JPS63111233A - Suction air inertia increasing device for internal combustion engine - Google Patents

Suction air inertia increasing device for internal combustion engine

Info

Publication number
JPS63111233A
JPS63111233A JP61257007A JP25700786A JPS63111233A JP S63111233 A JPS63111233 A JP S63111233A JP 61257007 A JP61257007 A JP 61257007A JP 25700786 A JP25700786 A JP 25700786A JP S63111233 A JPS63111233 A JP S63111233A
Authority
JP
Japan
Prior art keywords
intake
branch pipes
inertial
internal combustion
combustion engine
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP61257007A
Other languages
Japanese (ja)
Other versions
JPH0694813B2 (en
Inventor
Nobuji Eguchi
江口 展司
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.)
Hino Motors Ltd
Original Assignee
Hino Motors Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hino Motors Ltd filed Critical Hino Motors Ltd
Priority to JP61257007A priority Critical patent/JPH0694813B2/en
Publication of JPS63111233A publication Critical patent/JPS63111233A/en
Publication of JPH0694813B2 publication Critical patent/JPH0694813B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B27/00Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues
    • F02B27/001Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues the system having electrically controlled acoustic pulse generating devices, e.g. loudspeakers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B27/00Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues
    • F02B27/008Resonance charging
    • 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
    • F02M35/10006Air intakes; Induction systems characterised by the position of elements of the air intake system in direction of the air intake flow, i.e. between ambient air inlet and supply to the combustion chamber
    • F02M35/10026Plenum chambers
    • F02M35/10045Multiple plenum chambers; Plenum chambers having inner separation walls
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B3/00Engines characterised by air compression and subsequent fuel addition
    • F02B3/06Engines characterised by air compression and subsequent fuel addition with compression ignition
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Landscapes

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

Abstract

PURPOSE:To increase the volume efficiency of intake air and to improve an output, by a method wherein an acoustic pulse generating device is situated in the suction passage (branch pipe) of each cylinder, and based on a pressure pulse signal from a fuel feed pipe, control is made. CONSTITUTION:A suction passage 2 of a multicylinder diesel engine 1 contains branch pipes 6 (61-66) situated to each of cylinders 51-56. Regarding the branch pipes 6 of cylinders, the piston cycles of which are identical to each other, of the branch pipes 6, the upper streams of the branch pipes 61-63 of a first cylinder group A are collected to a first manifold 8a, and the upper streams of the branch pipes 64-66 of a second cylinder group B are collected to a second manifold 8b. The upper streams of the manifolds 8a and 8b are connected to a suction main pipe 9 through branch pipes 10a and 10b. An acoustic pulse generating device 12 is connected to each of the branch pipes 6, and the device 12 is controlled by a control device 15 according to a signal based on a pressure pulse from a fuel feed pipe 14 connected to a fuel injection nozzle 13.

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は、内燃機関の慣性過給装置に関し、更に詳しく
は吸気の慣性効果を増大させ、吸気の体積効率をいっそ
う向上させた内燃機関の吸気慣性増大装置に関する。
Detailed Description of the Invention (Industrial Field of Application) The present invention relates to an inertial supercharging device for an internal combustion engine, and more particularly to an inertial supercharging device for an internal combustion engine that increases the inertial effect of intake air and further improves the volumetric efficiency of intake air. The present invention relates to an intake inertia increasing device.

(従来の技fJ) 内燃機関では、吸気弁の開閉により、吸気通路の吸気が
圧力振動である吸気慣性波となって流れている。この吸
気慣性波を利用して吸気の体積効率を増大し、出力を向
上させるものが慣性過給装置である。
(Prior Art fJ) In an internal combustion engine, intake air in an intake passage flows as intake inertia waves, which are pressure vibrations, by opening and closing an intake valve. An inertial supercharging device uses this intake inertial wave to increase the volumetric efficiency of intake air and improve output.

吸気行程におけるピストンの吸入作用により吸気ポート
に発生した負圧は、吸気通路を負圧波として伝わり、吸
気通路の開放端で反射され、正圧波となって吸気ポート
に向けて返ってくる。
Negative pressure generated in the intake port by the suction action of the piston during the intake stroke is transmitted through the intake passage as a negative pressure wave, reflected at the open end of the intake passage, and returned to the intake port as a positive pressure wave.

