JP4320215B2 - Intake device for internal combustion engine - Google Patents

Intake device for internal combustion engine Download PDF

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Publication number
JP4320215B2
JP4320215B2 JP2003168909A JP2003168909A JP4320215B2 JP 4320215 B2 JP4320215 B2 JP 4320215B2 JP 2003168909 A JP2003168909 A JP 2003168909A JP 2003168909 A JP2003168909 A JP 2003168909A JP 4320215 B2 JP4320215 B2 JP 4320215B2
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JP
Japan
Prior art keywords
intake
negative pressure
block
valve
pipe
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 - Fee Related
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JP2003168909A
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Japanese (ja)
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JP2005002944A (en
Inventor
智典 井熊
一和 鬼頭
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.)
Mikuni Corp
Honda Motor Co Ltd
Original Assignee
Mikuni Corp
Honda Motor Co Ltd
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Publication date
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Priority to JP2003168909A priority Critical patent/JP4320215B2/en
Priority to CA2470599A priority patent/CA2470599C/en
Priority to US10/866,165 priority patent/US6997157B2/en
Priority to CNB2004100429954A priority patent/CN1316158C/en
Publication of JP2005002944A publication Critical patent/JP2005002944A/en
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Publication of JP4320215B2 publication Critical patent/JP4320215B2/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M35/00Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
    • F02M35/10Air intakes; Induction systems
    • F02M35/10209Fluid connections to the air intake system; their arrangement of pipes, valves or the like
    • F02M35/10229Fluid connections to the air intake system; their arrangement of pipes, valves or the like the intake system acting as a vacuum or overpressure source for auxiliary devices, e.g. brake systems; Vacuum chambers

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Characterised By The Charging Evacuation (AREA)

Description

【0001】
【発明の属する技術分野】
本発明は、内燃機関用吸気装置に関し、特に1つの気筒に2つの吸気管路を並列接続し、且つ一方の吸気管路に開閉弁を設けたデュアルポート型吸気マニホルドを含む吸気装置に関するものである。
【0002】
【従来の技術】
内燃機関の吸気装置として、1つの気筒に対して2つの吸気管路を並列接続し、負圧応動アクチュエータで開閉駆動されるバタフライ弁により、一方の吸気管路をエンジンの運転状況に応じて開閉するよう構成したものが知られている。
【0003】
このようなデュアルポート型吸気マニホルドを備えた吸気装置にあっては、バタフライ弁を開閉駆動する負圧応動アクチュエータに負圧を安定供給するために、負圧を蓄えるための蓄圧タンクが必要である(実公平3−41056号公報を参照されたい)。
【0004】
【特許文献1】
実公平3−41056号公報
【0005】
