted Critical
Publication of JPS6132118Y2 publication Critical patent/JPS6132118Y2/ja
Granted legal-status Critical Current

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  • Supercharger (AREA)
  • Means For Warming Up And Starting Carburetors (AREA)

Description

【考案の詳細な説明】 本考案は、2サイクル機関、特に、クランクケ
ース内に発生する脈動圧力にて燃料ポンプを駆動
し、このポンプより吐出される燃料を気化器の浮
子室内に供給するようにした形式の機関に装備さ
れる気化器始動装置に関するもので、クランクケ
ース内から気化器浮子室内内の上部空間に伝達さ
れる正圧を制御して、機関の低温状態からの始動
運転を、そのクランキング時から瞬機運転完了時
に至るまで終始スムーズに且つ自動的に行わせる
ことができ、しかも燃料ポンプの吐出燃料圧を利
用して前記正圧の大きさを精度よく完爆補正でき
るようににした構造簡単な前記始動装置を提供す
ることを目的とする。
[Detailed description of the invention] This invention is a two-cycle engine, in particular, a fuel pump is driven by the pulsating pressure generated in the crankcase, and the fuel discharged from the pump is supplied into the float chamber of the carburetor. This device is related to a carburetor starting device installed in a type of engine that controls the positive pressure transmitted from the inside of the crankcase to the upper space in the carburetor float chamber to start the engine from a low temperature state. The process can be performed smoothly and automatically from beginning to end from the time of cranking to the end of instantaneous operation, and the magnitude of the positive pressure can be accurately corrected for complete explosion using the discharge fuel pressure of the fuel pump. An object of the present invention is to provide a starting device having a simple structure.

そしてかかる目的を達成するために本考案は、
前記形式の2サイクル機関において、浮子室内の
上部空間とクランクケース内とを、該クランクケ
ース内に発生する脈動圧力のうち正圧のみを浮子
室側へ伝達する正圧取り出し装置を介して接続
し、前記浮子室内の上部空間と大気とを第1及び
第2大気導入路を介して各独立して連通させ、そ
の第1大気導入路には、ジエツトと、該第1大気
導入路を開閉し得る常閉型の開閉弁とを直列に介
装し、その開閉弁と前記燃料ポンプとの間に、機
関完爆時には該弁を開弁させるように該ポンプの
吐出燃料圧を該弁に作用させる燃料圧伝達装置を
設け、さらに前記第2大気導入路には、該第2大
気導入路を機関雰囲気温度が所定値以下では閉じ
所定値を超えると開く温度感知弁を設けたことを
特徴とする。
In order to achieve this purpose, the present invention
In the two-cycle engine of the above type, the upper space in the float chamber and the inside of the crankcase are connected via a positive pressure extraction device that transmits only positive pressure of the pulsating pressure generated in the crankcase to the float chamber side. , the upper space in the float chamber and the atmosphere are communicated independently through first and second atmosphere introduction passages, and the first atmosphere introduction passage includes a jet and a valve that opens and closes the first atmosphere introduction passage. A normally closed on-off valve is interposed in series between the on-off valve and the fuel pump, and the discharge fuel pressure of the pump is applied to the valve so as to open the valve at the time of a complete engine explosion. A fuel pressure transmission device is provided in the second atmosphere introduction passage, and the second atmosphere introduction passage is further provided with a temperature sensing valve that closes the second atmosphere introduction passage when the engine atmosphere temperature is below a predetermined value and opens when the engine atmosphere temperature exceeds a predetermined value. do.