これら正負の圧力波の合成により圧力振動が生じる。Pressure oscillations occur due to the combination of these positive and negative pressure waves.

このように吸気行程において吸気通路に発生した圧力振
動が吸気行程に与える影響には、慣性効果と脈動効果が
ある。慣性効果は、同一の吸気行程に圧力振動が影響を
与える場合をいう。
The influence of the pressure vibration generated in the intake passage during the intake stroke on the intake stroke includes an inertial effect and a pulsation effect. Inertia effect refers to the case where pressure oscillations affect the same intake stroke.

又、脈動効果は、ある吸気行程で発生した圧力振動が次
のサイクルの吸気イブ程に影響を与える場合をいう。慣
性効果及び脈動効果を含む吸気通路における圧力振動を
、本願では吸気慣性波というものとする。
Furthermore, the pulsation effect refers to a case where pressure vibrations generated in a certain intake stroke affect the intake stroke of the next cycle. In this application, pressure vibrations in the intake passage including inertial effects and pulsation effects are referred to as intake inertial waves.

吸気慣性波の固有振動数は、吸気通路の長さや断面積な
どにより定まる。そこで、吸気慣性波の固有振動数が吸
気弁の開閉タイミングとマツチング(同3!りするよう
に吸気通路の長さ、断面積などを設計する。これにより
、吸気弁の閉鎖直前に吸気ポートでの吸気慣性波が正圧
となるようにし、吸気の体積効率を向上させたものが慣
性過給装置である。
The natural frequency of the intake inertial wave is determined by the length and cross-sectional area of the intake passage. Therefore, the length and cross-sectional area of the intake passage are designed so that the natural frequency of the intake inertial wave matches the opening/closing timing of the intake valve. An inertial supercharging device improves the volumetric efficiency of intake air by making the intake inertial waves of the engine have a positive pressure.

(発明が解決しようとする問題点) しかし、従来は、吸気通路の仕様により定まる吸気慣性
波の振幅をそれ以上積極的に増幅して体積効率をいりそ
う向上させる思想はなかった。
(Problems to be Solved by the Invention) However, conventionally, there has been no idea of actively amplifying the amplitude of the intake inertial wave determined by the specifications of the intake passage to significantly improve the volumetric efficiency.

本発明の目的は、内燃機関の慣性過給装置において、吸
気通路の吸気慣性波を増幅させることにより、吸気の体
積効率をいっそう向上させた内燃機関の吸気慣性増大装
置を提供することにある。
An object of the present invention is to provide an intake inertia increasing device for an internal combustion engine that further improves the volumetric efficiency of intake air by amplifying intake inertia waves in an intake passage in an inertial supercharging device for an internal combustion engine.

(問題点を解決するための手段) 本発明は、吸気通路内に音響パルスを送る音響パルス発
生装置が設けられ、燃料噴射ノズルに燃料を供給する燃
料供給管の燃料の圧カノクルスを圧力信号とし、これを
電気信号に変換して、前記音響パルス発生装置を作動さ
せる制御装置が設けられている。
(Means for Solving the Problems) The present invention is provided with an acoustic pulse generator that sends acoustic pulses into the intake passage, and uses the fuel pressure canoculus of the fuel supply pipe that supplies fuel to the fuel injection nozzle as a pressure signal. , a control device is provided that converts this into an electrical signal and operates the acoustic pulse generator.

(実施例) 以下、図を参照して説明する。(Example) This will be explained below with reference to the drawings.

内燃機関1(以下に、機関と略称する)として、多気筒
のディーゼル機関を示す。本実施例では6気筒であるが
、気筒数はこれに限定されない。
A multi-cylinder diesel engine is shown as an internal combustion engine 1 (hereinafter abbreviated as engine). In this embodiment, there are six cylinders, but the number of cylinders is not limited to this.

機関1は、吸気通路2、吸気ポート3、吸気弁4及びシ
リング5などから成る吸気系統を有している。
The engine 1 has an intake system including an intake passage 2, an intake port 3, an intake valve 4, a sill 5, and the like.