【発明が解決しようとする課題】
しかるに、上記公報に開示された吸気装置の構造によると、蓄圧タンクを設けたために吸気マニホルドが大型化している上、負圧応動アクチュエータに負圧を供給する配管を簡略化することもできないものであった。
【0006】
【課題を解決するための手段】
このような目的を果たすために、本発明による請求項1においては、吸気管路長が互いに異なる2つの管路(短管路27・長管路28)を並列に有し複数の気筒の各燃焼室に連結された複数の独立吸気管(25)と当該独立吸気管のそれぞれに連通する共通のサージタンク(24)とを備えた吸気マニホルド体(26)と、前記2つの管路の一方を開閉する弁(29)と、前記弁を開閉駆動する負圧応動アクチュエータ(42)と、前記負圧応動アクチュエータに供給する作動圧を蓄える蓄圧タンク(46)とを有する内燃機関用吸気装置であって、前記吸気マニホルド体は、スロットルボディの連結部と前記サージタンクのエンジン側の壁とを一体形成された内側ブロック(31)と、前記サージタンクの反エンジン側の壁と前記独立吸気管の外側の半分を一体形成された外側ブロック(32)と、前記独立吸気管の対シリンダヘッド結合端と前記独立吸気管の内側の半分を一体形成された中間ブロック(35)とにより3分割構成されており、前記内側ブロックと前記中間ブロックとによって前記蓄圧タンクが形成され、前記中間ブロックに吸気管負圧を前記蓄圧タンクに導く孔(47)が形成されている共に前記孔を逆止する負圧チェック弁(48)が取り付けられていることを特徴とするものである。
【0007】
【課題を解決するための手段】
このような目的を果たすために、本発明においては、複数の気筒の各燃焼室(19)に個々に連結され且つシリンダブロック(13)の側方にシリンダ列方向に並設された複数の吸気管(独立吸気管部25)と、該吸気管のそれぞれに設けられ且つ共通のサージタンク(24)内に開口する2つの管路(短管路27・長管路28)と、該2つの管路の一方を開閉する弁(バタフライ弁29)と、該弁を駆動する負圧応動アクチュエータ(ダイヤフラムアクチュエータ42)と、該負圧応動アクチュエータの作動圧を蓄える蓄圧タンク(負圧チャンバ46)とを有する内燃機関用吸気装置(20)を、シリンダブロック側に曲率中心をおいて前記吸気管を湾曲させ、その内周側に前記弁で開閉する一方の管路(短管路27)を配置すると共に、該管路の内周側における前記弁の吸気下流側にて該弁に隣接する位置に前記蓄圧タンクを配置したことを特徴とするものとした。
【0008】
このようにすれば、シリンダブロックの側方に延在させるために湾曲させた吸気管の内周側の通常はデッドスペースとなる部分に蓄圧タンクを設けることができるため、吸気マニホルド体のコンパクト化を損なわずに済む。これに加えて、蓄圧タンクを弁に隣接配置することでアクチュエータをも隣接配置し得るので、負圧供給配管を短縮化することができる。
【0009】
【発明の実施の形態】
以下に添付の図面を参照して本発明について詳細に説明する。
【0010】
図1並びに図2は、本発明に基づいて構成された船外機のエンジン回りを示している。この船外機1は、スターンブラケット2を介して船尾板3に取り付けられる公知形式のものであり、そのエンジン4は、水平方向のチルト軸5回りで回動自在なようにスターンブラケット2に連結されたスイベルケース6と実質的に一体をなすマウントケース7上に搭載されている。そしてマウントケース7上に搭載されたエンジン4の略全体は、着脱自在なエンジンカバー8で覆われている。
【0011】
マウントケース7は、エクステンションケース9の上端に結合され、スクリューに至る駆動軸10とクランク軸11とがその内側で連結されている。
【0012】
エンジン4は、例えば直列4気筒のバーチカルクランク軸エンジンであり、クランクケース12、シリンダブロック13、及びシリンダヘッド14を有しており、航行時にはクランクケース12側が前方を向くように配置されている。またシリンダヘッド14には、吸気ポート15及び排気ポート16との連通が吸気弁17及び排気弁18で断続される燃焼室19が画成されている(図2)。
【0013】
クランクケース12、シリンダブロック13、及びシリンダヘッド14の一側面には、吸気装置20が対向して配設されている。この吸気装置20は、クランクケース12の進行方向についての前面に対向配置された吸気消音チャンバ21及びスロットルボディ22と、スロットルボディ22の出口に接続されたエルボ部23、エルボ部23から連続的に形成されたサージタンク部24、及びサージタンク部24から分岐されて各気筒の吸気ポート15に個々に連結された独立吸気管部25からなる吸気マニホルド体26とからなっている。この吸気装置20は、サージタンク部24がクランクケース12の側面にボルト止めされると共に、独立吸気管部25の下流側端部がシリンダヘッド14の側面にボルト止めされることでエンジン4に結合されている。
【0014】
シリンダブロック13の側方にシリンダ列方向に並設された独立吸気管部25の各独立管路には、吸気上流側に位置するサージタンク部24との接続部において、エンジンに近い側の短管路27と、エンジンから遠い側の長管路28との2つの管路が並列に設けられている。これらの2つの管路27・28は、その下流側で共通管路Cに連結されてシリンダヘッド14との結合端25cへと延出している。また各短管路27には、同時に同一方向に作動するバタフライ弁29が設けられている。
【0015】