以下、図面により本考案の一実施例について説
明すると、2サイクル機関1の吸気孔には気化器
2の吸気道3の下流端が接続されている。その気
化器2は、内部を吸気道3が貫通した気化器本体
4と、その下部に配置した浮子室5とよりなり、
吸気道3には、吸気道3を流れる空気量を制御す
る絞り弁6が配置されるとともに、吸気道3のベ
ンチユリ部7には主ジエツト8に連なる主ノズル
9が開口する。浮子室5内には浮子10が軸11
にて回動自在に軸支され浮子10の端部の浮子ア
ーム12は燃料流入路13内の弁在14に対向配
置した浮子弁15に対応配置される。燃料流入路
13には機関1のクランクケース1a内の脈動圧
力にて駆動される燃料ポンプ17より燃料が供給
されるものであり、この燃料は弁座14を介して
浮子室5内へ供給され、浮子10、浮子弁15及
び弁座14の協働によつて浮子室5には一定液面
X−Xが形成保持されるようになつている。燃料
ポンプ17はダイヤフラム18にて圧力室17A
とポンプ室17Bとに区分され、圧力室17Aは
脈動圧力19を介して機関のクランクケース1a
内に連絡され、ポンプ室17Bは吸入側逆止弁2
0を介して燃料タンク21に連絡されるとともに
吐出側逆止弁22を介して燃料流入路13に連絡
される。以上の構造は従来一般的に使用される構
造である。
An embodiment of the present invention will be described below with reference to the drawings. An intake hole of a two-stroke engine 1 is connected to the downstream end of an intake path 3 of a carburetor 2. The carburetor 2 consists of a carburetor body 4 through which an intake passage 3 passes, and a float chamber 5 disposed at the bottom of the carburetor body 4.
A throttle valve 6 for controlling the amount of air flowing through the intake passage 3 is disposed in the intake passage 3, and a main nozzle 9 connected to a main jet 8 opens in a bench lily portion 7 of the intake passage 3. Inside the float chamber 5, a float 10 is attached to a shaft 11.
A float arm 12 at the end of the float 10 is rotatably supported by a rotatable shaft and is disposed corresponding to a float valve 15 disposed opposite to a valve seat 14 in the fuel inlet passage 13 . Fuel is supplied to the fuel inlet passage 13 from a fuel pump 17 driven by pulsating pressure within the crankcase 1a of the engine 1, and this fuel is supplied into the float chamber 5 via the valve seat 14. , the float 10, the float valve 15, and the valve seat 14 cooperate to form and maintain a constant liquid level XX in the float chamber 5. The fuel pump 17 has a pressure chamber 17A with a diaphragm 18.
The pressure chamber 17A is divided into a pump chamber 17B and a pump chamber 17B.
The pump chamber 17B is connected to the suction side check valve 2.
0 to the fuel tank 21 and to the fuel inlet passage 13 via the discharge side check valve 22. The above structure is a structure commonly used in the past.

前記クランクケース内1a内と浮子室5内の上
部空間5Aとの間は、前記脈動圧力19より分岐
した連通路23を介して相互に連通されており、
その連通路23の途中には、クランクケース内1
a内の脈動圧力のうち正圧のみ浮子室5内の上部
空間5Aに伝達する正圧取り出し装置としての逆
止弁24が介装され、この弁24は、前記連通路
23の一部をなす弁通路を内部に形成したケーシ
ング25と、そのケーシング25に設けた弁座2
6に接離して該弁通路を開閉し得る弁体27と、
それを閉じ方向に弾発する弁ばね28とより構成
されている。
The inside of the crankcase 1a and the upper space 5A in the float chamber 5 are communicated with each other via a communication path 23 branched from the pulsating pressure 19,
In the middle of the communication path 23, there is a
A check valve 24 is interposed as a positive pressure take-off device that transmits only the positive pressure of the pulsating pressure in the float chamber 5 to the upper space 5A in the float chamber 5, and this valve 24 forms a part of the communication path 23. A casing 25 in which a valve passage is formed, and a valve seat 2 provided in the casing 25.
a valve body 27 that can come into contact with and separate from 6 to open and close the valve passage;
It is comprised of a valve spring 28 that springs it in the closing direction.

