JPS5970835A - Intake device of rotary piston engine - Google Patents

Intake device of rotary piston engine

Info

Publication number
JPS5970835A
JPS5970835A JP57181964A JP18196482A JPS5970835A JP S5970835 A JPS5970835 A JP S5970835A JP 57181964 A JP57181964 A JP 57181964A JP 18196482 A JP18196482 A JP 18196482A JP S5970835 A JPS5970835 A JP S5970835A
Authority
JP
Japan
Prior art keywords
intake
cylinder
engine
passage
compression wave
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
JP57181964A
Other languages
Japanese (ja)
Other versions
JPS619492B2 (en
Inventor
Haruo Okimoto
沖本 晴男
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.)
Mazda Motor Corp
Original Assignee
Mazda Motor Corp
Toyo Kogyo Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mazda Motor Corp, Toyo Kogyo Co Ltd filed Critical Mazda Motor Corp
Priority to JP57181964A priority Critical patent/JPS5970835A/en
Publication of JPS5970835A publication Critical patent/JPS5970835A/en
Publication of JPS619492B2 publication Critical patent/JPS619492B2/ja
Granted 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
    • F02B53/00Internal-combustion aspects of rotary-piston or oscillating-piston engines
    • F02B53/04Charge admission or combustion-gas discharge
    • F02B53/08Charging, e.g. by means of rotary-piston pump
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B53/00Internal-combustion aspects of rotary-piston or oscillating-piston engines
    • F02B2053/005Wankel engines
    • 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)
  • Characterised By The Charging Evacuation (AREA)

Abstract

PURPOSE:To improve the output of an engine throughout from its medium speed range to high speed range, by obtaining a supercharge effect due to the exhaust interference mutually between cylinders at high speed operation of the engine while a supercharge effect due to the inertia pulsation of each cylinder itself at medium speed operation of the engine, in the case of a two-cylinder engine of side intake port type. CONSTITUTION:At high speed operation of an engine, a compression wave, generated in, for instance, a passage 16b when an intake port 3 in a cylinder 1B is opened, is propagated to an intake port 3 immediately before full closing with a 180 deg. phase difference in a cylinder 1A by setting a passage in an adequate length between the intake ports 3, 3, and a supercharge is operated. Similarly thereafter, an output of the engine is increased by an exhaust interference effect mutually between the cylinders 1A, 1B. While a compression wave, generated in passages 16a, 16b at closing, causes inversion and reflection with expansion and compression by setting the length of a passage between each intake port 3 and an expansion chamber 21 with the reference at medium speed time, and is propagated as a secondary pulsating compression wave to the next intake port 3 immediately after opening, thus an output at the medium speed time can be improved by a supercharging effect due to the inertia pulsation of each cylinder itself.

Description

【発明の詳細な説明】 本発明は、ロータリピストンエンジンの吸気装置に関し
、詳しくは勺イド吸気ボート式の2気筒ロータリビス1
〜ンエンジンにおいて、吸気通路内に発生ずる吸気圧力
波、特に吸気ボート開口時および閉l」時に発生覆る圧
縮波を利用してエンジンの中回転時から高回転時に亙っ
て過給効果を1qるようにしたものに関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an intake system for a rotary piston engine, and more specifically, to an intake system for a rotary piston engine.
In engine engines, this technology utilizes the intake pressure waves generated in the intake passage, especially the overlapping compression waves generated when the intake boat is opened and closed, to increase the supercharging effect by 1q from medium to high engine speeds. It relates to something that is made to look like this.

一般に、サイド吸気ボート式の2気筒ロータリビス1−
ンエンジンは、2節トロコイド状の内周面を備えたロー
タハウジングと、その両側に位冒し吸気通路が間口する
吸気ボートを備えたサイドハウジングとで形成されたケ
ーシング内を、略三角形状のロータがエキセントリック
シャフトに支承されてM星回転運動するものであって、
かつ各気筒の1コータがエキセントリックシャフトの回
転角で180°の位相差を持つものであり、両気筒間で
上記180°の位相差を保ちながら各気筒においてロー
タの回転に伴い吸気、圧縮、爆発、膨張および排気の各
行程を順次行うようにしたものである。
In general, side intake boat type two-cylinder rotary vis 1-
The casing engine has a rotor housing with a two-section trochoidal inner circumferential surface, and a side housing with an intake boat with an intake passage opening on both sides. is supported by an eccentric shaft and rotates in an M star,
In addition, one coater in each cylinder has a phase difference of 180° with respect to the rotation angle of the eccentric shaft, and while maintaining the above 180° phase difference between both cylinders, intake, compression, and explosion are performed in each cylinder as the rotor rotates. , expansion and exhaust strokes are performed sequentially.

ところで、従来、このようなロータリピストンエンジン
において、吸気通路に過給機を設けて、力向上を図るこ
とはよく知られているが、過給機装備のために構造が犬
がかりどなるとともにロス1ヘアツブとなる嫌いがあっ
た。
By the way, it is well known that conventionally, in such a rotary piston engine, a supercharger is installed in the intake passage in order to improve the power, but the structure becomes complicated due to the supercharger, and the loss is increased. I had a dislike for it that made me angry.

また、従来、吸気圧力波により過給効果を4qる技術と
して、実公昭/15−2321@公報に開示されている
ように、単一気筒のロータリビス1〜ンエンジンにおい
て、吸気管を\1法の異なる2木の通路に分け、それぞ
れ別の吸気ボートを有し、エンジン高回転時は2本の吸
気通路を用い、低回転時は閉塞位置の遅い方の吸気通路
を閉止し、吸気を早目に閉塞することにより、吸気管の
寸法やコーンジン回転数の関数である吸気の最大圧力時
点での吸気の閉塞による過給作用を利用して広範囲のエ
ンジン回転域に亙って好適な充1眞効率を得るようにし
たものが提案されている。しかし、このものは、中−気
筒のロータリピストンエンジンに対するものであって、
吸気通路内で光生りる吸気圧力波をどのように利用する
のか、その構成1作用が定かでなく、直ちに実用に供し
得ないものであった。しかも、吸気ボートとしてペリボ
ートを用いているため、吸気ボートは吸気作動室が閉じ
る前に排気作動室と連通づることになり、排気作動室か
らの排気ガスの吹き返しにより過給効果を得ることが困
頻であった。特に、近年の市販車では、騒音低減や排気
ガス浄化のためにエンジン排圧が上昇し、高回転高負荷
時通常のエンジンで400〜600mmH(1(ゲージ
圧)程度にターボ過給機付エンジンでは1000 rm
n l−1g以上になっており、上記ベリボート方式に
よる充填効率向上は期待できないものとなっている。
In addition, conventionally, as a technology to increase the supercharging effect by 4Q using intake pressure waves, in a single cylinder rotary rev engine, the intake pipe is It is divided into two passages with different methods, each with a separate intake boat, and when the engine is running at high speeds, the two intake passages are used, and when the engine is running at low rotations, the intake passage that is at the later closing position is closed, and the intake air is blocked. By occluding the air early, optimal charging is achieved over a wide range of engine speeds by utilizing the supercharging effect caused by the occlusion of the intake air at the point of maximum intake pressure, which is a function of the intake pipe dimensions and cone engine speed. A method has been proposed that achieves the highest efficiency. However, this is for a middle-cylinder rotary piston engine,
It was not clear how to utilize the intake pressure waves generated in the intake passage, and the effect of the first structure was not clear, so it could not be put to practical use immediately. Moreover, since a peri-boat is used as the intake boat, the intake boat communicates with the exhaust working chamber before the intake working chamber closes, making it difficult to obtain a supercharging effect due to exhaust gas blowing back from the exhaust working chamber. It was frequent. In particular, in recent years commercially available cars, the engine exhaust pressure has increased to reduce noise and purify exhaust gas, and at high speeds and loads, normal engines have a pressure of 400 to 600 mmH (1 (gauge pressure)), and engines with turbochargers Then 1000 rm
n l-1g or more, and no improvement in filling efficiency can be expected by the VeriBot method.