吸気通路2は、次のように構成されている。The intake passage 2 is configured as follows.

各シリング51ないし56に、分岐管61ないし66が
設けられている。シリングのうちシリング51と56の
組、52と55の組、5コと5.の組は、それぞれピス
トン7のサイクルが同一である。
Each sill 51-56 is provided with a branch pipe 61-66. Of the shillings, shillings 51 and 56, 52 and 55, 5 and 5. The cycles of the pistons 7 in each set are the same.

シリング51.5□、5.から第1のシリング群Aがな
る。シリンダA群に対応する分岐管6、ないし63の上
流は、第1のマニホールド8aに集合されている。
Schilling 51.5□, 5. becomes the first shilling group A. Upstream portions of the branch pipes 6 to 63 corresponding to the cylinder A group are collected in a first manifold 8a.

又、シリング54.51.56がら!@2のシリング群
Bがなる。シリング8群に対応する分岐’f? 63 
tいし66の上流は、第2のマニホールド8bに集合さ
れている。
Also, 54.51.56 shillings! Schilling group B of @2 becomes. Branch 'f? corresponding to Schilling 8 group? 63
The upstream side of the t-shape 66 is assembled into the second manifold 8b.

第1のマニホールド8a、lびj@2のマニホールド8
bの上流は、それぞれブランチ通路10a110bを介
して1本の吸気率W9に対して二叉に分岐されて接続さ
れている。吸気本管9は図示しないエアクリーナに接続
されている。
First manifold 8a, lj@2 manifold 8
The upstream side of b is branched into two and connected to one intake rate W9 via branch passages 10a and 110b, respectively. The intake main pipe 9 is connected to an air cleaner (not shown).

これら分岐管6、マニホールド8、ブランチ通路10及
び吸気率y9の長さ、断面積などにより吸気慣性波の周
波数が決定され、機関1のある同調回伝数において吸気
弁の開閉速度とマツチングし、吸気弁4の閉鎖直前に吸
気ポート3での吸気慣性波が正圧となる。
The frequency of the intake inertial wave is determined by the length and cross-sectional area of the branch pipe 6, manifold 8, branch passage 10, intake rate y9, etc., and is matched with the opening/closing speed of the intake valve at a certain tuning frequency of the engine 1. Immediately before the intake valve 4 closes, the intake inertia wave at the intake port 3 becomes a positive pressure.

各分岐管6.ないし66にはそれぞれパルス管11、な
いし116が設けられ、その端部にはそれぞれ音響パル
ス発生装置12が設けられている。音響パルス発生器1
2は、電磁気的振動を利用したスピーカであり、パルス
管11を介して分岐管6内に音響パルスを送るものであ
る。
Each branch pipe6. A pulse tube 11 or 116 is provided in each of the channels 66, and an acoustic pulse generator 12 is provided at each end thereof. Acoustic pulse generator 1
Reference numeral 2 denotes a speaker that uses electromagnetic vibration, and sends acoustic pulses into the branch pipe 6 via the pulse tube 11.

吸気慣性波と音響パルスが共鳴するためには、音響パル
スの周波数f1が、分岐f6の吸気慣性波の周波数f2
と次の関係にあることを要する。
In order for the intake inertial wave and the acoustic pulse to resonate, the frequency f1 of the acoustic pulse must be equal to the frequency f2 of the intake inertial wave of the branch f6.
The following relationship is required.

L=f2n(nは大数) 音響パルスの周波数をflとするため、燃料供給の圧力
パルス数と時間当たり同数の音響パルスを発生させるよ
うにしている。
L=f2n (n is a large number) In order to set the frequency of the acoustic pulse to fl, the same number of acoustic pulses are generated per time as the number of pressure pulses for fuel supply.

