JPS6035540B2 - Flow path control device for helical intake port - Google Patents

Flow path control device for helical intake port

Info

Publication number
JPS6035540B2
JPS6035540B2 JP56122408A JP12240881A JPS6035540B2 JP S6035540 B2 JPS6035540 B2 JP S6035540B2 JP 56122408 A JP56122408 A JP 56122408A JP 12240881 A JP12240881 A JP 12240881A JP S6035540 B2 JPS6035540 B2 JP S6035540B2
Authority
JP
Japan
Prior art keywords
valve
passage
spiral
wall surface
intake
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
JP56122408A
Other languages
Japanese (ja)
Other versions
JPS5823228A (en
Inventor
頼成 前田
勝彦 本杉
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.)
Toyota Motor Corp
Original Assignee
Toyota Motor Corp
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 Toyota Motor Corp filed Critical Toyota Motor Corp
Priority to JP56122408A priority Critical patent/JPS6035540B2/en
Publication of JPS5823228A publication Critical patent/JPS5823228A/en
Publication of JPS6035540B2 publication Critical patent/JPS6035540B2/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F1/00—Cylinders; Cylinder heads 
    • F02F1/24—Cylinder heads
    • F02F1/42—Shape or arrangement of intake or exhaust channels in cylinder heads
    • F02F1/4228—Helically-shaped channels 
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B31/00—Modifying induction systems for imparting a rotation to the charge in the cylinder
    • F02B31/04—Modifying induction systems for imparting a rotation to the charge in the cylinder by means within the induction channel, e.g. deflectors
    • F02B31/042—Modifying induction systems for imparting a rotation to the charge in the cylinder by means within the induction channel, e.g. deflectors induction channel having a helical shape around the intake valve axis
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Lubrication Of Internal Combustion Engines (AREA)
  • Valve-Gear Or Valve Arrangements (AREA)

Description

【発明の詳細な説明】 本発明はへIJカル型吸気ボートの流路制御装置に関す
る。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a flow path control device for an IJ cal-type intake boat.

へIJカル型吸気ボートは通常吸気弁周りに形成された
渦巻部と、この渦巻部に接線状に接続されかつほぼまつ
すぐに延びる入口通路部とにより構成される。
The IJ cal-type intake boat is usually composed of a spiral portion formed around the intake valve and an inlet passage portion that is tangentially connected to the spiral portion and extends almost straight.

このようなヘリカル型吸気ボートを用いて吸入空気量の
少ない機関低速低負荷運転時に機関燃焼室内に強力な旋
回流を発生せしめようとすると吸気ボート形状が流れ抵
抗の大きな形状になってしまうので吸入空気量の多い機
関高速高負荷運転時に充填効率が低下するという問題が
ある。このような問題を解決するためにへIJカル型吸
気ボート入口通路部から分岐されてへりカル型吸気ボー
ト渦巻部の渦巻終端部に蓮適する分岐路をシリンダヘツ
ド内に形成し、分岐路内にアクチュェータによって作動
される常時閉鎖型開閉弁を設けて機関吸入空気量が所定
量よりも大きくなったときにアクチュェータを作動させ
て開閉弁を開弁するようにしたヘリカル型吸気ボート流
路制御装置が本出願人により既に提案されている。この
ヘリカル型吸気ボートでは機関吸入空気量の多い機関高
速高負荷運転時にへIJカル型吸気ボート入口通路部内
に送り込まれた吸入空気の一部が分岐路を介してへIJ
カル型吸気ボート渦巻部内に送り込まれるために吸入空
気流に対する流れ抵抗が低下し、斯くして高い充填効率
を得ることができる。しかしながらこの流路制御装置は
基本作動原理を示しているにすぎず、従ってこの流路制
御装置を実用化するには組立工数、製造の容易さ、確実
な作動、製造コストの面で種々の問題が残されている。
本発明は本願出願人により既に提案されている上述の基
本作動原理を実用化するのに適した構造を有するヘリカ
ル型吸気ボート流路制御装置を提供することにある。
If you try to use such a helical intake boat to generate a strong swirling flow in the combustion chamber of the engine when the engine is operating at low speed and low load with a small amount of intake air, the shape of the intake boat will have a large flow resistance. There is a problem in that the filling efficiency decreases when the engine is operated at high speed and under high load with a large amount of air. In order to solve this problem, a branch path is formed in the cylinder head that branches from the helical type intake boat inlet passage and is suitable for the end of the spiral of the helical type intake boat volute. A helical intake boat flow path control device is provided with a normally closed on-off valve operated by an actuator, and the actuator is operated to open the on-off valve when the amount of engine intake air exceeds a predetermined amount. This has already been proposed by the applicant. In this helical type intake boat, when the engine is operated at high speed and under high load with a large amount of engine intake air, part of the intake air sent into the inlet passage of the IJ helical type intake boat passes through the branch path to the IJ.
The flow resistance to the intake air flow is reduced because it is fed into the cull-type intake boat volute, and thus a high filling efficiency can be obtained. However, this flow path control device only shows the basic operating principle, and therefore, there are various problems in terms of assembly man-hours, ease of manufacturing, reliable operation, and manufacturing cost in order to put this flow path control device into practical use. is left behind.
An object of the present invention is to provide a helical intake boat flow path control device having a structure suitable for putting into practical use the above-mentioned basic operating principle that has already been proposed by the applicant of the present application.