前記浮子室5内の上部室間5Aは、互いに独立
した第1及び第2大気気導入路29,38を介し
て大気にそれぞれ連通されており、第1大気導入
路29には、ケーシング31にそれぞれ設けられ
たジエツト47及び開閉弁50が直列に介装され
る。開閉弁50は、ケーシング31に形成されて
第1大気導入路29の一部をなす弁孔48と、こ
の弁孔48を開閉し得る弁体33と、この弁体3
3を弁杆49を介して閉じ方向へ付勢する弁ばね
37とにより常閉型に構成され、その弁体33
は、以下に述べる燃料圧伝達装置30を介して前
記燃料ポンプ17に接続されている。即ちその装
置30は、前記燃料流入路13より分岐した燃料
圧力導入路51と、前記弁杆49に連結され且つ
ケーシング31に張設されたダイヤフラム36
と、このダイヤフラム36の一側に画成される大
気室35と、同ダイヤフラム36の他側に画成さ
れ且つ該燃料圧力導入路51にのみ連通する受圧
室34とより構成されており、従つてその受圧室
34に燃料圧力導入路51を通して燃料ポンプ1
7の所定値以上の吐出燃料圧が作用したときに
は、その燃料圧がダイヤフラム36を介して弁体
33を開き方向に移動させ得るようになつてい
る。
The upper chamber 5A in the float chamber 5 is communicated with the atmosphere through first and second atmospheric air introduction passages 29 and 38, which are independent of each other. A jet 47 and an on-off valve 50 are provided in series. The on-off valve 50 includes a valve hole 48 formed in the casing 31 and forming a part of the first atmosphere introduction path 29, a valve body 33 that can open and close this valve hole 48, and this valve body 3.
3 in the closing direction via a valve rod 49, the valve body 33 is normally closed.
is connected to the fuel pump 17 via a fuel pressure transmission device 30, which will be described below. That is, the device 30 includes a fuel pressure introduction path 51 branched from the fuel inflow path 13 and a diaphragm 36 connected to the valve rod 49 and stretched over the casing 31.
It is composed of an atmospheric chamber 35 defined on one side of the diaphragm 36, and a pressure receiving chamber 34 defined on the other side of the diaphragm 36 and communicating only with the fuel pressure introduction path 51. The fuel pump 1 is then passed through the fuel pressure introduction passage 51 into the pressure receiving chamber 34.
When a discharge fuel pressure equal to or higher than a predetermined value of 7 is applied, the fuel pressure can move the valve body 33 in the opening direction via the diaphragm 36.

また前記第2大気導入路38には、該路38を
機関雰囲気温度が所定値(例えば20℃)以下では
閉じ所定値を超えると開く温度感知弁39が介装
される。この温度感知弁39は弁本体40の弁座
41に対向して弁体42を備えるもので、この弁
体42は、密閉された膨縮室43内に一端が開口
した操作杆44に連結される。尚45は膨縮室4
3内に封入されたエーテル、パラフイン等の熱膨
脹材であり、46は弁体42を弁座41に対接す
るよう操作杆44を図において左方向へ押圧する
スプリングであり、機関雰囲気温度が一定温度を
超える場合においては、膨縮室43内の熱膨脹材
45が膨脹することによつて操作杆44がスプリ
ング46の押圧力に抗して図において右動し、弁
体42を弁座41より離反させて浮子室5内の上
部空間5Aに大気を導入するものであり、一方機
関雰囲気温度が一定温度以下においては熱膨脹材
45が収縮することによつて操作杆44はスプリ
ング46にて押圧されて左動し、弁体42は弁座
41に当接して第2大気導入路38から上記空間
5Aへの大気の導入を遮断するものである。
Further, a temperature sensing valve 39 is installed in the second atmospheric air introduction passage 38, which closes the passage 38 when the engine ambient temperature is below a predetermined value (for example, 20° C.) and opens when it exceeds a predetermined value. This temperature sensing valve 39 includes a valve body 42 facing a valve seat 41 of a valve body 40, and this valve body 42 is connected to an operating rod 44 having one end opened in a sealed expansion/contraction chamber 43. Ru. In addition, 45 is the expansion chamber 4
3 is a heat-expandable material such as ether or paraffin sealed in the chamber, and 46 is a spring that presses the operating rod 44 to the left in the figure so as to bring the valve body 42 into contact with the valve seat 41. In the case where the thermal expansion material 45 in the expansion/contraction chamber 43 expands, the operating rod 44 moves to the right in the figure against the pressing force of the spring 46, and the valve body 42 is separated from the valve seat 41. Atmospheric air is introduced into the upper space 5A in the float chamber 5. On the other hand, when the engine atmosphere temperature is below a certain temperature, the operating rod 44 is pressed by the spring 46 as the thermal expansion material 45 contracts. The valve body 42 moves to the left and comes into contact with the valve seat 41 to block the introduction of the atmosphere from the second atmosphere introduction path 38 into the space 5A.