吸気マニホルド体26は、その中間部に短管路27と長管路28とを並列に設けた独立吸気管部25と中空のサージタンク部24とを、基本的に2つ割の合わせ金型を用いて成型するために、図3に示したように、3つのブロックで構成されている。即ちこの吸気マニホルド体26は、図4に併せて示すように、対スロットルボディ結合部30及びサージタンク部24のエンジン側の壁24aを形成する内側ブロック31と、エンジン側に曲率中心をおく適宜な曲率で湾曲した吸気流線に沿う面P1で分割される独立吸気管部25の外周側の半部25a及びサージタンク24の反エンジン側の壁24bの一部を形成する外側ブロック32と、独立吸気管部25の内周側の半部25b、独立吸気管部25の対シリンダヘッド結合端25c、バタフライ弁支持部33、短管路27の上流側開口端34、及びサージタンク24の反エンジン側の壁24bに連続するエルボ部23を形成する中間ブロック35とからなっている。なお、内側ブロック31と中間ブロック35とは、サージタンク部24のエンジン側の壁24aに概ね平行な面P2に沿って分割される。
【0016】
これら3つのブロック31・32・35は、それぞれが合成樹脂材の射出成型によって個々に形成された後、例えば振動溶着法によって一体結合されるが、互いの接合面には、図5に示したように、凹部36と凸部37とが形成されており、凸部37が溶融して凹部36に溶着するように、所定の溶融代38が凸部37に設けられている。
【0017】
4つのバタフライ弁29は、図6に示したように、それぞれ個別に形成された軸ホルダ39a〜39cにより、その両端40a・40b並びに中間部40cが支持された共通の軸40上に設けられている。軸40の一端40bは、これに対応する軸ホルダ39bに形成された弾発片41により、がたがなく、且つ円滑に回動可能なように、径方向についての弾発力が加えられている。また外側ブロック32に一体形成された軸ホルダ39aは、軸40の他端40aに微小な隙間を介して対応し、中間部の3つの軸ホルダ39cは、軸40の中間部40cを極く緩く受容している。
【0018】
バタフライ弁29の軸40の他端40a側(クランク軸方向の上側)には、吸気管負圧で駆動される周知構造のダイヤフラムアクチュエータ42が連結されている。このダイヤフラムアクチュエータ42に対する負圧の供給を別途制御信号でオン/オフ駆動される電磁弁43で断続することにより、4つのバタフライ弁29が同時に開閉駆動されるようになっている。
【0019】
ここでダイヤフラムアクチュエータ42の大気室44は中間ブロック35に一体形成されており、部品点数の削減が図られている(図8)。
【0020】
内側ブロック31におけるサージタンク部24と隣接する位置には、図5に示すように、中間ブロック35におけるバタフライ弁29の近傍に形成された凹所45と共働して負圧チャンバ46を画成する膨出部46aが一体形成されている。つまり負圧チャンバ46は、エンジン側に曲率中心をおいて湾曲した独立吸気管部25の内周側に配置された短管路27のさらに内周側におけるバタフライ弁29の吸気下流側、即ちシリンダヘッド寄りにてバタフライ弁29に隣接する位置に配置されている。そして負圧チャンバ46内の気筒列方向中間部には、サージタンク24内にその底部が連通した筒状孔47が形成されており、筒状孔47には、負圧チェック弁48が装着されている。この負圧チェック弁48は、比較的軟質なキノコ形の弁部材49と、弁部材49を所定範囲に渡って軸方向移動自在に支持し、且つ弁部材49が当接する弁座50を備えた弁支持部材51とからなり、Oリングなどのシール部材52を介して弁支持部材51が筒状孔47に嵌着されている。
【0021】
このようにして、負圧チャンバ46の大部分、サージタンク24の大部分、及びこれらの間を連通し且つ負圧チェック弁48を装着する筒状孔47が、吸気マニホルド体26を構成する中間ブロック35に一体成型されている。これにより、負圧チャンバ46に吸気管負圧を導くための連結配管を別途設ける必要を無くしている。
【0022】
この負圧チェック弁48の作用により、吸気管内の負圧が高まると、弁部材49が吸気管側に吸引されて弁座50から離れ、これによって負圧チャンバ46内が負圧になる。吸気管内の負圧が低下すると、弁部材49が弁座50に押し付けられ、負圧チャンバ46内の負圧が高い状態に保たれる。
【0023】
負圧チャンバ46は、間に電磁弁43を介したゴムチューブ53によってダイヤフラムアクチュエータ42の負圧室54に接続されており、電磁弁43のオン/オフ作動により、負圧チャンバ46とダイヤフラムアクチュエータ42の負圧室54との間の連通が断続されるようになっている。この電磁弁43は、図7に示すように、中間ブロック35の側面におけるダイヤフラムアクチュエータ42の大気室44に隣接する位置に一体形成されたステー部55にねじ手段をもって取り付けられており、負圧チャンバ46がバタフライ弁支持部33に隣接配置されていることと相俟って、負圧チャンバ46、電磁弁43、及びダイヤフラムアクチュエータ42の負圧室54間を連結するゴムチューブ53のより一層の短縮化を実現している。
【0024】
上記構成により、ダイヤフラムアクチュエータ42の負圧室54に縮設された圧縮コイルばね56の伸長力でダイヤフラム57が大気室44側に押し出された状態では、バタフライ弁29が開き、バタフライ弁29の直前に位置する開口端34から共通管路Cを経て対シリンダヘッド結合端25cに到る短管路27が、長管路28の吸気上流端部と共に連通する状態(高速・高負荷運転領域)となる。また、ダイヤフラムアクチュエータ42の負圧室54に負圧を導入することによってダイヤフラム57を負圧室54側に引き寄せた状態では、バタフライ弁29が閉じ(図4に2点鎖線で示した状態)、短管路27の開口端34よりも吸気上流側にその開口端28aが位置する長管路28のみが連通する状態(低速・低負荷運転領域)となる。このようにして、エンジン4の運転状態に応じて吸気管路の断面積及び管路長を2段階に切り換えることができるようになっている。
【0025】