以下、添附図面を参照して本発明を詳細に説明する。Hereinafter, the present invention will be described in detail with reference to the accompanying drawings.

第1図並びに第2図を参照すると、1はシリンダブロッ
ク、2はシリンダブロック1内で往復動するピストン、
3はシリングブロック1上に固定されたシリンダヘツド
、4はピストン2とシリンダヘッド3間に形成された燃
焼室、5は吸気弁、6はシリンダヘッド3内に形成され
たヘリカル型吸気ボート、7は排気弁、8はシリンダヘ
ッド3内に形成された排気ボートを夫々示す。
Referring to FIG. 1 and FIG. 2, 1 is a cylinder block, 2 is a piston that reciprocates within the cylinder block 1,
3 is a cylinder head fixed on the cylinder block 1, 4 is a combustion chamber formed between the piston 2 and the cylinder head 3, 5 is an intake valve, 6 is a helical intake boat formed inside the cylinder head 3, 7 8 indicates an exhaust valve, and 8 indicates an exhaust boat formed within the cylinder head 3.

なお、図には示さないが燃焼室4内に点火栓が配置され
る。第3図から第5図に第2図のへりカル型吸気ボート
6の形状を図解的に示す。
Although not shown in the figure, an ignition plug is disposed within the combustion chamber 4. 3 to 5 schematically show the shape of the helical type intake boat 6 shown in FIG. 2.

このヘリカル型吸気ボート6は第4図に示されるように
流路軸線aがわずかに轡曲した入口通路部Aと、吸気弁
5の弁軸周りに形成された渦巻部Bとにより構成され、
入口通路部Aは渦巻部Bに接線状に接続される。第3図
、第4図並びに第7図に示されるように入口通路部Aの
渦巻軸線bに近い側の側壁面9の上方側壁面9aは下方
を向いた傾斜面に形成され、この傾斜面9aの中は渦巻
部Bに近づくに従って広くなり、入口通路部Aと渦巻部
Bとの接続部においては第7図に示されるように側壁面
9の全体が下向に向いた傾斜面9aに形成される。側壁
面9の上半分は吸気弁ガイド10(第2図)周りの吸気
ボート上壁面上に形成された円筒状突起11の周壁面に
滑らかに叢続され、一方側壁面9の下半分は渦巻部Bの
渦巻終端部Cにおいて渦巻部Bの側壁面12に接続され
る。なお、渦巻部Bの上壁面13は渦巻終端部Cにおい
て下向きの急傾斜壁肌こ接続される。一方、第1図から
第5図に示されるようにシリンダヘッド3内には入口通
路部Aから分岐されたほぼ一様断面の分岐路14が形成
され、この分岐路14は渦巻終端部Cに接続される。
As shown in FIG. 4, this helical intake boat 6 is composed of an inlet passage section A in which the flow path axis a is slightly curved, and a spiral section B formed around the valve axis of the intake valve 5.
The inlet passage section A is tangentially connected to the spiral section B. As shown in FIGS. 3, 4, and 7, the upper side wall surface 9a of the side wall surface 9 on the side closer to the spiral axis b of the inlet passage A is formed into a downwardly oriented inclined surface, and this inclined surface The inside of 9a becomes wider as it approaches the spiral part B, and at the connection part between the inlet passage part A and the spiral part B, the entire side wall surface 9 forms a downwardly facing inclined surface 9a, as shown in FIG. It is formed. The upper half of the side wall surface 9 is smoothly connected to the peripheral wall surface of a cylindrical protrusion 11 formed on the upper wall surface of the intake boat around the intake valve guide 10 (FIG. 2), while the lower half of the side wall surface 9 is spirally connected. It is connected to the side wall surface 12 of the spiral portion B at the spiral end portion C of the portion B. Incidentally, the upper wall surface 13 of the spiral portion B is connected to the steeply downwardly inclined wall surface at the spiral end portion C. On the other hand, as shown in FIGS. 1 to 5, a branch passage 14 with a substantially uniform cross section is formed in the cylinder head 3, branching from the inlet passage part A, and this branch passage 14 is connected to the spiral terminal part C. Connected.