次に前記実施例の作用を説明する。先ず機関雰
囲気温度が一定温度(例えば20℃)を超えている
状態における始動時について説明すると、機関の
クランキング操作によつてクランクケース1a内
の発生する脈動圧力は連通路23から正圧取り出
し装置24の弁体27へ作用するので、スプリン
グ28を適当に選定することによつて弁体27は
正圧により弁座26より離間して連通路23の下
流側へ正圧のみを取出し、浮子室5内の上部空間
5Aへ正圧を導入する。一方、この際、第2大気
導入路38に配置した温度感知弁39の熱膨脹材
45は膨脹してその体積を増加するので、操作杆
44、弁体42はスプリング46のばね力に抗し
て図において右動し、弁座41を開放して第2大
気導入路38より上部空間5Aに大気を導入する
ものである。
Next, the operation of the above embodiment will be explained. First of all, when starting when the engine ambient temperature exceeds a certain temperature (for example, 20°C), the pulsating pressure generated in the crankcase 1a due to engine cranking is transferred to the positive pressure extraction device from the communication passage 23. 24, so by appropriately selecting the spring 28, the valve body 27 is separated from the valve seat 26 by positive pressure, and only positive pressure is taken out to the downstream side of the communication passage 23, and the float chamber Positive pressure is introduced into the upper space 5A in the 5. On the other hand, at this time, the thermal expansion material 45 of the temperature sensing valve 39 disposed in the second atmosphere introduction path 38 expands and increases its volume, so that the operating rod 44 and the valve body 42 resist the spring force of the spring 46. It moves to the right in the figure, opens the valve seat 41, and introduces the atmosphere into the upper space 5A from the second atmosphere introduction path 38.

従つて、かかる温度状態においては、浮子室5
内の上部空間5A内に連通路23から正圧が導入
されるが、その正圧は第2大気導入路38より大
気へ開放されるので、該上部空間5A内は大気圧
に保持されるものであつて、始動に際して比較的
薄目の始動用混合気が機関へ供給されるので、機
関雰囲気温度の高い状態における始動時、あるい
は熱間再始動時の運転をスムーズに行わせること
ができる。
Therefore, in such a temperature state, the float chamber 5
Positive pressure is introduced from the communication passage 23 into the upper space 5A, but since the positive pressure is released to the atmosphere from the second atmosphere introduction passage 38, the inside of the upper space 5A is maintained at atmospheric pressure. Since a relatively thin starting air-fuel mixture is supplied to the engine at the time of starting, smooth operation can be achieved at the time of starting in a state where the engine ambient temperature is high or at the time of hot restart.

次に、機関雰囲気温度が一定温度(例えば20
℃)以下における始動時について説明する。
Next, the engine ambient temperature is set to a constant temperature (e.g. 20
℃) and below will be explained.

第2大気導入路38内の温度感知弁39は、膨
縮室43内の熱膨脹材45が機関雰囲気温度によ
つて収縮して体積を減少させるので、操作杆44
はスプリング46のばね力によつて図において左
動し、これによつて弁体42は弁座41を閉じて
2大気導入路38を閉塞し、浮子室5内の上部空
間5Aを大気と遮断する。
The temperature sensing valve 39 in the second atmosphere introduction path 38 is operated by the operating rod 44 because the thermal expansion material 45 in the expansion/contraction chamber 43 contracts and reduces its volume due to the engine ambient temperature.
is moved to the left in the figure by the spring force of the spring 46, thereby causing the valve body 42 to close the valve seat 41 and block the second atmosphere introduction path 38, thereby cutting off the upper space 5A in the float chamber 5 from the atmosphere. do.