長管通路28の最上流部と短管通路27とを隔てる管壁58の下流側端縁と、サージタンク24内における短管通路27の開口端34とは、図4に示したように、同一平面D上に置かれている。この平面Dは、独立吸気管部25の対シリンダヘッド結合端25cの軸線と共に金型のパーティング面に直交しており、これにより、中間ブロック35の型抜きに支障が生じないようにしている。なお、前記した負圧チャンバ46を形成する凹所45の軸線並びに負圧チェック弁48を装着する筒状孔47の軸線も、中間ブロック35の型抜きを考慮して共に金型のパーティング面に直交している。
【0026】
ダイヤフラムアクチュエータ42の大気室44の中心軸Aの向きは、中間ブロック35の型抜き方向、つまり平面Dに平行する方向に対して傾斜しているが(図8参照)、この大気室44は、別のスライド金型61を用いて成型される。なお、大気室44の開口面62を図8における真上に向け、中心軸Aを平面Dに平行させれば、別のスライド金型61を廃止することも可能である。
【0027】
【発明の効果】
以上詳述した通り本発明によれば、複数の気筒の各燃焼室に個々に連結され且つシリンダ列方向に並設された複数の独立吸気管部を、エンジン側に曲率中心をおいて湾曲させ、その内周側にバタフライ弁で開閉する短管路を配置すると共に、該管路の内周側におけるバタフライ弁の吸気下流側、即ちシリンダヘッド寄りにてバタフライ弁に隣接する位置にバタフライ弁を駆動するダイヤフラムアクチュエータへの作動圧を蓄える負圧チャンバを配置するものとしたので、シリンダブロックの側方に延在させるために湾曲させた吸気管の内周側の通常はデッドスペースとなる部分を有効活用することができることから、吸気マニホルド体のコンパクト化をより一層推進する上に多大な効果を奏することができる。特に負圧チャンバをバタフライ弁に隣接配置することにより、ダイヤフラムアクチュエータに負圧チャンバを近接させることができるので、負圧供給配管をより一層短縮化する上にも効果的である。
【図面の簡単な説明】
【図1】本発明が適用された船外機の要部側面図
【図2】本発明が適用された船外機の上面図
【図3】本発明による吸気マニホルド体の分解斜視図
【図4】本発明による吸気マニホルド体の水平断面図
【図5】本発明による吸気マニホルド体の要部水平断面図
【図6】本発明による吸気マニホルド体の要部垂直断面図
【図7】本発明による吸気マニホルド体の要部上面図
【図8】本発明による吸気マニホルド体のダイヤフラムアクチュエータの形成部を一部断面にして示す要部上面図
【符号の説明】
19 燃焼室
20 内燃機関用吸気装置
24 サージタンク
25 独立吸気管部
27 短管路
28 長管路
29 バタフライ弁
42 ダイヤフラムアクチュエータ
46 負圧チャンバ
[0001]
BACKGROUND OF THE INVENTION
The present invention relates to an intake device for an internal combustion engine, and more particularly to an intake device including a dual port type intake manifold in which two intake pipes are connected in parallel to one cylinder and an open / close valve is provided in one intake pipe. is there.
[0002]
[Prior art]
As an intake system for an internal combustion engine, two intake pipes are connected in parallel to one cylinder, and one of the intake pipes is opened and closed according to the operating condition of the engine by a butterfly valve driven to open and close by a negative pressure actuator. What is configured to do is known.
[0003]
In an intake device equipped with such a dual port intake manifold, a pressure accumulation tank for accumulating negative pressure is necessary to stably supply negative pressure to a negative pressure responsive actuator that opens and closes the butterfly valve. (See Japanese Utility Model Publication No. 3-41056).
[0004]
[Patent Document 1]
Japanese Utility Model Publication No. 3-41056
[Problems to be solved by the invention]
However, according to the structure of the intake device disclosed in the above publication, the intake manifold is enlarged because the pressure accumulation tank is provided, and the piping for supplying the negative pressure to the negative pressure actuator cannot be simplified. there were.