そこで、本発明者等は、ロータリピストンエンジンにお
けるサイド吸気ボートの吸気特性を検討するに、 (+)  吸気ボート間口時には作動室の残留排気ガス
の圧力によって吸気が圧縮され、吸気通路内の吸気ボー
ト部分に圧縮波が発生すること(i)  吸気ボート閉
口時には吸気の慣性により吸気が圧縮されて吸気通路内
の吸気ボート部分に圧縮波が発生づ”ること を知見した。このことから、一方の気筒で′の上記(+
)の開口性圧縮波を他方の気筒の特に吸気の吹き返しが
生じる全開直前の吸気ボートに作用せしめれば過給効果
が19られることく以下、排気干渉効果という)、およ
び各気筒での上記(11)の開口性圧縮波を2度反転さ
せて2次脈動圧縮波どして該各気筒の特に排気の吹き返
しが生じる次の開口直後の吸気ボー1〜に作用せしめれ
ば“過給効果が得られること(以下、慣性脈動効果とい
う)を児い出したのである。特に、上記排気干渉効果は
、近年、エンジンの排気系に排気浄化用の触媒装置が介
設されて排圧が高くなっている関係上、その効果が顕著
で、出力要求の強いエンジン高負荷高回転時に有効で゛
ある。尚、サイド吸気ボー1〜と異なり、吸気通路がロ
ータハウジングに間口づるべり一7エラル吸気ボートの
場合には、該吸気ボー1〜が常に作動室に開口している
ため、上記排気干渉効果は生じない。
Therefore, when examining the intake characteristics of the side intake boat in a rotary piston engine, the inventors found that (+) When the intake boat is open, the intake air is compressed by the pressure of the residual exhaust gas in the working chamber, and the intake boat in the intake passage is compressed by the pressure of the residual exhaust gas in the working chamber. (i) When the intake boat is closed, the intake air is compressed due to the inertia of the intake air, and compression waves are generated in the intake boat section in the intake passage. Above (+
), the supercharging effect can be obtained by applying the aperture compression wave of the other cylinder, especially to the intake boat just before full opening, where intake air blowback occurs. If the opening compression wave of 11) is reversed twice to create a secondary pulsating compression wave and applied to each cylinder, especially to the intake bow 1 immediately after the next opening where exhaust gas blowback occurs, "supercharging effect" can be achieved. (hereinafter referred to as the inertial pulsation effect).In particular, the above-mentioned exhaust interference effect has been developed in recent years due to the introduction of catalyst devices for exhaust purification in engine exhaust systems, which have increased exhaust pressure. The effect is remarkable and is effective when the engine is under high load and at high rotation speeds with strong output requirements.In addition, unlike the side intake bows 1~, the intake passage is located on the rotor housing. In this case, the intake bow 1~ always opens into the working chamber, so the above-mentioned exhaust interference effect does not occur.

すなわち、本発明の目的は、」上記の如きサイド吸気ボ
ート式の2気筒ロータリピストンエンジンにおいで、吸
気ボートの間口期間、各気筒の吸気通路を連通しかつ閉
1コ時圧縮波を膨張波を経て2次脈動圧縮波に反転する
だめの拡大室の位置、雨気筒の吸気ボート間の通路長さ
、および上記拡大室から各気筒の吸気ボートまでの通路
長さを適切に設定して、5000〜7000 rpni
のエンジン高回転時には排気干渉効果にJ:す、350
0〜5000 rIlmのエンジン中回転時には慣性脈
動効果によりそれぞれ過給を行うようにすることにより
、過給機等を用いることなく既存の吸気系の僅かな設h
1変更による極めて簡単な構成でもってエンジンの中回
転時から高回転時に亙って充填効率を高めで出力向上を
図らんとするものである。
That is, an object of the present invention is to provide a side intake boat type two-cylinder rotary piston engine as described above, to connect the intake passages of each cylinder during the intake boat frontage period, and to convert the compression wave to the expansion wave when the engine is closed. By appropriately setting the position of the expansion chamber of the reservoir which then reverses into a secondary pulsating compression wave, the passage length between the intake boats of the rain cylinder, and the passage length from the expansion chamber to the intake boat of each cylinder, the 5000 ~7000 rpni
When the engine speed is high, the exhaust interference effect occurs.
By performing supercharging using the inertial pulsation effect during engine rotations of 0 to 5000 rIlm, the existing intake system can be easily configured without using a supercharger or the like.
This is an extremely simple configuration with one change, and aims to increase the charging efficiency and improve the output from medium to high engine speeds.