一方、燃料ポンプ17は不作動であるから、燃
料圧伝達装置30の受圧室34内には何等の燃料
圧力も作用せず、ダイヤフラム36は弁ばね37
にて右方へ押圧され、弁体33は弁座32に当接
して第1大気導入路29を閉塞し、浮子室5内の
上部空間5Aを大気と遮断する。
On the other hand, since the fuel pump 17 is inactive, no fuel pressure acts within the pressure receiving chamber 34 of the fuel pressure transmission device 30, and the diaphragm 36
The valve element 33 contacts the valve seat 32 and closes the first atmosphere introduction passage 29, thereby cutting off the upper space 5A in the float chamber 5 from the atmosphere.

かかる状態において機関のクランキング操作を
行うと、クランクケース1a内に発生する脈動圧
力は正圧取り出し装置24の弁体27へ作用する
ものであり、前述した通り該脈動圧力のうちの正
圧のみが連通路23を介して浮子室5内の上部空
間5A内に伝達される。かかる正圧が上部空間5
A内に伝達されるや、該上部空間5A内に即座に
大気圧より正圧に変換するので、(このとき第
1,第2大気導入路29,38は遮断されてい
る。)、主ノズル9等の燃料噴口に作用する圧力差
は大となり、これら燃料噴口より多量の燃料を吸
気道3内へ供給でき、低温始動に適した始動用濃
混合気を機関へ供給することができるもので良好
な機関始動性が得られる。
When the engine is cranked in such a state, the pulsating pressure generated in the crankcase 1a acts on the valve body 27 of the positive pressure take-off device 24, and as described above, only the positive pressure of the pulsating pressure is released. is transmitted into the upper space 5A in the float chamber 5 via the communication path 23. This positive pressure causes the upper space 5
As soon as the pressure is transmitted into the upper space 5A, the atmospheric pressure is immediately converted to positive pressure (at this time, the first and second atmospheric air introduction passages 29 and 38 are blocked), and the main nozzle The pressure difference acting on the fuel nozzles 9, etc. is large, and a large amount of fuel can be supplied into the intake passage 3 from these fuel nozzles, and a rich mixture for starting suitable for low-temperature starting can be supplied to the engine. Good engine startability can be obtained.

次いで、機関が完爆すると、機関の回転数が上
昇して吸気道3内の負圧は上昇するので、クラン
キング時と同様に浮子室5内の上部空間5Aに正
圧を供給し続けると、前述の如く吸気道内負圧の
増加に伴つて過濃なる混合気を機関へ供給し、機
関の可燃限界を超えて機関が停止する場合があ
る。
Next, when the engine completely explodes, the engine speed increases and the negative pressure in the intake passage 3 increases, so if you continue to supply positive pressure to the upper space 5A in the float chamber 5 as during cranking, As described above, as the negative pressure in the intake tract increases, an excessively rich air-fuel mixture is supplied to the engine, which may exceed the flammability limit of the engine and cause the engine to stop.

然しながら本考案においては、機関が完爆して
機関回転数が上昇するや、この回転の上昇に伴つ
て燃料ポンプ17のダイヤフラム18の振動数が
増加して燃料吐出圧力が上昇する点に着目し、こ
の燃料吐出圧力を燃料圧伝動装置30の受圧室3
4内へ導入するようにしたものである。即ち機関
が完爆するや、急激に増加された燃料吐出圧力が
受圧室34内へ導入されるので、ダイヤフラム3
6はこの増加された圧力にて図において左動し、
弁ばね37の閉弁力に抗して弁体33を弁座32
より難間させて浮子室5内の上部空間5Aと大気
とをこの第1大気導入路29を介して連絡するも
のである。
However, the present invention focuses on the point that when the engine completely explodes and the engine speed increases, the frequency of the diaphragm 18 of the fuel pump 17 increases and the fuel discharge pressure increases as the engine speed increases. , this fuel discharge pressure is transferred to the pressure receiving chamber 3 of the fuel pressure transmission device 30.
It was designed to be introduced into 4. That is, when the engine completely explodes, the rapidly increased fuel discharge pressure is introduced into the pressure receiving chamber 34, so that the diaphragm 3
6 moves to the left in the figure with this increased pressure,
The valve body 33 is moved against the valve seat 32 against the valve closing force of the valve spring 37.
The upper space 5A in the float chamber 5 and the atmosphere are communicated through the first atmosphere introduction path 29 with more difficulty.