燃料噴射7ズル13の時間当たり噴射数と吸気弁4の時
間当たり開閉数は同じである。一方、慣性過給の同調回
転数時における吸気慣性波の周波数は吸気弁4の時間当
たりrfA閉数と同じである。従って、燃料供給の圧力
パルス数は吸気慣性波の周波数と同じであり、これと同
数の音響パルスを発生させれば、吸気慣性波と共鳴する
ことになる。
The number of injections per hour of the fuel injection valve 13 and the number of openings and closings of the intake valve 4 per hour are the same. On the other hand, the frequency of the intake inertial wave at the synchronized rotational speed of inertia supercharging is the same as the number of rfA closings of the intake valve 4 per hour. Therefore, the number of pressure pulses for fuel supply is the same as the frequency of the intake inertial wave, and if the same number of acoustic pulses is generated, it will resonate with the intake inertial wave.

このため、次のように構成されている。燃料噴射ノズル
13と図示しない燃料噴射ポンプが、燃料供給?714
により接続されている。この燃料供給管14における燃
料の圧力パルスを圧力信号とし、それを電気信号に変換
し、処理する制御装置15が設けられている。燃料供給
の圧カバルスと時間当たり同数又はn倍数の周波数の音
響パルスを音響パルス発生装置12に発生させる。
For this reason, it is configured as follows. Does the fuel injection nozzle 13 and a fuel injection pump (not shown) supply fuel? 714
connected by. A control device 15 is provided which converts the pressure pulse of the fuel in the fuel supply pipe 14 into a pressure signal, converts it into an electric signal, and processes it. The acoustic pulse generator 12 generates acoustic pulses having a frequency equal to or n times the frequency of the fuel supply pressure caballus per hour.

ただし、燃料供給管14における燃料の圧力パルスと吸
気慣性波は時間的ずれにより位相が異なるから、制御装
置15により位相をずらして一致させる。
However, since the pressure pulse of the fuel in the fuel supply pipe 14 and the intake inertia wave have different phases due to a time lag, the control device 15 shifts the phases to match them.

制御装置15は、燃料の圧力信号を電気信号に変換する
センサ部、フィルタ回路、吸気慣性波と同位相にする回
路及び増幅回路などを備乏ている。
The control device 15 is equipped with a sensor unit that converts a fuel pressure signal into an electrical signal, a filter circuit, a circuit that makes the phase in phase with the intake inertial wave, an amplifier circuit, and the like.

16は、音響パルス発生装置12を作動させる電源であ
る。
16 is a power source that operates the acoustic pulse generator 12.

上記のように構成された本実施例は、次のように作用す
る。
This embodiment configured as described above operates as follows.

吸気弁4の開閉により、吸気通路2では吸気慣性波とな
って流れている。この吸気慣性波は、ある同調回転数に
おいて吸気弁4の開閉速度と同調し、吸気弁4の閉鎖直
前に吸気ポート3で正圧となる。
Due to the opening and closing of the intake valve 4, intake inertia waves flow in the intake passage 2. This intake inertial wave synchronizes with the opening/closing speed of the intake valve 4 at a certain synchronized rotational speed, and becomes a positive pressure at the intake port 3 immediately before the intake valve 4 closes.

一方、燃料供給管14における燃料の圧力信号が制御装
置15により電気信号に変換され1、燃料供給の圧力パ
ルスと同数(又はn倍数)且つ同位相の音響パルスを音
響パルス発生器12に発生させる。
On the other hand, the fuel pressure signal in the fuel supply pipe 14 is converted into an electric signal by the control device 15, and the acoustic pulse generator 12 generates acoustic pulses having the same number (or n times) and phase as the fuel supply pressure pulses. .

この音響パルスと各分岐管6.ないし66において吸気
慣性波は、重畳、共鳴する。重畳吸気慣性波は増幅され
るので、吸気の体積効率はいっそう向上したものとなる
This acoustic pulse and each branch pipe 6. At 66, the intake inertial waves are superimposed and resonate. Since the superimposed intake inertial waves are amplified, the volumetric efficiency of intake air is further improved.

尚、上記実施例に本発明が限定されることはない。例え
ば、パルス管11は、各分岐管に設けられる他、ブラン
チ部10など吸気通路にもうけられていればよい。
Note that the present invention is not limited to the above embodiments. For example, the pulse tube 11 may be provided in each branch pipe or in an intake passage such as the branch portion 10.