分岐路14の入口関口15は入口通路部Aの入口開□近
傍において側壁面9上に形成され、分岐路14の出口開
□16は渦巻終端部Cにおいて側壁面12の上端部に形
成される。この出口閉口16の上綾部は渦巻部Bの上壁
面13に面一に連結され、更に出口関口16は渦巻部B
の上壁面13に沿って渦巻方向に旋回する旋回流に対向
するように形成される。シリンダヘッド3内には分岐路
14を貫通して延びる開閉弁挿入孔17が穿設され、こ
の開閉弁挿入孔17内には夫々通路開閉弁の作用をなす
港勤弁18が挿入される。第9図を参照すると、摺敷弁
18は開閉弁挿入孔17内に鉄着された中空スリーブ1
9と、中空スリーブ19中に沼動可能に挿入されかつ分
岐路14内に突出可能な弁体20と、ロッド21を介し
て弁体20に結合されたピストン22とを具備し、ロッ
ド21は中空スリーブ19内に形成された隔壁23を貫
通する。中空スリーブ19の外周面と開閉弁挿入孔17
の内周面間には一対の○リング24,25が挿入され、
隔壁23上にはロッド21と密封的に接触するシール部
村26が取付けられる。弁体20と隔壁23間には弁体
20を常時下方に向けて押圧する圧縮ばね27が挿入さ
れ、弁体20の外周面上には第9図並びに第10図に示
されるように複数個の空気逃し溝28が形成される。一
方、中空スリーブ19の上方部には関孔29が穿設され
、第9図に示す実施例ではこの関孔29はステムガィド
10から上方に突出する吸気弁5のステムに指向される
。ピストン22と隔壁23間に形成される作動油圧室3
川ま中空スリーブ19に形成された油導入孔31を介し
て中空スリーブ19周りに形成された環状潤滑油通路3
2に蓮適する。この環状潤滑油通路32は潤滑油路33
を介して各気筒の摺動弁18に通ずる集合通路34に蓮
適する。集合通路34は下方に延びる潤滑油供給通路3
5、電磁開閉弁36並びに潤滑油供給通路37を介して
図示しない機関駆動の潤滑油供給ポンプに後続され、電
磁開閉弁36のソレノイドは電子制御ユニット38の出
力端子に接続される。−方、集合通路34は上方に延び
る潤滑油返戻通路39、4・断面積の絞り通路40並び
に潤滑油返戻通路41を介して図示しない潤滑油溜りに
接続される。なお、第9図からわかるように絞り通路4
0‘ま集合通路40の上方でかつ作動油圧室30の上方
に配置されている。電子制御ユニット38はディジタル
コンピュータからなり、各種の演算処理を行なうマイク
ロプロセッサ(MPU)50、ランダムアクセスメモリ
(RAM)51、制御プログラム、演算定数等が予め格
納されているリードオンリメモリ(ROM)52、入力
ボート53並びに出力ボート54が双方向性バス55を
介して互に接続されている。
The entrance gate 15 of the branch passage 14 is formed on the side wall surface 9 near the entrance opening □ of the inlet passage section A, and the exit opening □ 16 of the branch passage 14 is formed at the upper end of the side wall surface 12 at the spiral terminal end C. . The upper twill portion of this outlet closing port 16 is connected flush with the upper wall surface 13 of the spiral portion B, and the exit closing port 16 is connected flush with the upper wall surface 13 of the spiral portion B
It is formed so as to face a swirling flow that swirls in a spiral direction along the upper wall surface 13 of. An on-off valve insertion hole 17 is formed in the cylinder head 3 and extends through the branch passage 14, and a port valve 18 functioning as a passage on-off valve is inserted into each of the on-off valve insertion holes 17. Referring to FIG. 9, the sliding valve 18 has a hollow sleeve 1 iron-fitted in the opening/closing valve insertion hole 17.
9, a valve body 20 movably inserted into the hollow sleeve 19 and capable of protruding into the branch passage 14, and a piston 22 coupled to the valve body 20 via a rod 21, the rod 21 It passes through a partition 23 formed within the hollow sleeve 19. Outer peripheral surface of hollow sleeve 19 and on-off valve insertion hole 17
A pair of ○ rings 24 and 25 are inserted between the inner peripheral surfaces of
A sealing village 26 is mounted on the partition wall 23 in sealing contact with the rod 21. A compression spring 27 is inserted between the valve body 20 and the partition wall 23 to constantly press the valve body 20 downward, and a plurality of compression springs 27 are inserted on the outer peripheral surface of the valve body 20 as shown in FIGS. 9 and 10. An air relief groove 28 is formed. On the other hand, a stopper hole 29 is bored in the upper part of the hollow sleeve 19, and in the embodiment shown in FIG. A working hydraulic chamber 3 formed between the piston 22 and the partition wall 23
An annular lubricating oil passage 3 formed around the hollow sleeve 19 via an oil introduction hole 31 formed in the hollow sleeve 19
Lotus is suitable for 2. This annular lubricating oil passage 32 is a lubricating oil passage 33
It is connected to a collecting passageway 34 which leads to the sliding valve 18 of each cylinder via the cylinder. The collective passage 34 is the lubricating oil supply passage 3 extending downward.
5. It is followed by an engine-driven lubricating oil supply pump (not shown) via an electromagnetic on-off valve 36 and a lubricating oil supply passage 37, and the solenoid of the electromagnetic on-off valve 36 is connected to an output terminal of an electronic control unit 38. On the other hand, the collective passage 34 is connected to a lubricating oil reservoir (not shown) through a lubricating oil return passage 39 extending upward, a throttle passage 40 having a cross-sectional area of 4, and a lubricating oil return passage 41. Furthermore, as can be seen from Fig. 9, the throttle passage 4
0' is disposed above the collective passage 40 and above the hydraulic pressure chamber 30. The electronic control unit 38 is comprised of a digital computer, including a microprocessor (MPU) 50 that performs various calculation processes, a random access memory (RAM) 51, and a read-only memory (ROM) 52 in which control programs, calculation constants, etc. are stored in advance. , an input boat 53 and an output boat 54 are connected to each other via a bidirectional bus 55.