これによるとその上部空間5A内の正圧は第1
大気導入路29よりジエツト47を介して徐々に
大気へ開放されて、正圧の圧力値を徐々に大気圧
側へ近づけることができるので、機関へ供給する
混合気濃度を希薄化傾向に補正することができて
機関完爆運転性を良好に行ない得るものである。
尚、正圧の大気への開放量制御は前記ジエツト4
7の有効径を適当に選定することによつて行ない
得るものである。
According to this, the positive pressure in the upper space 5A is the first
It is gradually released to the atmosphere from the atmosphere introduction passage 29 via the jet 47, and the pressure value of the positive pressure can be gradually brought closer to the atmospheric pressure side, so that the mixture concentration supplied to the engine is corrected to tend to be diluted. This makes it possible to achieve good engine complete explosion operability.
The amount of positive pressure released to the atmosphere is controlled by the jet 4.
This can be achieved by appropriately selecting the effective diameter of 7.

次いで、機関の瞬機運転が進み機関雰囲気温度
が一定温度を超えて上昇するや、膨縮室43内の
熱膨脹材45は膨脹してその体積を増加するの
で、操作杆44はスプリング46のばね力に抗し
て図において右動し、弁体42が弁座41を開放
して第2大気導入路38にて浮子室5内の上部空
間5Aと大気とを連通して該空間5Aを大気圧に
復帰させ、以後大気圧状態を保持するものであ
る。従つて、混合気をさらに希薄化傾向に制御す
ることができ、機関の運転を安定させることがで
きる。
Next, as the instantaneous operation of the engine progresses and the engine ambient temperature rises above a certain temperature, the thermal expansion material 45 in the expansion and contraction chamber 43 expands and increases its volume, so that the operating rod 44 is moved by the spring 46. The valve body 42 moves to the right in the figure against the force, opens the valve seat 41, communicates the upper space 5A in the float chamber 5 with the atmosphere through the second atmosphere introduction passage 38, and enlarges the space 5A. The pressure is returned to atmospheric pressure and the atmospheric pressure is maintained thereafter. Therefore, the air-fuel mixture can be controlled to tend to be more diluted, and the operation of the engine can be stabilized.