この目的を達成りるため、本発明の構成は、2節1−ロ
]イド状の内周面を備えたロータハウジングと、その両
側に位置し吸気通路が間口する吸気ボートを備えた1ノ
イドハウジングとで形成されたケーシング内を、略三角
形状のロータがエキセントリックシャフトに支承されて
遊星回転運動するものひあって、各1」−夕がエキセン
トリックシャフトの回転角で180°の位相差を持つ2
気筒ロータリピストンエンジンにおいて、 a、吸気ボー1への間口期間θをエキセン1〜リツクシ
1フフ[−の回転角で270〜320°の範囲に設定づ
゛ること、 b、各気筒の吸気通路をスロツ1−ルバルブ下流におい
(連通J8連通路を右づる拡大室を設りること、 C6該連通路おにびぞの下流の吸気通路ににつで形成さ
れる両気筒の吸気ボート間の通路長さしを0.57〜1
.37mになるように設定づること d、上記拡大室から各気筒の吸気ボートまでの吸気通路
の通路長さ91を0.17へ、Q、15mになるように
設定すること の条件のもとで、5000〜7000ppmのエンジン
高回転時、一方の気筒の吸気ポート間口時に吸気通路内
に発生する圧縮波を上記連通路を介して他方の気筒の全
開直前の吸気ボートに伝播さVて過給を行う一方、30
00〜5000 ppmのエンジン中回転時、各気筒の
吸気ポート閉口時に吸気通路内に発生ずる圧縮波を上記
拡大室で2度反転した2次脈動圧縮波を該各気筒の間口
直後の吸気ボー1〜に伝播させて過給を行うようにした
もので、よってエンジン高回転時での気筒相互間の排気
干渉効果およびエンジン中回転時での各気筒自身の慣性
脈動効果によりエンジンの中回転域から高回転域に亙る
広範囲において充填効率を高めるようにしたものである
In order to achieve this object, the configuration of the present invention is to provide a rotor housing having a two-node rotor housing and an intake boat having an intake passage located on both sides of the rotor housing. A substantially triangular rotor is supported by an eccentric shaft and performs planetary rotation within the casing formed by the housing, so that each 1" and 1" angle has a phase difference of 180° with respect to the rotation angle of the eccentric shaft. 2
In a cylinder rotary piston engine, a. The frontage period θ to the intake bow 1 is set in the range of 270 to 320 degrees at the rotation angle of the eccentric 1 to the cylinder 1 fufu [-. b. The intake passage of each cylinder is set. downstream of the throttle valve (connection J8 An enlarged chamber extending to the right of the communication passage is provided; C6 the passage length between the intake boats of both cylinders formed in the intake passage downstream of the communication passage) Sashio 0.57~1
.. Under the conditions that d is set to be 37 m, the length 91 of the intake passage from the expansion chamber to the intake boat of each cylinder is set to 0.17, and Q is set to 15 m. When the engine is running at a high speed of 5,000 to 7,000 ppm, the compression wave generated in the intake passage when the intake port of one cylinder is opened is propagated through the communication passage to the intake boat of the other cylinder just before it is fully opened, thereby generating supercharging. while doing 30
During medium rotation of the engine at 00 to 5000 ppm, the compression wave generated in the intake passage when the intake port of each cylinder is closed is reversed twice in the expansion chamber, and a secondary pulsating compression wave is generated at the intake bow 1 immediately after the frontage of each cylinder. Therefore, the exhaust interference effect between cylinders at high engine speeds and the inertial pulsation effect of each cylinder itself at medium engine speeds cause supercharging to be carried out from the mid-speed range of the engine. This is designed to increase charging efficiency over a wide range of high rotational speeds.

ここにおいて、上記排気干渉効果を得るエンジン高回転
時としての5000〜7000 ppmの限定は、一般
に最高出力および最高速度がこの範囲に設定されている
ことから、エンジンの高負荷高回転運転領域であって、
顕箸な過給効果の発揮による充填効率向上、出力向上に
有効な領域であることによるものである。また、上記慣
性脈動効果を得るエンジン中回転時としての3500〜
5゜O,Orpmの限定は、慣性脈動効果をエンジンの
中回転域に発揮させるよう設定すると高回転域での脈動
波の谷く1次脈動膨張波)が生じて上記排気干渉効果を
損うことから、この谷が上記エンジン高回転時としての
700 Orpm以上で生じるように設定するためには
下限が350 Orpm以上となることによるのである
Here, the limitation of 5,000 to 7,000 ppm at high engine speed to obtain the above-mentioned exhaust interference effect does not apply to the engine's high-load, high-speed operation range, since the maximum output and maximum speed are generally set within this range. hand,
This is because it is an effective area for improving charging efficiency and output by exerting a significant supercharging effect. In addition, 3,500 to 3,500 at engine medium rotation to obtain the above-mentioned inertial pulsation effect.
The limitation of 5°O, Orpm is that if it is set so that the inertial pulsation effect is exerted in the engine's medium rotation range, a trough of the pulsation wave (first-order pulsation expansion wave) will occur in the high rotation range, impairing the above exhaust interference effect. Therefore, in order to set the valley so that it occurs at 700 Orpm or more, which is the time when the engine is at high speed, the lower limit must be 350 Orpm or more.

また、上記設定事項aての吸気ボー1−間口期間θの上
限である320°は、ナイド吸気ボー1〜を介して先行
作動室と後続作動室が連通するのを防止するためで、ロ
ータ側面による実質的な開口期間よりナイドシールによ
る開口期間は約40°大きくなり、このサイドシール開
口期間のラップを避けるために間に40°以上の間隔を
設ける必要がある。これ以下に開口期間を抑さえること
にJ:す、ナイドシール外側のサイドハウジング内摺面
とロータ側面との間の微少間隙〈通常200μ程度)を
介しての吸気作動室とそれに続< 471気作動室との
連通を防止し、アイドリングのような低回転低負荷時に
おける排気ガスの吸気作動室への持ちこみを防止し安定
した燃焼を確保するものである。一方、その下限である
270°は、吸入上死点(TDC)から下死点(BDC
)までの幾何学的な吸気行程の最低期間であり、吸気を
効果的に行うためには、少なくとも開[1期間をこれ以
上に設定する必要がある。
In addition, the upper limit of the intake bow 1-frontage period θ in the above setting item a, 320°, is to prevent the preceding working chamber from communicating with the succeeding working chamber via the nide intake bow 1. The opening period due to the side seal is approximately 40° longer than the actual opening period due to the side seal opening period, and it is necessary to provide an interval of 40° or more between the side seal opening periods to avoid overlap. In order to suppress the opening period to less than this, the intake working chamber is connected to the intake working chamber through a minute gap (usually about 200μ) between the inner sliding surface of the side housing on the outside of the nide seal and the rotor side. This prevents communication with the intake chamber and prevents exhaust gas from being carried into the intake working chamber during low rotation and low load conditions such as idling, thereby ensuring stable combustion. On the other hand, the lower limit of 270° is from top dead center (TDC) to bottom dead center (BDC).
This is the minimum period of the geometrical intake stroke up to ), and in order to effectively perform intake, it is necessary to set at least one period longer than this.

尚、本発明の吸気ボートの開口期間はロータ側面ににる
吸気ボートの実質的な開閉期間であって、勺イドシール
によるものではない。これは、本発明で問題とする高い
回転域における有効な、圧力波の発生伝播に関しては、
サイドシール外側の微少間隙は実質的に影響を及ぼさな
いためである。
Incidentally, the opening period of the intake boat of the present invention is the substantial opening/closing period of the intake boat on the side surface of the rotor, and is not due to the intake seal. This means that regarding the effective generation and propagation of pressure waves in the high rotation range that is the problem of the present invention,
This is because the minute gap outside the side seal has no substantial effect.