更に、電子制御ユニット38内には各種のクロック信号
を発生するクロツク発生器56が設けられる。入力ボー
ト53には負圧センサ57がAD変換器58を介して接
続され、更に入力ボート53には回転数センサ59が接
続される。負圧センサ57は図示しない気化器後流の吸
気マニホルド内の負圧に比例した出力電圧を発生し、こ
の電圧がAD変換器58において対応する2進数に変換
されてこの2進数が入力ボート53並びにバス55を介
してMPU50に読み込まれる。回転数センサ59はク
ランクシャフトが所定クランク角度回転する毎にパルス
を発生し、このパルスが入力ボート53並びにバス55
を介してMPU5川こ読み込まれる。一方、出力ボート
54は電力増中回路60を介して電磁開閉弁36のソレ
ノィド‘こ接続される。第11図は電磁開閉弁36を作
動すべき機関回転数N(r.p.m)と吸気マニホルド
内の負圧P(一肌日夕)との関係を示している。
Furthermore, a clock generator 56 is provided within the electronic control unit 38 for generating various clock signals. A negative pressure sensor 57 is connected to the input boat 53 via an AD converter 58, and a rotation speed sensor 59 is further connected to the input boat 53. The negative pressure sensor 57 generates an output voltage proportional to the negative pressure in the intake manifold downstream of the carburetor (not shown), and this voltage is converted into a corresponding binary number by the AD converter 58, and this binary number is sent to the input port 53. It is also read into the MPU 50 via the bus 55. The rotation speed sensor 59 generates a pulse every time the crankshaft rotates by a predetermined crank angle, and this pulse is sent to the input boat 53 and the bus 55.
The MPU5 is loaded via. On the other hand, the output boat 54 is connected to the solenoid of the electromagnetic on-off valve 36 via a power increase circuit 60. FIG. 11 shows the relationship between the engine rotational speed N (r.p.m.) at which the electromagnetic on-off valve 36 should be operated and the negative pressure P (per day) in the intake manifold.