[0006]
[Means for Solving the Problems]
In order to achieve such an object, according to a first aspect of the present invention, each of a plurality of cylinders having two pipes (short pipe 27 and long pipe 28) having different intake pipe lengths in parallel are provided. An intake manifold body (26) having a plurality of independent intake pipes (25) connected to the combustion chamber and a common surge tank (24) communicating with each of the independent intake pipes; and one of the two pipe lines An intake device for an internal combustion engine having a valve (29) for opening and closing the valve, a negative pressure responsive actuator (42) for opening and closing the valve, and a pressure accumulating tank (46) for storing operating pressure supplied to the negative pressure responsive actuator there are, the intake manifold body, integrally formed inner block and the engine side of the wall of the surge tank and the connecting portion of the throttle body (31), the independent intake and opposite side to the engine of the wall of the surge tank An outer block (32) formed integrally with the outer half of the independent intake pipe and a cylinder block coupling end of the independent intake pipe and an intermediate block (35) formed integrally with the inner half of the independent intake pipe. The pressure accumulation tank is formed by the inner block and the intermediate block, and a hole (47) for guiding intake pipe negative pressure to the pressure accumulation tank is formed in the intermediate block, and the hole is non-returned. A negative pressure check valve (48) is attached.
[0007]
[Means for Solving the Problems]
In order to achieve such an object, in the present invention, a plurality of intake air units individually connected to the combustion chambers (19) of a plurality of cylinders and arranged side by side in the cylinder row direction on the side of the cylinder block (13). A pipe (independent intake pipe portion 25), two pipe lines (short pipe line 27 and long pipe line 28) provided in each of the intake pipes and opened in a common surge tank (24), A valve that opens and closes one of the pipe lines (butterfly valve 29), a negative pressure responsive actuator (diaphragm actuator 42) that drives the valve, and a pressure accumulation tank (negative pressure chamber 46) that stores the operating pressure of the negative pressure responsive actuator An internal combustion engine intake device (20) having an internal combustion engine having a curvature center on the cylinder block side, the intake pipe being curved, and one pipe line (short pipe line 27) opened and closed by the valve disposed on the inner peripheral side thereof As well as And shall be characterized in that a said accumulator tank to a position adjacent the valve at an intake downstream side of the valve in the inner peripheral side of the pipeline.
[0008]
In this way, since the accumulator tank can be provided in a portion that is normally a dead space on the inner peripheral side of the intake pipe that is curved to extend to the side of the cylinder block, the intake manifold body can be made compact. Without damaging it. In addition to this, since the accumulator tank can be arranged adjacent to the valve, the actuator can be arranged adjacent to the valve, so that the negative pressure supply pipe can be shortened.
[0009]
DETAILED DESCRIPTION OF THE INVENTION
Hereinafter, the present invention will be described in detail with reference to the accompanying drawings.
[0010]
1 and 2 show the engine periphery of an outboard motor constructed according to the present invention. The outboard motor 1 is of a known type that is attached to the stern plate 3 via a stern bracket 2, and the engine 4 is connected to the stern bracket 2 so as to be rotatable around a horizontal tilt shaft 5. It is mounted on a mount case 7 that is substantially integral with the swivel case 6. The substantially entire engine 4 mounted on the mount case 7 is covered with a detachable engine cover 8.
[0011]
The mount case 7 is coupled to the upper end of the extension case 9, and a drive shaft 10 and a crank shaft 11 reaching the screw are connected to each other on the inside.
[0012]
The engine 4 is, for example, an in-line four-cylinder vertical crankshaft engine, and includes a crankcase 12, a cylinder block 13, and a cylinder head 14, and is arranged so that the crankcase 12 side faces forward when sailing. The cylinder head 14 also defines a combustion chamber 19 in which communication with the intake port 15 and the exhaust port 16 is intermittently connected by the intake valve 17 and the exhaust valve 18 (FIG. 2).
[0013]
An intake device 20 is disposed on one side of the crankcase 12, the cylinder block 13, and the cylinder head 14 so as to face each other. The intake device 20 includes an intake silencer chamber 21 and a throttle body 22 that are opposed to the front surface in the traveling direction of the crankcase 12, and an elbow portion 23 and an elbow portion 23 that are connected to the outlet of the throttle body 22. The surge tank portion 24 is formed, and an intake manifold body 26 is formed of an independent intake pipe portion 25 branched from the surge tank portion 24 and individually connected to the intake port 15 of each cylinder. The intake device 20 is coupled to the engine 4 by the surge tank portion 24 being bolted to the side surface of the crankcase 12 and the downstream end portion of the independent intake pipe portion 25 being bolted to the side surface of the cylinder head 14. Has been.