また、上記設定事項すでの連通路を有Jる拡大室のスロ
ットルバルブ下流位置設定は、スロットルバルブの存在
が圧力波(圧縮波および膨張波)の伝播の抵抗となるの
でそれを避【ブるためであり、圧力波をその減衰を小さ
くして有効に伝播させるためである。
In addition, the downstream position of the throttle valve in the expansion chamber that has the communication path as described above is important because the presence of the throttle valve acts as a resistance to the propagation of pressure waves (compression waves and expansion waves), so it is necessary to avoid it. This is to reduce the attenuation of pressure waves and propagate them effectively.

さらに、上記設定事項Cでの内気筒の吸気ボート間の通
路長さしは、排気干渉効果を得るように設定されたもの
で、 L=(θ−゛180−00) X (60/36ON)Xc   ・・・(I)の式か
ら求められた値Cある。すなわら、上記式において、θ
は吸気ボー1−開口期間でθ−270〜32o°であり
、180°は内気局間の位相差であり、またθ0は無効
期間であって、吸気ボート間口から圧縮波が実質的に発
生ザるまでの期間と効果的に過給を行うために該間口圧
縮波を伝播させる吸気ボート全閉直前の時期から全開ま
での期間とを合算したもので約20°である。よって〈
θ−180−〇〇)は一方の吸気ボートでの圧縮波発生
から他方の吸気ボートへの伝播までに要づ゛るエキセン
トリックシャフトの回転角度を表わづ。また、Nはエン
ジン回転数でN=5000〜7000 rpmであり、
60 / 360 Nは1°回転するのに要する時間(
秒)を表わす。また、Cは圧縮波の伝播速!1m(音速
)であって、20℃rc=343m/S℃ある。これら
の値から、L=0゜57〜1.37mどなる。
Furthermore, the length of the passage between the intake boats of the inner cylinder in the above setting C is set to obtain the exhaust interference effect, L = (θ-゛180-00) X (60/36ON) Xc...There is a value C obtained from the formula (I). That is, in the above formula, θ
is the intake bow 1-opening period, θ-270 to 32o, 180° is the phase difference between internal air stations, and θ0 is the invalid period, during which compression waves are substantially generated from the intake boat opening. This is approximately 20°, which is the sum of the period from the time immediately before the intake boat is fully closed to the time when the intake boat is fully opened, during which the frontage compression wave is propagated in order to effectively perform supercharging. Therefore,
θ-180-〇〇) represents the rotation angle of the eccentric shaft required from generation of compression waves in one intake boat to propagation to the other intake boat. In addition, N is the engine rotation speed, N = 5000 to 7000 rpm,
60 / 360 N is the time required to rotate 1 degree (
seconds). Also, C is the propagation speed of compression waves! 1 m (sound speed) and 20°Crc = 343m/S°C. From these values, L=0°57~1.37m.

さらにまた、上記設定事項dでの拡大室と各気筒の吸気
ボートとの間の通路長さρ1は、慣性脈動効果を得るよ
うに設定されたもので、1+、=(360−θ+61 
) X60/36ONXc X 1/22− (II)の式
から求められた値である。すなわち、上記式に83いて
、36o°は吸気行程の間隔であり、吸気ボート開口期
間θ−270〜320′であり、!: 7jθ1は閉口
時圧縮波が発生してがら吸気ボート全閉までの期間と吸
気ボート開口から2次脈動圧縮波が伝播されるまでの期
間とを台枠した無効期間であって、サイド吸気θ+ 央
20’であり、よって(360−θ+θ1)は閉口時圧
縮波発生から2次脈動圧縮波伝播までに要するエキセン
トリックシャフトの回転角度を表わす。また、エンジン
回転数N = 3500〜5000 ram テ、上記
(I>式と同様ニ60 / 360 N ハ1°回転す
るのに要する時間(秒)を表わす。また、圧力波の伝播
速度c=343m/s  (20’C)である。さらに
、2は脈動波の正の次数で2次脈動を利用するのでZ=
2であり、1/2zは2次脈動が2往復する行程の逆数
を表わす。よって、これらの値から、U+=0.17〜
0.45mとなる。
Furthermore, the passage length ρ1 between the expansion chamber and the intake boat of each cylinder in the setting item d above is set to obtain an inertial pulsation effect, and is 1+, = (360-θ+61
) X60/36ONXc X 1/22- (II) That is, in the above formula 83, 36° is the interval of the intake stroke, and the intake boat opening period θ-270 to 320', ! : 7jθ1 is an invalid period that is defined by the period when the intake boat is fully closed while the compression wave is generated at the time of closing, and the period until the secondary pulsating compression wave is propagated from the intake boat opening, and the side intake θ+ Therefore, (360-θ+θ1) represents the rotation angle of the eccentric shaft required from the generation of the compression wave at the time of closing the mouth to the propagation of the secondary pulsating compression wave. In addition, the engine rotation speed N = 3500 to 5000 ram te, similar to the above formula (I), represents the time (seconds) required to rotate 1 degree. Also, the propagation speed of the pressure wave c = 343 m /s (20'C).Furthermore, since 2 is a positive order of the pulsating wave and uses the second-order pulsation, Z=
2, and 1/2z represents the reciprocal of the stroke in which the secondary pulsation makes two reciprocations. Therefore, from these values, U+=0.17~
It becomes 0.45m.

尚、<I)、(I)式では、圧力波の伝播に対する吸入
空気の流れの影響を無視している。これは、流速が音速
に比べて小さく、吸気通路の長さにほとんど変化をもた
らさないためである。
Note that <I), Equation (I) ignores the influence of the flow of intake air on the propagation of pressure waves. This is because the flow velocity is smaller than the speed of sound and causes almost no change in the length of the intake passage.

以下、本発明を図面に示す実施例に基づいて詳細に説明
する。
Hereinafter, the present invention will be described in detail based on embodiments shown in the drawings.

第1図および第2図において、1△おJ:び1Bはサイ
ド吸気ボート式の2気筒ロークリピストンエンジンにお
ける第1気筒および第2気筒であって、各気筒IA、I
Bは、各々、2節トロコイド状の内周面2aを備えたロ
ータハウジング2と、その両側に位置し後述の吸気通路
16a、16bが開口する吸気ボート3を備えたり一イ
ドハウジング4,4とで形成されたケーシング5内を、
略三角形状のロータ6がエキセン1〜リツクシせフト7
に支承されて遊星回転運動し、かっ各気筒IA。
In FIGS. 1 and 2, 1△ and J: and 1B are the first and second cylinders of a side-intake boat type two-cylinder low-repetition piston engine, and each cylinder IA, I
B includes a rotor housing 2 having a two-bar trochoidal inner circumferential surface 2a, and an intake boat 3 located on both sides of the rotor housing 2, in which intake passages 16a and 16b, which will be described later, are opened. The inside of the casing 5 formed by
A substantially triangular rotor 6 connects the eccentric 1 to lift shaft 7.
Each cylinder IA is supported by a planetary rotary motion.