なお、第11図の実線Wよりも上のハッチング領域にお
いて電磁開閉弁36が作動せしめられる。第11図にお
いて実線Wで示す機関回転数Nと負圧Pとの関係は関数
の形で或いはデータテーブルの形で予めROM52内に
格納されている。MPU50では回転数センサ59の出
力信号から機関回転数Nが計算され、この機関回転数N
と負圧Pを表わす負圧センサ57の出力信号とがROM
52に記憶された関数Wと比較されて機関回転数Nと負
圧Pが第11図のハッチング領域にあるときには出力ボ
ート54に駆動信号が書き込まれる。このとき、電磁開
閉弁36のソレノィドが付勢されるために電磁開閉弁3
6が関弁せしめられ、その結果加圧された潤滑油が潤滑
油供給通路37、電磁開閉弁36並びに潤滑油供給通路
35を介して集合通路34内に供給される。次いでこの
潤滑油は一方では絞り通路40並びに潤滑油返戻通路4
1を介して潤滑油溜りに返戻され、他方では環状潤滑油
通路32を介して作動油圧室30内に流入する。このと
き絞り通路40の断面積はかなり小さいので集合通路4
0内の圧力はかなり高く、従ってピストン22が圧縮は
ね27に抗して上昇するために弁体20が上昇して分岐
路14を開□せしめる。なお、弁体20の外周面には空
気逃し溝28が形成されているので弁体20が上昇して
も弁体20と燭23間の中空スリ−ブ内部室が加圧され
ることがなく、斯くして弁体20は容易に上昇する。ピ
ストン22が上昇すると関孔29が作動油圧室30内に
開口するために作動油圧室30内の潤滑油が開孔29か
ら流出し、その結果作動油圧室30内の潤滑油圧が低下
するためにピストン22は開孔29が作動油圧室30内
に閉口したところで停止する。従って開孔39はピスト
ン22の上昇位置を規制するストッパの役割を果す。更
に、前述したように開孔29は吸気弁5のステムに指向
されているために開孔29から噴出する潤滑油によって
吸気弁5のステムとガイド10間の潤滑を行なうことが
できる。なお、関孔29はシリンダヘッド上の潤滑を必
要とする箇所、例えば動弁機構のカム面上に指向させる
ことができる。一方、機関回転数Nと負圧Pとの交点が
第11図のハッチング領域でない領域に移ると電磁開閉
弁36のソレノィドが消勢されるために電磁開閉弁36
が閉弁する。
Note that the electromagnetic on-off valve 36 is operated in the hatched area above the solid line W in FIG. The relationship between engine speed N and negative pressure P, indicated by a solid line W in FIG. 11, is stored in the ROM 52 in advance in the form of a function or data table. The MPU 50 calculates the engine rotation speed N from the output signal of the rotation speed sensor 59, and calculates the engine rotation speed N.
and the output signal of the negative pressure sensor 57 representing the negative pressure P are stored in the ROM.
When the engine speed N and the negative pressure P are in the hatched area in FIG. 11, a drive signal is written to the output boat 54. At this time, the solenoid of the electromagnetic on-off valve 36 is energized, so the electromagnetic on-off valve 3
6 is closed, and as a result, pressurized lubricating oil is supplied into the collective passage 34 via the lubricating oil supply passage 37, the electromagnetic on-off valve 36, and the lubricating oil supply passage 35. This lubricating oil then passes through the throttle passage 40 on the one hand and the lubricating oil return passage 4 on the other hand.
1 to the lubricating oil reservoir, and on the other hand it flows into the hydraulic pressure chamber 30 via the annular lubricating oil passage 32. At this time, since the cross-sectional area of the throttle passage 40 is quite small, the collective passage 4
The pressure in the valve 0 is quite high, so that the piston 22 rises against the compression spring 27, causing the valve body 20 to rise and open the branch passage 14. Furthermore, since an air relief groove 28 is formed on the outer peripheral surface of the valve body 20, even if the valve body 20 rises, the internal chamber of the hollow sleeve between the valve body 20 and the candle 23 will not be pressurized. , thus the valve body 20 is easily raised. When the piston 22 rises, the separator hole 29 opens into the working hydraulic pressure chamber 30, so that the lubricating oil in the working hydraulic pressure chamber 30 flows out from the opening 29, and as a result, the lubricating oil pressure in the working hydraulic pressure chamber 30 decreases. The piston 22 stops when the opening 29 closes into the hydraulic pressure chamber 30. Therefore, the opening 39 serves as a stopper that restricts the upward position of the piston 22. Further, as described above, since the aperture 29 is oriented toward the stem of the intake valve 5, the lubricating oil jetted from the aperture 29 can lubricate the space between the stem of the intake valve 5 and the guide 10. Note that the checkpoint hole 29 can be directed toward a location on the cylinder head that requires lubrication, such as a cam surface of a valve mechanism. On the other hand, when the intersection of the engine speed N and the negative pressure P moves to a region other than the hatched region in FIG.
is closed.