以上のように本考案によれば、クランクケース
内に発生する脈動圧力にて燃料ポンプを駆動し、
このポンプより吐出される燃料を気化器の浮子室
内に供給するようにした2サイクル機関におい
て、前記浮子室内の上部空間とクランクケース内
とを、該クランクケース内に発生する脈動圧力の
うち正圧のみを浮子室側へ伝達する正圧取り出し
装置を介して接続し、前記浮子室内の上部空間と
大気とを第1及び第2大気導入路を介して各独立
して連通させ、その第1大気導入路には、ジエツ
トと、該第1大気導入路を開閉し得る常閉型の開
閉弁とを直列に介装し、その開閉弁と前記燃料ポ
ンプとの間に、機関完爆時には該弁を開弁させる
ように該ポンプの吐出燃料圧を該弁に作用させる
燃料圧伝達装置を設け、さらに前記第2大気導入
路には、該第2大気導入路を機関雰囲気温度が所
定値以下では閉じ所定値を超えると開く温度感知
弁を設けたので、機関雰囲気温度が所定値以下に
おける、機関のクランキング時には、クランクケ
ース内の正圧をそのまま浮子室内の上部空間に供
給して、気化器で生成される混合気の濃度を始動
に最適な高い他に制御することができ、次いで機
関が完爆状態になると、急激に増大する燃料ポン
プの吐出燃料圧を利用して前記開閉弁を開弁させ
第1大気導入路のジエツトを通して浮子室内上部
空間を大気に多少開放することにより、該上部空
間に作用する正圧を減少させて、上記混合気濃度
を完爆後の瞬機運転に最適なクランキング時より
も低い値に補正することができ、さらに機関の瞬
機運転が進んで機関雰囲気温度が所定値を超える
と、前記温度感知弁が開弁して第2大気導入路を
通して浮子室内上部空間を大気に大きく開放する
ことにより、該上部空間を大気圧下に置いて上記
混合気濃度を機関の通常運転に最適な、さらに低
い値に制御することができ、従つて機関の低温状
態からの始動運転を、そのクランキング時から瞬
機運転完了時に至るまで終始スムーズにしかも自
動的に行わせることができる。特に、前記正圧に
対する完爆補正手段は、既存の燃料ポンプの吐出
燃料圧を前記開閉弁に単に作用させるだけの構造
簡単なものであるから、コストの低減に寄与する
ことができ、その上その燃料ポンプの吐出燃料圧
は、機関のクランキングから完爆にかけては確実
に上昇変化を示し且つ完爆後の瞬機運転状態では
圧力変動が比較的少ないから、上記完爆補正を精
度よく行うことができると共に、瞬機運転中にお
ける混合気濃度の変動を抑えることができる。
As described above, according to the present invention, the fuel pump is driven by the pulsating pressure generated in the crankcase,
In a two-cycle engine in which the fuel discharged from this pump is supplied into a float chamber of a carburetor, the upper space of the float chamber and the inside of the crankcase are controlled to have a positive pressure out of the pulsating pressure generated within the crankcase. The upper space in the float chamber is connected to the atmosphere through a positive pressure take-out device that transmits only the air to the float chamber side, and the upper space in the float chamber and the atmosphere are independently communicated via first and second atmosphere introduction passages, and the first atmosphere A jet and a normally-closed on-off valve capable of opening and closing the first atmosphere introduction path are interposed in series in the inlet passage, and the valve is inserted between the on-off valve and the fuel pump when the engine is completely detonated. A fuel pressure transmission device is provided for applying the discharge fuel pressure of the pump to the valve so as to open the valve, and the second atmosphere introduction passage is further provided with a fuel pressure transmission device that applies the discharge fuel pressure of the pump to the valve so as to open the valve. A temperature sensing valve that closes and opens when it exceeds a predetermined value is installed, so when the engine is cranking when the engine ambient temperature is below a predetermined value, the positive pressure in the crankcase is directly supplied to the upper space in the float chamber, and the carburetor is activated. The concentration of the air-fuel mixture generated in the engine can be controlled to a high level that is optimal for starting, and then when the engine reaches a complete explosion state, the opening/closing valve is opened using the rapidly increasing discharge fuel pressure of the fuel pump. By opening the upper space of the float chamber to the atmosphere to some extent through the jet of the first atmosphere introduction passage, the positive pressure acting on the upper space is reduced, and the above-mentioned mixture concentration is optimized for instantaneous operation after complete detonation. When the engine's instantaneous operation progresses and the engine atmosphere temperature exceeds a predetermined value, the temperature sensing valve opens and the float passes through the second atmosphere introduction path. By greatly opening the upper space of the interior to the atmosphere, it is possible to place the upper space under atmospheric pressure and control the above-mentioned mixture concentration to a lower value that is optimal for normal operation of the engine, thereby reducing the low temperature of the engine. Starting operation from a state can be smoothly and automatically performed from beginning to end from the time of cranking to the time of completion of instantaneous operation. In particular, the complete explosion correction means for the positive pressure has a simple structure that simply causes the discharge fuel pressure of the existing fuel pump to act on the opening/closing valve, so it can contribute to cost reduction, and also The discharge fuel pressure of the fuel pump reliably shows an upward change from engine cranking to complete explosion, and pressure fluctuations are relatively small in the instantaneous operation state after complete explosion, so the above-mentioned complete explosion correction is performed accurately. At the same time, fluctuations in the mixture concentration during instantaneous engine operation can be suppressed.