1Bのロータ6.6はエキセン1−リックシA771〜
7の回転角で180°の位相差を持ち、上記各ロータ6
の回転に伴ってケーシング5内を3つの作動室8,8.
8に区画して、各々の気筒1Δ、1Bにおいて上記18
0°の位相差でもって吸気、圧縮、爆発、膨張J3よび
排気の各行程を順次行うものである。尚、9は各気筒1
Δ、IBにおいてロータハウジング2に開設された排気
ポート、10 a3よび11はリーディング側およびト
レーリング側点火プラグ、12はロータ6の側面に装着
されたサイドシール、13はロータ6の各頂部に装着さ
れICアペックスシール、14はロータ6の各頂部両側
面に装着されたコーナシールである。
1B rotor 6.6 is eccentric 1-Ricci A771~
Each rotor 6 has a phase difference of 180° at a rotation angle of 7.
As the casing 5 rotates, three working chambers 8, 8 .
18 in each cylinder 1Δ, 1B.
The intake, compression, explosion, expansion J3, and exhaust strokes are performed in sequence with a phase difference of 0°. In addition, 9 is each cylinder 1
Exhaust ports opened in the rotor housing 2 at Δ and IB, 10 a3 and 11 are leading side and trailing side spark plugs, 12 is a side seal attached to the side of the rotor 6, 13 is attached to each top of the rotor 6 The IC apex seals 14 are corner seals attached to both sides of the top of the rotor 6.

上記吸気ポー1〜3はロータ6側面によって開閉され、
該吸気ポー1−3の開口期間θはエキセン1〜リツクシ
ト71〜7の回転角で270〜320°の範囲に設定さ
れている。
The intake ports 1 to 3 are opened and closed by the side surface of the rotor 6,
The opening period θ of the intake port 1-3 is set in the range of 270 to 320 degrees based on the rotation angle of the eccentrics 1 to 71 to 7.

一方、15はエアクリーナ、16は内気筒1A。On the other hand, 15 is an air cleaner, and 16 is an inner cylinder 1A.

1Bに吸気を供給するための主吸気通路であって、該主
吸気通路16には吸入空気量を検出する■アフローメー
タ17およびその下流に吸入空気量を制御す′るスロッ
トルバルブ18が配設されている。
1B, and the main intake passage 16 is provided with an aflow meter 17 for detecting the amount of intake air and a throttle valve 18 downstream thereof for controlling the amount of intake air. It is set up.

上記主吸気通路16は等長の第1および第2吸気通路1
6a、16bに分岐されたのも」上記吸気ボーI−3,
3を介して各気筒1A、1Bの作動室88に連通されて
いる。また、該第1 J5よび第2吸気通路16a、1
6bにはそれぞれ−」上記エアフローメータ17の出力
に応じて燃料噴剣吊を制御する電磁弁式の燃料噴射ノズ
ル19.19が配設されている。
The main intake passage 16 has first and second intake passages 1 of equal length.
6a and 16b are the above-mentioned intake bow I-3,
3 to the working chambers 88 of each cylinder 1A, 1B. In addition, the first J5 and the second intake passages 16a, 1
6b are respectively provided with electromagnetic valve type fuel injection nozzles 19 and 19 that control the fuel injection depending on the output of the air flow meter 17.

そして、上記主吸気通路16の分岐部4Jスロツトルバ
ルブ18下流に位置し、該分岐部は、第1吸気通路16
aと第2吸気通路16bとを連通する連通路20を有す
る拡大室21によって構成されている。上記連通路20
の通路面積は圧力波(排気干渉効果ての圧縮波)をその
減衰を小さくして有効に伝)ヱリ−るにうに第1.第2
吸気通路゛16a、16bの最小通路面積と同等かそれ
以上に設定されている。また、上記拡大室21の容積は
、エンジン排気量に対して0.5〜2倍(低負荷用おJ
:び高負荷用の2系統の吸気ボートを設りた場合ではそ
のトータルで)に設定されており、0゜5倍以下では膨
張波と圧縮波間の反転効果が得られない一方、2倍以上
では圧ツノ波が拡散してしまい慣性脈動効果が著しく低
下することに依る。まに1上記拡大室21は、エンジン
の加速時又は減速時等の過渡運転時に、11ハノる吸入
空気のザージタンクどして機能し、燃料の良好な応答性
を確保づるものである。
The branch portion 4J of the main intake passage 16 is located downstream of the throttle valve 18, and the branch portion is located in the first intake passage 16.
It is constituted by an enlarged chamber 21 having a communication passage 20 that communicates the intake passage a with the second intake passage 16b. The above communication path 20
The passage area is the first to effectively transmit pressure waves (compression waves due to exhaust interference effects) by reducing their attenuation. Second
It is set to be equal to or larger than the minimum passage area of the intake passages 16a and 16b. In addition, the volume of the expansion chamber 21 is 0.5 to 2 times the engine displacement (for low load use).
: If two systems of intake boats for high loads are installed, the total value is set to 0. This is because the pressure horn waves are diffused and the inertial pulsation effect is significantly reduced. The enlarged chamber 21 functions as a surge tank for intake air during transient operations such as acceleration or deceleration of the engine, ensuring good fuel response.

また、上記内気筒1△、1Bの吸気ポー1〜3゜3間の
通路長さしは、連通路20の通路長さ92と該連通路2
0下流の第1おにび第2吸気通路1(3a 、 16b
−(7)各通路長さ9.+、9+ とを加算したものと
なり(L−U2+2Q+ )、該通路長さLは、500
0〜7000 ppmのエンジン高回転時を塁tlF−
とじて上述の(I>式から、L−((270〜320)
−180−20)x60/360x (5000〜70
00)×343 〜0.57〜1.3.7 (m) に設定されている。尚、この場合、上記通路長さ91お
よび9.2はそれぞれ各通路の中心長さをどっている。
Further, the passage length between the intake ports 1 to 3°3 of the inner cylinders 1△ and 1B is the passage length 92 of the communication passage 20 and the passage length 92 of the communication passage 20.
0 downstream first and second intake passages 1 (3a, 16b
-(7) Each passage length9. +, 9+ (L-U2+2Q+), and the passage length L is 500
0 to 7000 ppm at high engine speed tlF-
From the above formula (I>, L-((270-320)
-180-20)x60/360x (5000~70
00)×343 to 0.57 to 1.3.7 (m). In this case, the passage lengths 91 and 9.2 respectively correspond to the center length of each passage.

さらに、上記第1.第2吸気通路168.16bの通路
長さ脅1、っまり該各吸気通路16 a 。
Furthermore, the above 1. The passage length of the second intake passage 168.16b is 1, that is, each intake passage 16a.