(発明の効果) 本発明は、制御装置により燃料噴射の圧力信号を電気信
号に変換し、音響パルス発生装置に吸気慣性波と共鳴す
る周波数の音響パルスを発生させる。
(Effects of the Invention) According to the present invention, a control device converts a fuel injection pressure signal into an electric signal, and causes an acoustic pulse generator to generate an acoustic pulse having a frequency that resonates with an intake inertial wave.

従って、吸気慣性波を強制増幅させることにより、吸気
の体積効率をいっそう向上させ、出力を増大させること
ができる。
Therefore, by forcibly amplifying the intake inertial waves, the volumetric efficiency of intake air can be further improved and the output can be increased.

又、燃料噴射の圧力パルスを圧力信号を電気信号に変換
し、音響パルスを吸気慣性波と共鳴する周波数とするの
で、音響パルスと吸気慣性波の共鳴が確実に行なわれる
ことになる。
Further, since the pressure pulse of fuel injection is converted into an electric signal and the acoustic pulse is set to a frequency that resonates with the intake inertial wave, resonance between the acoustic pulse and the intake inertial wave is ensured.

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

第1図は、本発明の一実施例を示す正面図である。 第2図は、第1図の吸気系統を示す概略図である。 1:内燃機関 2:吸気通路 3:吸気ポート4:吸気
弁 5ニジリング 11:パルス管12:音響パルス発
生器 13:燃料噴射ノズル14:燃料供給管 15:
制御装置 16:電源
FIG. 1 is a front view showing one embodiment of the present invention. FIG. 2 is a schematic diagram showing the intake system of FIG. 1. 1: Internal combustion engine 2: Intake passage 3: Intake port 4: Intake valve 5 Niji ring 11: Pulse tube 12: Acoustic pulse generator 13: Fuel injection nozzle 14: Fuel supply pipe 15:
Control device 16: power supply

Claims (1)

【特許請求の範囲】 吸気弁の閉鎖直前に吸気ポートでの吸気慣性波が正圧と
なるようにして吸気の体積効率を向上させる内燃機関の
慣性過給装置において、前記吸気通路に音響パルスを送
る音響パルス発生装置と、 燃料噴射ノズルに燃料を供給する燃料供給管の圧力パル
スを圧力信号とし、これを電気信号に変換して前記音響
パルスを作動させる制御装置とを備えて成り、吸気慣性
波と音響パルスを共鳴させることを特徴とする内燃機関
の吸気慣性増大装置。
[Claims] In an inertial supercharging device for an internal combustion engine that improves the volumetric efficiency of intake air by making an intake inertial wave at an intake port become a positive pressure immediately before closing an intake valve, an acoustic pulse is applied to the intake passage. A control device that converts the pressure pulse of the fuel supply pipe that supplies fuel to the fuel injection nozzle into a pressure signal and converts it into an electric signal to operate the acoustic pulse. An intake inertia increasing device for an internal combustion engine characterized by resonating waves and acoustic pulses.
JP61257007A 1986-10-30 1986-10-30 Device for increasing intake inertia of internal combustion engine Expired - Lifetime JPH0694813B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP61257007A JPH0694813B2 (en) 1986-10-30 1986-10-30 Device for increasing intake inertia of internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP61257007A JPH0694813B2 (en) 1986-10-30 1986-10-30 Device for increasing intake inertia of internal combustion engine

Publications (2)

Publication Number Publication Date
JPS63111233A true JPS63111233A (en) 1988-05-16
JPH0694813B2 JPH0694813B2 (en) 1994-11-24

Family

ID=17300425

Family Applications (1)

Application Number Title Priority Date Filing Date
JP61257007A Expired - Lifetime JPH0694813B2 (en) 1986-10-30 1986-10-30 Device for increasing intake inertia of internal combustion engine

Country Status (1)

Country Link
JP (1) JPH0694813B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0492787A1 (en) * 1990-12-24 1992-07-01 Ford Motor Company Limited Electronically tuned intake manifold

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0492787A1 (en) * 1990-12-24 1992-07-01 Ford Motor Company Limited Electronically tuned intake manifold

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JPH0694813B2 (en) 1994-11-24

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