[0014]
In the independent pipes of the independent intake pipes 25 arranged side by side in the cylinder row direction on the side of the cylinder block 13, there is a short part on the side close to the engine in the connection part with the surge tank part 24 located on the intake upstream side. Two pipelines, a pipeline 27 and a long pipeline 28 far from the engine, are provided in parallel. These two pipe lines 27 and 28 are connected to the common pipe line C on the downstream side and extend to the coupling end 25 c with the cylinder head 14. Each short pipe 27 is provided with a butterfly valve 29 that simultaneously operates in the same direction.
[0015]
The intake manifold body 26 is basically formed by combining an independent intake pipe portion 25 and a hollow surge tank portion 24 each having a short pipe line 27 and a long pipe line 28 in parallel at a middle portion thereof into a split mold. As shown in FIG. 3, it is composed of three blocks. That is, as shown in FIG. 4, the intake manifold body 26 includes an inner block 31 that forms an engine side wall 24a of the anti-throttle body coupling portion 30 and the surge tank portion 24, and an appropriate center of curvature on the engine side. An outer block 32 that forms part of the outer peripheral side half portion 25a of the independent intake pipe portion 25 and the wall 24b opposite to the engine side of the surge tank 24, which is divided by a plane P1 along the intake streamline curved with a large curvature; A half portion 25b on the inner peripheral side of the independent intake pipe portion 25, a cylinder head coupling end 25c of the independent intake pipe portion 25, a butterfly valve support portion 33, an upstream side open end 34 of the short pipe line 27, and a surge tank 24 It consists of an intermediate block 35 that forms an elbow portion 23 continuous with the wall 24b on the engine side. The inner block 31 and the intermediate block 35 are divided along a plane P2 that is substantially parallel to the engine-side wall 24a of the surge tank portion 24.
[0016]
These three blocks 31, 32, and 35 are individually formed by injection molding of a synthetic resin material, and then integrally joined by, for example, a vibration welding method. The joint surfaces shown in FIG. As described above, the concave portion 36 and the convex portion 37 are formed, and a predetermined melting allowance 38 is provided in the convex portion 37 so that the convex portion 37 is melted and welded to the concave portion 36.
[0017]
As shown in FIG. 6, the four butterfly valves 29 are provided on a common shaft 40 on which both ends 40a and 40b and the intermediate portion 40c are supported by individually formed shaft holders 39a to 39c. Yes. One end 40b of the shaft 40 is subjected to a resilient force in the radial direction so that it can be smoothly rotated by a resilient piece 41 formed on the corresponding shaft holder 39b. Yes. Further, the shaft holder 39a integrally formed with the outer block 32 corresponds to the other end 40a of the shaft 40 through a minute gap, and the three shaft holders 39c in the middle portion loosen the middle portion 40c of the shaft 40 very loosely. I accept.
[0018]
A diaphragm actuator 42 having a known structure that is driven by negative pressure of the intake pipe is connected to the other end 40a side (the upper side in the crankshaft direction) of the shaft 40 of the butterfly valve 29. The supply of negative pressure to the diaphragm actuator 42 is interrupted by an electromagnetic valve 43 that is turned on / off by a separate control signal, so that the four butterfly valves 29 are driven to open and close simultaneously.
[0019]
Here, the air chamber 44 of the diaphragm actuator 42 is integrally formed with the intermediate block 35, and the number of parts is reduced (FIG. 8).
[0020]
As shown in FIG. 5, a negative pressure chamber 46 is defined at a position adjacent to the surge tank portion 24 in the inner block 31 in cooperation with a recess 45 formed in the vicinity of the butterfly valve 29 in the intermediate block 35. A bulging portion 46a is integrally formed. In other words, the negative pressure chamber 46 is provided on the intake downstream side of the butterfly valve 29 on the inner peripheral side of the short pipe 27 arranged on the inner peripheral side of the independent intake pipe portion 25 curved with the center of curvature on the engine side, that is, the cylinder. It is arranged at a position adjacent to the butterfly valve 29 close to the head. A cylindrical hole 47 whose bottom communicates with the inside of the surge tank 24 is formed in the middle part of the negative pressure chamber 46 in the cylinder row direction. A negative pressure check valve 48 is mounted in the cylindrical hole 47. ing. The negative pressure check valve 48 includes a relatively soft mushroom-shaped valve member 49, and a valve seat 50 that supports the valve member 49 so as to be movable in the axial direction over a predetermined range and to which the valve member 49 abuts. The valve support member 51 includes a valve support member 51, and the valve support member 51 is fitted into the cylindrical hole 47 through a seal member 52 such as an O-ring.