このとき作動油圧室30内の潤滑油は絞り通路40を介
して徐々に流出するためにピストン22が徐々に下降し
、弁体20が分岐路14を遮断する。前述したように絞
り通路40は集合通路34並びに作動油圧室30よりも
上方に設けられているのでピストン22が最下降位置ま
で達しても集合通路34並びに作動油圧室3川ま潤滑油
で満たされている。従って再び電磁開閉弁36が開弁し
たとき作動油圧室30内を即座に加圧でき、斯くして分
岐路14を即座に開□することができる。第11図にお
いてハッチングで示す領域は吸入空気量が多い領域を示
しており、従って吸入空気量が多いときには糟勤弁18
が開弁し、吸入空気量が少ないときには酒動弁18が閉
弁することがわかる。上述したように吸入空気量が少な
い機関低速低負荷運転時には摺動弁18が分岐路14を
遮断している。
At this time, the lubricating oil in the hydraulic pressure chamber 30 gradually flows out through the throttle passage 40, so the piston 22 gradually descends, and the valve body 20 blocks the branch passage 14. As mentioned above, since the throttle passage 40 is provided above the collective passage 34 and the hydraulic pressure chamber 30, even when the piston 22 reaches the lowest position, the collective passage 34 and the hydraulic pressure chamber 3 are filled with lubricating oil. ing. Therefore, when the electromagnetic on-off valve 36 is opened again, the inside of the hydraulic pressure chamber 30 can be pressurized immediately, and the branch passage 14 can thus be opened immediately. In FIG. 11, the hatched area indicates a region where the amount of intake air is large. Therefore, when the amount of intake air is large, the
It can be seen that the alcohol valve 18 is opened and the alcohol valve 18 is closed when the amount of intake air is small. As described above, the sliding valve 18 blocks the branch passage 14 when the engine is operated at low speed and under low load with a small amount of intake air.

このとき入口通路部A内に送り込まれた混合気は渦巻部
Bの上壁面13に沿って旋回しつつ渦巻部B内に下降し
、次いて旋回しつつ燃焼室4内に流入するので燃焼室4
内には強力な旋回流が発生せしめられる。一方、吸入空
気量が多い機関高速高負荷運転時には摺動弁18が開弁
するので入口通路部A内に送り込まれた浪合気の一部が
流れ抵抗の小さな分岐路14を介して渦巻部B内に送り
込まれる。前述したように分岐路14の出口開ロー6の
上端緑は渦巻部Bの上壁面13に面一に連結されている
ので分岐路14から流出した混合気は渦巻部Bの上壁面
13に沿って旋回する全混合気流と正面衝突して渦巻部
Bの上壁面13に沿う全混合気流を減速せしめる。即ち
、渦巻部B内に発生する旋回流のうちで渦巻部Bの上端
面13に沿う旋回流が最も強力であり、この旋回力をも
つ全混合気流が減速せしめられる。このように機関高速
高負荷運転時には摺動弁18が開弁することによって全
体の流路面積が増大するばかりでなく強力な旋回力をも
つ全混合気流が減速せしめられることにより旋回流が大
中に弱められるので高い充填効率を確保することができ
る。また上述したように傾斜面9aを設けることによっ
て入口通路部Aに送り込まれた混合気の一部は下向きの
力を与えられ、その結果この混合気は旋回することなく
入口通路部Aの下壁面に沿って渦巻部B内に流入するた
めに流入抵抗は小さくなり、斯くして高速高負荷運転時
における充填効率を更に高めることができる。以上述べ
たように本発明によれば分岐路の出口開□の上端緑が渦
巻部の上壁面に面一に連結されているので摺動弁が開弁
したときに分岐路から流出する混合気により渦巻部の上
壁面に沿って強力な旋回力をもって旋回する全混合気流
を減速せしめることができ、斯くして旋回流を大中に弱
めることができるので高い充填効率を得ることができる
。
At this time, the air-fuel mixture sent into the inlet passage part A descends into the swirl part B while swirling along the upper wall surface 13 of the swirl part B, and then flows into the combustion chamber 4 while swirling, so that the mixture enters the combustion chamber 4. 4
A strong swirling flow is generated inside. On the other hand, when the engine is operated at high speed and under high load with a large amount of intake air, the sliding valve 18 is opened, so that a part of the Nami Aiki sent into the inlet passage A flows through the branch passage 14 with low flow resistance to the spiral part B. sent inside. As mentioned above, the upper green end of the outlet opening row 6 of the branch passage 14 is connected flush with the upper wall surface 13 of the spiral part B, so that the air-fuel mixture flowing out from the branch passage 14 flows along the upper wall surface 13 of the spiral part B. It collides head-on with the swirling total air mixture flow, thereby decelerating the total air mixture flow along the upper wall surface 13 of the swirl portion B. That is, among the swirling flows generated in the swirling portion B, the swirling flow along the upper end surface 13 of the swirling portion B is the strongest, and the entire air mixture flow having this swirling force is decelerated. In this manner, when the engine is operated at high speed and under high load, the sliding valve 18 opens, which not only increases the overall flow path area, but also decelerates the entire air mixture flow, which has a strong swirling force, thereby increasing the swirling flow. Since it is weakened, high filling efficiency can be ensured. Further, as described above, by providing the inclined surface 9a, a part of the air-fuel mixture fed into the inlet passage A is given a downward force, and as a result, the air-fuel mixture is moved to the lower wall of the inlet passage A without swirling. Since the fluid flows into the spiral portion B along the curve, the inflow resistance becomes small, thus making it possible to further improve the filling efficiency during high-speed, high-load operation. As described above, according to the present invention, the upper green end of the branch outlet opening □ is connected flush with the upper wall surface of the spiral part, so that the air-fuel mixture flows out from the branch channel when the slide valve opens. This makes it possible to decelerate the total air mixture flow that swirls with a strong swirling force along the upper wall surface of the swirling portion, and in this way, the swirling flow can be weakened to a large extent, so that high filling efficiency can be obtained.

