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JPS6340251B2 - - Google Patents
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JPS6340251B2 - - Google Patents

Info

Publication number
JPS6340251B2
JPS6340251B2 JP57208149A JP20814982A JPS6340251B2 JP S6340251 B2 JPS6340251 B2 JP S6340251B2 JP 57208149 A JP57208149 A JP 57208149A JP 20814982 A JP20814982 A JP 20814982A JP S6340251 B2 JPS6340251 B2 JP S6340251B2
Authority
JP
Japan
Prior art keywords
intake
load
passage
low
cylinder
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
JP57208149A
Other languages
Japanese (ja)
Other versions
JPS5999031A (en
Inventor
Asao Tadokoro
Haruo Okimoto
Ikuo Matsuda
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.)
Matsuda KK
Original Assignee
Matsuda KK
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 Matsuda KK filed Critical Matsuda KK
Priority to JP57208149A priority Critical patent/JPS5999031A/en
Publication of JPS5999031A publication Critical patent/JPS5999031A/en
Publication of JPS6340251B2 publication Critical patent/JPS6340251B2/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)

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、詳しくは低負荷用と高負荷用との2系
統のサイド吸気ポート式の2気筒ロータリピスト
ンエンジンにおいて吸気通路内に発生する吸気圧
力波を利用してエンジン高負荷高回転時に過給効
果を得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 particularly, the present invention relates to an intake system for a rotary piston engine. This invention relates to a device that uses intake pressure waves to obtain a supercharging effect when the engine is under high load and high rotation speed.

一般に、このような2系統のサイド吸気ポート
式の2気筒ロータリピストンエンジンとして、2
節トロコイド状の内周面を有するロータハウジン
グとその両側に位置する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
エキセントリツクシヤフトに支承されて遊星回転
運動し、かつ低負荷用絞り弁を備えた低負荷用吸
気通路と高負荷用絞り弁を備えた高負荷用吸気通
路とが上記低負荷用絞り弁下流において各々独立
して上記各サイドハウジングに設けた低負荷用お
よび高負荷用吸気ポートによつて作動室に開口す
るものであつて、各気筒のロータがエキセントリ
ツクシヤフトの回転角で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。
そして、エンジンの低負荷時には上記低負荷用絞
り弁のみを開作動して低負荷用吸気通路のみから
吸気を供給する一方、エンジンの高負荷時には高
負荷用絞り弁をも開作動して高負荷用吸気通路か
らも吸気の供給を行うことにより充填効率を高め
て出力向上を図るようにした、いわゆるデユアル
インダクシヨン方式と称されるものが知られてい
る。尚、上記低負荷用絞り弁を低負荷用吸気通路
内に設ける型式の他に、低負荷用吸気通路と高負
荷用吸気通路との分岐部上流に設ける型式のもの
も含まれる。
In general, as a two-system side intake port type two-cylinder rotary piston engine, two
A substantially triangular rotor is supported by an eccentric shaft and rotates planetarily within a casing formed by a rotor housing having a nodular trochoidal inner peripheral surface and side housings located on both sides of the rotor housing. A low-load intake passage equipped with a throttle valve and a high-load intake passage equipped with a high-load throttle valve are independently provided in each of the side housings downstream of the low-load throttle valve. The load intake port opens into the working chamber, and the rotor of each cylinder has a phase difference of 180° at the rotation angle of the eccentric shaft, and the above 180° phase difference between the two cylinders. The intake, compression, explosion, expansion, and exhaust strokes are sequentially performed in each cylinder as the rotor rotates while maintaining the
When the engine is under low load, only the low-load throttle valve is opened to supply intake air only from the low-load intake passage, while when the engine is under high load, the high-load throttle valve is also opened and the high-load throttle valve is opened. A so-called dual induction system is known in which intake air is also supplied from the intake passage to increase filling efficiency and improve output. In addition to the type in which the low-load throttle valve is provided in the low-load intake passage, there is also a type in which the low-load throttle valve is provided upstream of the branch between the low-load intake passage and the high-load intake passage.

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吸
気の過給を行うことにより、充填効率を高めて出
力向上を図るようにすることはよく知られている
が、過給機を要するため、構造が大がかりとなる
とともにコストアツプとなる嫌いがあつた。
By the way, it is well known that conventionally, in such a rotary piston engine, a supercharger is installed in the intake passage to supercharge the intake air, thereby increasing the charging efficiency and increasing the output. However, since it requires a supercharger, the structure becomes large-scale and costs increase.