[0021]
In this way, most of the negative pressure chamber 46, most of the surge tank 24, and the cylindrical hole 47 that communicates between them and mounts the negative pressure check valve 48 are intermediate parts constituting the intake manifold body 26. The block 35 is integrally molded. As a result, there is no need to separately provide a connection pipe for guiding the intake pipe negative pressure to the negative pressure chamber 46.
[0022]
When the negative pressure in the intake pipe increases due to the action of the negative pressure check valve 48, the valve member 49 is sucked to the intake pipe side and is separated from the valve seat 50, whereby the negative pressure chamber 46 becomes negative pressure. When the negative pressure in the intake pipe decreases, the valve member 49 is pressed against the valve seat 50 and the negative pressure in the negative pressure chamber 46 is kept high.
[0023]
The negative pressure chamber 46 is connected to the negative pressure chamber 54 of the diaphragm actuator 42 by a rubber tube 53 with an electromagnetic valve 43 interposed therebetween. When the electromagnetic valve 43 is turned on / off, the negative pressure chamber 46 and the diaphragm actuator 42 are connected. Communication with the negative pressure chamber 54 is interrupted. As shown in FIG. 7, the electromagnetic valve 43 is attached to a stay portion 55 integrally formed at a position adjacent to the atmospheric chamber 44 of the diaphragm actuator 42 on the side surface of the intermediate block 35 with a screw means. Coupled with the fact that 46 is disposed adjacent to the butterfly valve support 33, the rubber tube 53 that connects the negative pressure chamber 46, the electromagnetic valve 43, and the negative pressure chamber 54 of the diaphragm actuator 42 is further shortened. Has been realized.
[0024]
With the above configuration, in the state where the diaphragm 57 is pushed out to the atmosphere chamber 44 side by the extension force of the compression coil spring 56 contracted in the negative pressure chamber 54 of the diaphragm actuator 42, the butterfly valve 29 opens and immediately before the butterfly valve 29. A state in which the short pipe line 27 extending from the open end 34 located at the center to the cylinder head coupling end 25c through the common pipe C and the intake upstream end of the long pipe line 28 is communicated (high speed / high load operation region) Become. When the diaphragm 57 is drawn toward the negative pressure chamber 54 by introducing a negative pressure into the negative pressure chamber 54 of the diaphragm actuator 42, the butterfly valve 29 is closed (the state indicated by a two-dot chain line in FIG. 4), Only the long pipe 28 where the opening end 28a is located upstream of the opening end 34 of the short pipe 27 communicates (low speed / low load operation region). In this way, the cross-sectional area of the intake pipe and the pipe length can be switched in two stages according to the operating state of the engine 4.
[0025]
As shown in FIG. 4, the downstream edge of the pipe wall 58 separating the most upstream portion of the long pipe passage 28 from the short pipe passage 27 and the open end 34 of the short pipe passage 27 in the surge tank 24 It is placed on the same plane D. This plane D is orthogonal to the parting surface of the mold together with the axis of the cylinder head coupling end 25c of the independent intake pipe portion 25, so that the middle block 35 is not obstructed. . Note that the axis of the recess 45 forming the negative pressure chamber 46 and the axis of the cylindrical hole 47 in which the negative pressure check valve 48 is mounted are also taken into account in consideration of die cutting of the intermediate block 35. It is orthogonal to.
[0026]
The direction of the central axis A of the atmospheric chamber 44 of the diaphragm actuator 42 is inclined with respect to the die-cutting direction of the intermediate block 35, that is, the direction parallel to the plane D (see FIG. 8). It is molded using another slide mold 61. If the opening surface 62 of the atmospheric chamber 44 is directed right above in FIG. 8 and the central axis A is parallel to the plane D, another slide mold 61 can be eliminated.
[0027]
【The invention's effect】
As described above in detail, according to the present invention, the plurality of independent intake pipe portions individually connected to the combustion chambers of the plurality of cylinders and arranged in parallel in the cylinder row direction are curved with the center of curvature on the engine side. The short pipe line that opens and closes by the butterfly valve is arranged on the inner peripheral side, and the butterfly valve is disposed at the position adjacent to the butterfly valve on the inner peripheral side of the pipe, on the downstream side of the intake of the butterfly valve, that is, closer to the cylinder head. Since the negative pressure chamber that stores the operating pressure to the diaphragm actuator to be driven is arranged, the part of the intake pipe that is curved in order to extend to the side of the cylinder block is usually a dead space. Since it can be used effectively, a great effect can be achieved in further promoting the downsizing of the intake manifold body. In particular, by disposing the negative pressure chamber adjacent to the butterfly valve, the negative pressure chamber can be brought close to the diaphragm actuator, which is effective in further shortening the negative pressure supply pipe.