また本発明によれば機関が本体具備している潤滑油圧を
用いて簡単な機構で分岐路の開閉制御を行なうことがで
きるので信頼性を向上できると共に製造コストを低減す
ることができる。更に潤滑油圧による油圧制御を採用す
ることによって摺動弁の寸法を小型化できるのでスペー
スの狭いシリンダヘツドもこ容易に取付けることができ
る。更に、摺動弁のピストン作動油圧室が潤滑油返戻用
絞り通路を介して常時潤滑油溜りに蓮適しているために
電磁開閉弁に漏れが生じても漏れた加圧潤滑油は絞り通
路を介して潤滑油溜り}こ返戻されるので沼勤弁が誤作
動することはなく、更に絞り通路が作動油圧室よりも上
方に配置されているので作動油圧室は潤滑油で常時満た
され、従って電磁開閉弁が関弁したときに分岐路を即座
に関口することができる。
Further, according to the present invention, the opening and closing of the branch passage can be controlled by a simple mechanism using the lubricating oil pressure provided in the main body of the engine, so that reliability can be improved and manufacturing costs can be reduced. Furthermore, by adopting hydraulic control using lubricating oil pressure, the size of the slide valve can be reduced, so that it can be easily installed in a cylinder head with a narrow space. Furthermore, since the piston-operated hydraulic chamber of the sliding valve is always connected to the lubricant reservoir via the lubricant return throttle passage, even if there is a leak in the electromagnetic on-off valve, the leaked pressurized lubricant will flow through the throttle passage. Since the lubricating oil reservoir is returned to the lubricating oil reservoir through When the electromagnetic on-off valve is closed, the branch can be immediately closed.

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

第1図は本発明に係る内燃機関の平面図、第2図は第1
図の0−ロ線に沿つみた断面図、第3図はへりカル型吸
気ボートの形状を示す斜視図、第4図は第3図の平面図
、第5図は第3図の分岐路に沿って切断した側面断面図
、第6図は第4図のW−の線に沿ってみた断面図、第7
図は第4図の肌−肌線に沿ってみた断面図、第8図は第
4図の肌−脚線に沿ってみた断面図、第9図は流路制御
装置の全体図、第10図は第9図のX−X線に沿ってみ
た断面図、第11図は損動弁の開弁領域を示す図である
。 5・・…・吸気弁、6・・・・・・ヘリカル型吸気ボー
ト、14・・・・・・分岐路、18…・・・摺動弁、2
0・・・・・・弁体、36・・…・電磁開閉弁。 第2図 孫6図 孫l図 第3図 繁7図 第8図 孫ll図 務4図 第5図 鱗9図 鯖l○図
FIG. 1 is a plan view of an internal combustion engine according to the present invention, and FIG.
3 is a perspective view showing the shape of the helical intake boat, 4 is a plan view of 3, and 5 is a branch road of 3. 6 is a sectional view taken along the line W- in FIG. 4, and FIG.
The figure is a sectional view taken along the skin-to-skin line in Figure 4, Figure 8 is a sectional view taken along the skin-to-leg line in Figure 4, Figure 9 is an overall view of the flow path control device, and Figure 10 is a sectional view taken along the skin-to-skin line in Figure 4. The figure is a sectional view taken along the line XX in FIG. 9, and FIG. 11 is a diagram showing the valve opening area of the loss-operating valve. 5... Intake valve, 6... Helical intake boat, 14... Branch path, 18... Sliding valve, 2
0... Valve body, 36... Solenoid on-off valve. Figure 2: Grandson 6 Figure: Grandchild l Figure 3: Shigetsu 7 Figure 8: Grandson ll Administration 4 Figure 5: Scales 9 Figure: Mackerel l○ Figure