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

図面は本考案による2サイクル機関の気化器始
動装置の一実施例を示す要部縦断面図を含む系統
図である。 1a……クランクケース、2……気化器、5…
…浮子室、5A……上部空間、17……燃料ポン
プ、24……正圧取り出し装置としての逆止弁、
29……第1大気導入路、30……燃料圧伝動装
置、38……第2大気導入路、39……温度感知
弁、47……ジエツト、50……開閉弁。
The drawing is a system diagram including a vertical sectional view of essential parts showing an embodiment of the carburetor starting device for a two-cycle engine according to the present invention. 1a... crankcase, 2... carburetor, 5...
...Float chamber, 5A... Upper space, 17... Fuel pump, 24... Check valve as a positive pressure extraction device,
29...First atmosphere introduction path, 30...Fuel pressure transmission device, 38...Second atmosphere introduction path, 39...Temperature sensing valve, 47...Jet, 50...Opening/closing valve.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] クランクケース内に発生する脈動圧力にて燃料
ポンプを駆動し、このポンプより吐出される燃料
を気化器の浮子室内に供給するようにした2サイ
クル機関において、前記浮子室内の上部空関とク
ランクケース内とを、該クランクケース内に発生
する脈動圧力のうち正圧のみを浮子室側へ伝達す
る正圧取り出し装置を介して接続し、前記浮子室
内の上部空間と大気とを第1及び第2大気導入路
を介して各独立して連通させ、その第1大気導入
路には、ジエツトと、該第1大気導入路を開閉し
得る常閉型の開閉弁とを直列に介装し、その開閉
弁と前記燃料ポンプとの間に、機関完爆時には該
弁を開弁させるように該ポンプの吐出燃料圧を該
弁に作用させる燃料圧伝達装置を設け、さらに前
記第2大気導入路には、該第2大気導入路を機関
雰囲気温度が所定値以下では閉じ所定値を超える
と開く温度感知弁を設けたことを特徴とする、2
サイクル機関の気化器始動装置。
In a two-cycle engine in which a fuel pump is driven by pulsating pressure generated in the crankcase, and the fuel discharged from the pump is supplied into a float chamber of a carburetor, an upper air barrier in the float chamber and a crankcase The upper space in the float chamber is connected to the atmosphere through a positive pressure take-out device that transmits only positive pressure of the pulsating pressure generated in the crankcase to the float chamber, and the upper space in the float chamber is connected to the atmosphere in the first and second The first atmosphere introduction passages are connected to each other independently through the atmosphere introduction passages, and the first atmosphere introduction passages are interposed in series with a jet and a normally-closed on-off valve capable of opening and closing the first atmosphere introduction passages. A fuel pressure transmission device is provided between the opening/closing valve and the fuel pump, and the fuel pressure transmission device applies the discharge fuel pressure of the pump to the valve so as to open the valve when the engine completely explodes, and the fuel pressure transmission device is further provided in the second atmospheric air introduction path. 2 is characterized in that the second atmosphere introduction passage is provided with a temperature sensing valve that closes when the engine atmosphere temperature is below a predetermined value and opens when it exceeds a predetermined value.
Carburetor starter for cycle engines.
JP12678981U 1981-08-27 1981-08-27 Two-cycle engine carburetor starter Granted JPS5832155U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12678981U JPS5832155U (en) 1981-08-27 1981-08-27 Two-cycle engine carburetor starter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12678981U JPS5832155U (en) 1981-08-27 1981-08-27 Two-cycle engine carburetor starter

Publications (2)

Publication Number Publication Date
JPS5832155U JPS5832155U (en) 1983-03-02
JPS6132118Y2 true JPS6132118Y2 (en) 1986-09-18

Family

ID=29920563

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12678981U Granted JPS5832155U (en) 1981-08-27 1981-08-27 Two-cycle engine carburetor starter

Country Status (1)

Country Link
JP (1) JPS5832155U (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3445839C2 (en) * 1984-12-15 1997-03-13 Stihl Maschf Andreas Automatic start for an internal combustion engine, in particular the engine of a chain saw

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5032901A (en) * 1973-05-05 1975-03-29
JPS539932A (en) * 1976-07-16 1978-01-28 Fuji Heavy Ind Ltd Carbureter for internal combustion engine

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5032901A (en) * 1973-05-05 1975-03-29
JPS539932A (en) * 1976-07-16 1978-01-28 Fuji Heavy Ind Ltd Carbureter for internal combustion engine

Also Published As

Publication number Publication date
JPS5832155U (en) 1983-03-02

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