16bの拡大室21への開口端面がら作動室8への間口
(吸気ボート3)までの通路長ざplは、3500〜5
000rl)、mのエンジン中回転時を基準として一ト
記(I)式から 9+   =  (360−(270〜 320)  
−1−20)X60/360X (3500〜5000
)X343X1/2X2 〜0.17〜0.45 (m) に設定されている。
The passage length pl from the opening end face to the expansion chamber 21 of 16b to the frontage (intake boat 3) to the working chamber 8 is 3500 to 5
000rl), m from the equation (I) based on the engine's medium rotation: 9+ = (360-(270~320)
-1-20)X60/360X (3500~5000
)X343X1/2X2 ~0.17~0.45 (m).

尚、第2図中、22は排気ポート9に接続された排気通
路、23は排気通路22の途中に介設された触媒装置く
図示せず)を補助リ−る排気浄化用の拡大マニホールド
である。
In Fig. 2, 22 is an exhaust passage connected to the exhaust port 9, and 23 is an enlarged manifold for exhaust purification that auxiliary feeds a catalyst device (not shown) interposed in the middle of the exhaust passage 22. be.

次に、その作動を第3図により説明するに、高出力を要
する5000へ−700Orpmのエンジン高回転時に
は、一方の気筒例えば第2気筒1Bの吸気ボート3開口
時に第2吸気通路16b内に発生した開口時圧縮波は、
上記5000〜70QOrpmの高回転時を基準として
上記(1)式により内気筒1A、1Bの吸気ボート3,
3間の通路長さLを0.57〜1.37mに設定したこ
とにより、第2吸気通路16b→拡大室21の連通路2
0→第1吸気通路16aを経て、18o°の位相差をも
って先に吸気行程に入って全開直前状態である第1気筒
1Δの吸気ボート3に伝播される。
Next, to explain its operation with reference to FIG. 3, when the engine is running at a high speed of 5,000 to 700 rpm, which requires high output, a phenomenon occurs in the second intake passage 16b when one cylinder, for example, the intake boat 3 of the second cylinder 1B, is opened. The compression wave at the time of opening is
Based on the above equation (1), the intake boat 3 of the inner cylinders 1A and 1B is
By setting the passage length L between 3 to 0.57 to 1.37 m, the communication passage 2 from the second intake passage 16b to the enlarged chamber 21
0 → via the first intake passage 16a, and is propagated to the intake boat 3 of the first cylinder 1Δ, which enters the intake stroke first with a phase difference of 18o and is in a state immediately before full opening.

その結果、この圧縮波により、全開直前の第1気筒1Δ
の吸気ボート3からの吸気の吹き返しが抑制されて吸気
が作動室8内へ押し込まれ、つまり過給が行われること
になる。続いて、上記第2気筒1Bの吸気ボート3開口
がら18o′後に開口づる第1気筒1Aの吸気ポート3
がら発生する開口時圧縮波は同様に全開直前の第2気筒
1Bの吸気ボート3−伝播されて過給が行われる。以後
同様にして、気□筒1Δ、1B相互間での排気干渉効果
による顕著なる過給効果によって、5060〜7000
 rl’1mのエンジン高回転時での充填効率が増大し
て出力を大「]]に向上さけることができる。
As a result, due to this compression wave, the first cylinder 1Δ just before full opening is
The blowback of the intake air from the intake boat 3 is suppressed, and the intake air is forced into the working chamber 8, which results in supercharging. Next, the intake port 3 of the first cylinder 1A opens 18 o' after the opening of the intake port 3 of the second cylinder 1B.
Similarly, the compression wave generated at the time of opening is propagated through the intake boat 3 of the second cylinder 1B just before full opening, and supercharging is performed. Thereafter, in the same way, due to the remarkable supercharging effect due to the exhaust interference effect between the cylinders 1Δ and 1B, the temperature was increased to 5060~7000.
The charging efficiency increases at high engine speeds of rl'1m, and the output can be greatly improved.

一方、3500〜5000 ppmのエンジン中回転時
には、各気筒1A、IBにおいて吸気ポート3閉口時に
第1.第2吸気通路16a、16a内に発生ずる閉口時
圧縮波は、各吸気ポート3と拡大室21との間の通路長
さ91を3500〜5゜00 rprIlのエンジン中
回転時を基準として上記(H)式にJ:す0.17〜0
.45tnに設定したことにより、第1.第2吸気通路
16a、16b→拡大室21(膨張波に反転して反射)
=)第1゜第2吸気通路16a、16b−’吸気ポー1
−3(吸気ボート3開塞により膨張波のまま反則)→第
1゜第2吸気通路16a、16b→拡大室21(圧縮波
に反転して反IJJ)→第1.第2吸気通路16a。
On the other hand, at medium engine speeds of 3500 to 5000 ppm, when the intake port 3 is closed in each cylinder 1A and IB, the first. The compression waves generated in the second intake passages 16a, 16a at the time of closing are determined by the above (( H) In the formula, J: 0.17~0
.. By setting it to 45tn, the first. Second intake passages 16a, 16b → expansion chamber 21 (inverted and reflected by expansion waves)
=) 1st゜Second intake passage 16a, 16b-'Intake port 1
-3 (foul as an expansion wave due to intake boat 3 opening) → 1st degree, second intake passages 16a, 16b → expansion chamber 21 (reversed to a compression wave and becomes anti-IJJ) → 1st degree. Second intake passage 16a.

16bを経て、2次脈動圧縮波として各気筒IA。16b, each cylinder IA as a secondary pulsating compression wave.

1Aの次の開口直後の吸気ボー1−3に伝播される。It is propagated to the intake bow 1-3 immediately after the next opening of 1A.

その結果、この2次脈動圧縮波により、開口時の各気筒
IA、1Bの吸気ポート3からの排気の吹き返しが抑制
されて吸気が作動室8内へ押し込まれて過給が行われる
ことになる。よって、各気筒1△、IB自身での慣性脈
動効果による過給効果にJ:す、3500〜5000p
pmの1ニンジン中回転時での充填効率が増大して出力
を向上させることができる。尚、上記慣性脈動効果は、
エンジンの高回転域で1次脈動膨張波として作用するが
、2次脈動圧縮波の作用範囲を3500〜5000rp
mを基準どして設定したことにより、上記1次脈動膨張
波は7000 ppm以上でしか作用せず、上記エンジ
ン高回転時(5000〜7000rpm )での排気干
渉効果による過給効果を損うことはない。
As a result, this secondary pulsating compression wave suppresses the blowback of exhaust gas from the intake ports 3 of each cylinder IA and 1B when the cylinders are opened, and the intake air is forced into the working chamber 8 to perform supercharging. . Therefore, for each cylinder 1△, the supercharging effect due to the inertial pulsation effect in IB itself is J: 3500~5000p.
It is possible to increase the filling efficiency during one rotation of pm and improve the output. The above inertial pulsation effect is
It acts as a primary pulsating expansion wave in the high rotation range of the engine, but the acting range of the secondary pulsating compression wave has been reduced from 3500 to 5000 rpm.
By setting m as a reference, the primary pulsating expansion wave acts only at 7000 ppm or more, which impairs the supercharging effect due to exhaust interference effect at high engine speeds (5000 to 7000 rpm). There isn't.