Claims (1)

【特許請求の範囲】[Claims] 1 吸気弁周りに形成さた渦巻部と、該渦巻部に接線状
に接続されかつほぼまつすぐに延びる入口通路部とによ
り構成されたヘリカル型吸気ポートにおいて、上記入口
通路部から分岐された分岐路の出口開口を該渦巻部の渦
巻終端部に連通せしめ、該出口開口を渦巻部の上壁面に
沿う旋回流に対向するように渦巻部側壁面の上端部に形
成すると共に該出口開口の上端縁を渦巻部上壁面に面一
に連結せしめ、該分岐路内に該分岐路の開閉制御をする
油圧駆動の摺動弁を挿入し、該摺動弁の作動油圧室を吸
入空気量に応動する切換弁を介して油圧源に接続して吸
入空気量が所定量以上のときに該摺動弁を開弁するよう
にしたヘリカル型吸気ポートの流路制御装置。
1. In a helical intake port configured with a spiral portion formed around the intake valve and an inlet passage portion connected tangentially to the spiral portion and extending almost straight, a branch branched from the inlet passage portion. The outlet opening of the passage is communicated with the spiral terminal end of the spiral portion, and the exit opening is formed at the upper end of the side wall surface of the spiral portion so as to oppose the swirling flow along the upper wall surface of the spiral portion, and the upper end of the exit opening The edge is connected flush to the upper wall surface of the spiral part, a hydraulically driven sliding valve for controlling the opening and closing of the branching passage is inserted into the branching passage, and the operating hydraulic chamber of the sliding valve is adjusted in response to the amount of intake air. A flow path control device for a helical intake port, which is connected to a hydraulic power source via a switching valve that opens the sliding valve when the amount of intake air exceeds a predetermined amount.
JP56122408A 1981-08-06 1981-08-06 Flow path control device for helical intake port Expired JPS6035540B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP56122408A JPS6035540B2 (en) 1981-08-06 1981-08-06 Flow path control device for helical intake port

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP56122408A JPS6035540B2 (en) 1981-08-06 1981-08-06 Flow path control device for helical intake port

Publications (2)

Publication Number Publication Date
JPS5823228A JPS5823228A (en) 1983-02-10
JPS6035540B2 true JPS6035540B2 (en) 1985-08-15

Family

ID=14835057

Family Applications (1)

Application Number Title Priority Date Filing Date
JP56122408A Expired JPS6035540B2 (en) 1981-08-06 1981-08-06 Flow path control device for helical intake port

Country Status (1)

Country Link
JP (1) JPS6035540B2 (en)

Also Published As

Publication number Publication date
JPS5823228A (en) 1983-02-10

Similar Documents

Publication Publication Date Title
US4269360A (en) Fuel injection nozzle
US4466395A (en) Flow control device of a helically-shaped intake port
KR960041683A (en) Structure of intake system of internal combustion engine and method of manufacturing intake passage of internal combustion engine
JPS6035535B2 (en) Flow path control device for helical intake port
JP2004084670A (en) Valve operated by water pressure
US3859970A (en) Engine retarder brake
US5558061A (en) Engine cylinder intake port
US4467749A (en) Flow control device of a helically-shaped intake port
EP0514854B1 (en) An intake air control device for an internal combustion engine
JPS6035539B2 (en) Flow path control device for helical intake port
JPH0670371B2 (en) Multi-cylinder engine intake system
US5179917A (en) Intake air control device for an internal combustion engine
JPS6023468Y2 (en) Flow path control device for helical intake port
JPS6026183Y2 (en) Flow path control device for helical intake port
JPS6026184Y2 (en) Flow path control device for helical intake port
JPS6017928B2 (en) Flow path control device for helical intake boat
JPS6022171B2 (en) Flow path control device for helical intake port
US4467750A (en) Flow control device of a helically-shaped intake port
JP2009103117A (en) Engine blow-by gas returning apparatus
US20040065285A1 (en) Variable engine valve actuator
JPS5823228A (en) Passage control device of helical type suction port
JPS6323546Y2 (en)
US4466396A (en) Flow control device of a helically-shaped intake port
JPS609378Y2 (en) Flow path control device for helical intake port
JPS6226589Y2 (en)