[Brief description of the drawings]
FIG. 1 is a side view of an essential part of an outboard motor to which the present invention is applied. FIG. 2 is a top view of the outboard motor to which the present invention is applied. FIG. 3 is an exploded perspective view of an intake manifold body according to the present invention. 4 is a horizontal cross-sectional view of an intake manifold body according to the present invention. FIG. 5 is a horizontal cross-sectional view of the main part of the intake manifold body according to the present invention. Fig. 8 is a top plan view of the main part of the intake manifold body according to the present invention. Fig. 8 is a top plan view of the main part of the diaphragm actuator forming part of the intake manifold body according to the present invention.
19 Combustion chamber 20 Intake device 24 for internal combustion engine Surge tank 25 Independent intake pipe section 27 Short pipe line 28 Long pipe line 29 Butterfly valve 42 Diaphragm actuator 46 Negative pressure chamber

Claims (2)

吸気管路長が互いに異なる2つの管路を並列に有し複数の気筒の各燃焼室に連結された複数の独立吸気管と当該独立吸気管のそれぞれに連通する共通のサージタンクとを備えた吸気マニホルド体と、前記2つの管路の一方を開閉する弁と、前記弁を開閉駆動する負圧応動アクチュエータと、前記負圧応動アクチュエータに供給する作動圧を蓄える蓄圧タンクとを有する内燃機関用吸気装置であって、
前記吸気マニホルド体は、スロットルボディの連結部と前記サージタンクのエンジン側の壁とを一体形成された内側ブロックと、前記サージタンクの反エンジン側の壁と前記独立吸気管の外側の半分を一体形成された外側ブロックと、前記独立吸気管の対シリンダヘッド結合端と前記独立吸気管の内側の半分を一体形成された中間ブロックとにより3分割構成されており、前記内側ブロックと前記中間ブロックとによって前記蓄圧タンクが形成され、前記中間ブロックに吸気管負圧を前記蓄圧タンクに導く孔が形成されている共に前記孔を逆止する負圧チェック弁が取り付けられていることを特徴とする内燃機関用吸気装
A plurality of independent intake pipes connected in parallel to the combustion chambers of a plurality of cylinders, and a common surge tank communicating with each of the independent intake pipes. For an internal combustion engine having an intake manifold body, a valve for opening and closing one of the two pipe lines, a negative pressure responsive actuator for opening and closing the valve, and a pressure accumulating tank for storing an operating pressure supplied to the negative pressure responsive actuator An air intake device,
The intake manifold body has an inner block formed integrally with a throttle body connecting portion and an engine side wall of the surge tank, and an anti-engine side wall of the surge tank and an outer half of the independent intake pipe. The outer block formed is divided into a cylinder head coupling end of the independent intake pipe and an intermediate block integrally formed with the inner half of the independent intake pipe, and the inner block and the intermediate block are divided into three parts. The pressure accumulation tank is formed by the internal combustion engine, and a hole for guiding the intake pipe negative pressure to the pressure accumulation tank is formed in the intermediate block, and a negative pressure check valve for reversing the hole is attached. Engine intake system
前記内側ブロックと前記外側ブロックと前記中間ブロックは、合成樹脂材の射出成型品であり、振動溶着法によって一体結合されていることを特徴とする請求項に記載の内燃機関用吸気装置。 The intake device for an internal combustion engine according to claim 1 , wherein the inner block, the outer block, and the intermediate block are injection molded products of a synthetic resin material, and are integrally coupled by a vibration welding method.
JP2003168909A 2003-06-13 2003-06-13 Intake device for internal combustion engine Expired - Fee Related JP4320215B2 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
JP2003168909A JP4320215B2 (en) 2003-06-13 2003-06-13 Intake device for internal combustion engine
CA2470599A CA2470599C (en) 2003-06-13 2004-06-10 Dual port intake device for an internal combustion engine formed by injection molding
US10/866,165 US6997157B2 (en) 2003-06-13 2004-06-14 Dual port intake device for an internal combustion engine formed by injection molding
CNB2004100429954A CN1316158C (en) 2003-06-13 2004-06-14 Dual port intake device for an internal combustion engine formed by injection molding

Applications Claiming Priority (1)

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JP2003168909A JP4320215B2 (en) 2003-06-13 2003-06-13 Intake device for internal combustion engine

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JP4320215B2 true JP4320215B2 (en) 2009-08-26

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