したがって、このように、各気筒1Δ、1Bにおいて、
エンジン高回転時(5000〜7000ppm )での
全開直前の吸気ボート3に対−する排気干渉効果、およ
びエンジン中回転時(ζ3500〜5000rl)m)
での開1」直後の吸気ボート3に対する慣性脈動効果に
より、第4図に示すようにエンジンの中回転域から高回
転域に亙ってエンジンの出力を向上させることができる
。尚、第4図では、連通路20および拡大室21がなく
排気干渉効果および慣性脈動効果のない従来例〈破線で
示づ)に対しで、エンジン高回転時として6000pp
m@14準として排気干渉効果を得るように設定する(
実線で示す〉とともに、1−レジン中回転時とし一’C
4000rpmを基準として慣1η脈動効果を得るよう
に設定したく一点鎖線で示ツ゛)場合にお【プるエンジ
ンの出力トルク特性を示す。
Therefore, in this way, in each cylinder 1Δ, 1B,
Exhaust interference effect on the intake boat 3 just before full opening at high engine speeds (5000-7000ppm) and at medium engine speeds (ζ3500-5000rl)
Due to the inertial pulsation effect on the intake boat 3 immediately after opening 1'', the output of the engine can be improved from the middle rotation range to the high rotation range of the engine, as shown in FIG. In addition, in Fig. 4, compared to the conventional example (shown by the broken line) which does not have the communication passage 20 and the expansion chamber 21 and has no exhaust interference effect or inertial pulsation effect, the engine speed is 6000pp at high engine speed.
Set to obtain the exhaust interference effect as m@14 standard (
〉 indicated by a solid line, and when rotating during 1-resin, 1'C.
The output torque characteristics of the engine are shown when the setting is set to obtain the 1η pulsation effect with reference to 4000 rpm (as shown by the dashed line).

また、上記連通路20を右づる拡大室21は、スロット
ルバルブ18下流に位置するので、該スロットルバルブ
18によって圧力波が減衰されることがなく、上記排気
干渉効果a′3J:び慣性脈動効果を有効に発揮するこ
とができ、過給効果の確実化を図ることができる。
Furthermore, since the enlarged chamber 21 extending to the right in the communication path 20 is located downstream of the throttle valve 18, the pressure waves are not attenuated by the throttle valve 18, and the exhaust interference effect a'3J and the inertial pulsation effect are prevented. can be effectively exerted, and the supercharging effect can be ensured.

また、上記排気干渉効果および慣性脈動効果による過給
効果は、各気筒IA、1Bの吸気ボート3の開口期間、
第1吸気通路16aと第2吸気通路16bとを連通づ°
る連通路20を有する拡大窒21の位置、並びに内気筒
IA、1Bの吸気ポート3,3間の通路長さLおよび上
記拡大室21と吸気ポート3との間の通路長さ91を上
述の如く設定することによって得られ、過給機等を要さ
ないので、既存の吸気系の僅かな設81変更で済み、構
造が極めて簡単なものであり、よって容易にかつ安価に
実施でき、構造の簡略化およびコストダウン化を大巾に
図ることができる。
Further, the supercharging effect due to the exhaust interference effect and the inertial pulsation effect is caused by the opening period of the intake boat 3 of each cylinder IA, 1B,
The first intake passage 16a and the second intake passage 16b are communicated with each other.
The position of the enlarged nitrogen 21 having the communication passage 20, the passage length L between the intake ports 3 and 3 of the inner cylinders IA and 1B, and the passage length 91 between the enlarged chamber 21 and the intake port 3 are determined as described above. Since it does not require a supercharger or the like, only a slight change in the existing intake system is required, and the structure is extremely simple, so it can be implemented easily and inexpensively. simplification and cost reduction can be achieved to a large extent.

尚、本発明は上記実施例に限定されるものではなく、そ
の他種々の変形例をも包含するものである。例えば、上
記実施例では燃わ1噴射式のロータリピストンエンジン
に適用した例を示したが、気化器式のしのにも適用でき
るのは勿論のことである。しかし、燃料噴射式の場合、
上記実施例の如く燃料唱剣ノズル19を連通路20(拡
大室21)下流の吸気通路15a、161)に設けるご
とによって、該吸気通路16a、16bの通路長さ91
が良くなることによる燃料の応答性の悪化を防止できる
ので好ましい。
It should be noted that the present invention is not limited to the above-mentioned embodiments, but also includes various other modifications. For example, in the above embodiment, an example was shown in which the present invention was applied to a single fuel injection type rotary piston engine, but it goes without saying that the present invention can also be applied to a carburetor type engine. However, in the case of fuel injection type,
As in the above embodiment, by providing the fuel nozzle 19 in the intake passages 15a, 161 downstream of the communication passage 20 (enlarged chamber 21), the passage length 91 of the intake passages 16a, 16b is
This is preferable because it is possible to prevent deterioration in fuel responsiveness due to improvement in .

また、上記実施例は、各気筒1△、1Bに対しそれぞれ
一つの吸気通路16a、161)を設けた一系統の場合
について述べたが、本発明は各気筒に対し異なる吸気ボ
ートをもつ独立した低負荷用と高負荷用との2系統の吸
気通路を設ける場合にも適用できる。この場合、2系統
の吸気系の両方又はいずれか一方が排気干渉効果および
慣性脈動効果を得るように設定すればよい。但し、2系
統の吸気ボー小の閉口時期が異なるものにあっては閉口
時期の遅い方に上記効果を得るように設定覆ることが好
ましい。
Further, in the above embodiment, one system is provided in which each cylinder 1Δ, 1B is provided with one intake passage 16a, 161), but the present invention provides an independent system with a different intake port for each cylinder. It can also be applied when two intake passages are provided, one for low load and one for high load. In this case, both or one of the two intake systems may be set to obtain the exhaust interference effect and the inertial pulsation effect. However, if the closing timings of the two systems have different intake bows, it is preferable to set the closing timing later so as to obtain the above effect.

加えて、各気筒の吸気ボー1−の聞]]時期は上死点後
エキセントリックシャフトの回転角で30〜60°の範
囲に設定することが充填効率の向上を図る上でりrまし
い。また、吸排気オーバラップ期間はエキセントリック
シャフトの回転角でO〜20°の範囲に設定することが
、充填効率の向上を図るとともに1ダイリユーシヨンガ
スの持込み量を少なくしてエンジン低負荷時の失火を防
止できるので好ましい。
In addition, in order to improve the charging efficiency, it is preferable to set the timing between the intake bows 1 and 1 of each cylinder to a range of 30 to 60 degrees in rotation angle of the eccentric shaft after top dead center. In addition, setting the intake/exhaust overlap period to a range of 0 to 20° in terms of the rotation angle of the eccentric shaft improves charging efficiency and reduces the amount of 1-dilution gas brought in during low engine loads. This is preferable because misfires can be prevented.

以上説明したように、本発明によれば、1ノイド吸気ポ
一ト式の2気筒ロータリビス1ヘンエンジンにおいて、
5000〜7000ppmのエンジン高回転時には気筒
相互間の排気干渉効果にJ:り過給効果を1qるととも
に、3500〜5000ppmのエンジン中回転時には
各気筒自身の慣性脈動効果により過給効果を得るように
したので、過給機等を要さずに既存の吸気系の僅かな設
計変更による極めて簡単な構成でもって、エンジンの中
回転域から高回転域に亙って充填効率を高めて高負荷時
の出ノj向上を図ることができ、よってエンジン出力向
」二対策の容易実施化およびコストダウン化に大いに寄
与するものである。
As explained above, according to the present invention, in a 1-noid intake point type 2-cylinder rotary vis 1-hen engine,
At high engine speeds of 5,000 to 7,000 ppm, the supercharging effect is reduced by 1q due to the exhaust interference effect between cylinders, and at medium engine speeds of 3,500 to 5,000 ppm, the supercharging effect is obtained by the inertial pulsation effect of each cylinder itself. Therefore, with an extremely simple configuration that requires only a slight design change to the existing intake system without the need for a supercharger, the charging efficiency can be increased from the mid- to high-speed range of the engine, and it can be used under high loads. This greatly contributes to the ease of implementation of measures to improve engine output and to cost reduction.

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

図面は本発明の実施例を示し、第1図は全体説明図、第
2図は全体概略構成図、第3図は第1および第2気筒の
吸気行程を示す説明図、第4図は本発明による出力トル
ク特性を示すグラフである。 1△・・・第1気筒、1B・・・第2気筒、2・・・ロ
ータハウジング、2a・・・2節1ヘロコイド状内周面
、3・・・吸気ポート、4・・・サイドハウジング、5
・・・ケーシング、6・・・ロータ、7・・・エキセン
トリックシャフト、16・・・主吸気通路、16a・・
・第1吸気通路、16b・・・第2吸気通路、18・・
・スロットルバルブ、20・・・連通路、21・・・拡
大室。 ←201
The drawings show an embodiment of the present invention, and FIG. 1 is an overall explanatory diagram, FIG. 2 is an overall schematic configuration diagram, FIG. 3 is an explanatory diagram showing the intake stroke of the first and second cylinders, and FIG. 4 is an illustration of the main body. 3 is a graph showing output torque characteristics according to the invention. 1△...First cylinder, 1B...Second cylinder, 2...Rotor housing, 2a...2-node 1 herocoid-shaped inner peripheral surface, 3...Intake port, 4...Side housing , 5
...Casing, 6...Rotor, 7...Eccentric shaft, 16...Main intake passage, 16a...
・First intake passage, 16b...Second intake passage, 18...
- Throttle valve, 20... Communication passage, 21... Expansion chamber. ←201

Claims (1)

【特許請求の範囲】[Claims] (1)2節トロコイド状の内周面を備えたロータハウジ
ングと、その両側に位置し吸気通路が間口する吸気ボー
トを備えたサイドハウジングとで形成されたケーシング
内を、略三角形状のロータがエキセントリックシャフト
に支承されて遊星回転運動するものであって、各ロータ
がエキセントリックシャフトの回転角で180°の位相
差を持つ2気筒ロータリピストンエンジンにおいて、 a、吸気ボートの開口期間をエキセントリフクシ1フフ
トの回転角で270〜320°の範囲に設定1−ること
、 b、各気筒の吸気通路をスロワ1〜ルバルブ下流におい
て連通づる連通路を右゛す“る拡大至を設(プること、 C6該連通路およびその下流の吸気通路にょって形成さ
れる両気筒の吸気ボート間の通路長さを0.57〜1.
37mになるように設定り−ること d、上記拡大室から各気筒の吸気ボー1〜までの吸気通
路の通路長さを0.17〜0.45mになるように設定
すること の条件のもとで、5000〜7000 ppm (D 
エンジン高回転時、一方の気筒の吸気ボー1〜開口時に
吸気通路内に発生する圧縮波を上記連通路を介して使方
の気筒の全開直前の吸気ボートに伝播させて過給を行う
一方、3500〜500Q rpmのエンジン中回転時
、各気筒の吸気ボート開口時に吸気通路内に発生する圧
縮波を開拡大室で2度反転した2次脈動圧縮波を該各気
筒の開口直後の吸気ポー1−に伝播さゼて過給を行うよ
うにしたことを特徴と覆るU−クリビス1−ンエンジン
の吸気装置。
(1) A substantially triangular rotor runs inside a casing formed by a rotor housing with a two-bar trochoidal inner circumferential surface and a side housing with intake boats located on both sides of the rotor housing with intake passages opening. In a two-cylinder rotary piston engine that is supported by an eccentric shaft and performs planetary rotation, and each rotor has a phase difference of 180° at the rotation angle of the eccentric shaft, a. Set the rotation angle of the foot in the range of 270 to 320 degrees. b. Set the intake passage of each cylinder from the thrower 1 to the downstream side of the valve. , C6 The length of the passage between the intake boats of both cylinders formed by the communication passage and the intake passage downstream thereof is 0.57 to 1.
The length of the intake passage from the enlarged chamber to the intake bow 1 of each cylinder is set to be 0.17 to 0.45 m. and 5000 to 7000 ppm (D
When the engine is running at high speed, a compression wave generated in the intake passage when the intake bow of one cylinder is opened is propagated through the communication passage to the intake boat of the cylinder in use just before it is fully opened, and supercharging is performed. When the engine rotates at 3500 to 500 Q rpm, the compression wave generated in the intake passage when the intake port of each cylinder is opened is reversed twice in the expansion chamber, and the secondary pulsating compression wave is transferred to the intake port 1 immediately after the opening of each cylinder. - An intake system for a U-crivis 1-engine, characterized by supercharging by propagation to the engine.
JP57181964A 1982-10-15 1982-10-15 Intake device of rotary piston engine Granted JPS5970835A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP57181964A JPS5970835A (en) 1982-10-15 1982-10-15 Intake device of rotary piston engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP57181964A JPS5970835A (en) 1982-10-15 1982-10-15 Intake device of rotary piston engine

Publications (2)

Publication Number Publication Date
JPS5970835A true JPS5970835A (en) 1984-04-21
JPS619492B2 JPS619492B2 (en) 1986-03-24

Family

ID=16109943

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57181964A Granted JPS5970835A (en) 1982-10-15 1982-10-15 Intake device of rotary piston engine

Country Status (1)

Country Link
JP (1) JPS5970835A (en)

Also Published As

Publication number Publication date
JPS619492B2 (en) 1986-03-24

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