また、従来、吸気圧力波により過給効果を得る
技術として、実公昭45−2321号公報に開示されて
いるように、単一気筒のロータリピストンエンジ
ンにおいて、吸気管を寸法の異なる2本の通路に
分け、それぞれ別の吸気ポートを有し、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、吸気管の寸法やエンジン
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
ン回転域に亙つて好適な充填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、
単一気筒のロータリピストンエンジンに対するも
のであつて、吸気通路内で発生する吸気圧力波を
どのように利用するのか、その構成、作用が定か
でなく、直ちに実用に供し得ないものであつた。
しかも、吸気ポートとしてペリフエラルポートを
用いているため、吸気ポートは吸気作動室が閉じ
る前に排気作動室と連通することになり、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
得ることが困難であつた。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
400〜600mmHg(ゲージ圧)程度に、ターボ過給機
付エンジンでは1000mmHg以上になつており、上
記ペリフエラルポート方式による充填効率向上は
期待できないものとなつている。
In addition, conventionally, as a technique for obtaining a supercharging effect using intake pressure waves, as disclosed in Japanese Utility Model Publication No. 45-2321, in a single-cylinder rotary piston engine, the intake pipe is divided into two passages of different sizes. The engine is divided into two sections, each with a separate intake port, and when the engine is running at high speeds, two intake passages are used, and when the engine is running at low speeds, the intake passage that is at the later closing position is closed, and the intake air is blocked earlier. , which utilizes the supercharging effect due to intake air blockage at the point of maximum intake pressure, which is a function of intake pipe dimensions and engine speed, to obtain suitable charging efficiency over a wide range of engine speeds. Proposed. But this one is
It was designed for a single-cylinder rotary piston engine, and it was not clear how to utilize the intake pressure waves generated in the intake passage, and its structure and operation were not clear, so it could not be put into practical use right away.
Moreover, since a peripheral port is used as the intake port, the intake port communicates with the exhaust working chamber before the intake working chamber closes, and a supercharging effect can be obtained by blowing back exhaust gas from the exhaust working chamber. was difficult. In particular, in recent years commercially available cars, engine exhaust pressure has increased to reduce noise and purify exhaust gas.
The pressure is about 400 to 600 mmHg (gauge pressure), and in a turbocharged engine it is more than 1000 mmHg, making it impossible to expect improvement in charging efficiency by the peripheral port 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ポートの吸気特性を検討
するに、 (i) 吸気ポート開口時には作動室の残留排気ガス
の圧力によつて吸気が圧縮され、吸気通路内の
吸気ポート部分に圧縮波が発生すること (ii) 吸気ポート閉口時には吸気の吹き返しが生じ
ていること を知見した。このことから、一方の気筒での上記
(i)の圧縮波を他方の気筒の特に上記吸気の吹き返
しが生じる全閉直前の吸気ポートに作用せしめれ
ば過給効果が効果的に得られること(以下、排気
干渉効果という)を見い出したのである。この排
気干渉効果は、上述の如く、近年、エンジン排気
系に排気浄化用の触媒装置が介設されて排圧が高
くなつていることから、その効果が顕著である。
Therefore, when examining the intake characteristics of the side intake port in a rotary piston engine, the present inventors found that (i) when the intake port is opened, the intake air is compressed by the pressure of the residual exhaust gas in the working chamber, and the air inside the intake passage is compressed. We found that compression waves occur at the intake port (ii) When the intake port is closed, intake air blows back. From this, the above for one cylinder
It has been found that a supercharging effect can be effectively obtained by applying the compression wave (i) to the other cylinder, especially the intake port immediately before fully closing, where the intake air blowback occurs (hereinafter referred to as the exhaust interference effect). It is. As mentioned above, this exhaust interference effect is remarkable because in recent years, catalyst devices for purifying exhaust gas have been installed in engine exhaust systems, resulting in higher exhaust pressures.

尚、サイド吸気ポート式と異なり、吸気通路が
ロータハウジングに開口するペリフエラル吸気ポ
ート式にあつては、該吸気ポートが常に作動室に
開口しているために上記にような効果は生じな
い。
Note that, unlike the side intake port type, in the peripheral intake port type in which the intake passage opens into the rotor housing, the above effect does not occur because the intake port always opens into the working chamber.

すなわち、本発明は、上記の如き2系統のサイ
ド吸気ポート式の2気筒ロータリピストンエンジ
ンにおいて、各吸気ポートの開口期間、各気筒の
少なくとも一方の吸気通路の連通位置、および各
気筒の少なくとも一方の吸気ポート間の通路長さ
を適切に設定することにより、5000〜7000rpmの
エンジン高回転時、少なくとも一方の吸気系統で
の排気干渉効果により過給効果を得、よつて過給
機等を用いることなく既存の吸気系の簡易な設計
変更による簡単な構成によつてエンジン高負荷高
回転時の充填効率を高めて出力向上を有効に図る
ことを目的とするものである。
That is, the present invention provides a two-system side intake port type two-cylinder rotary piston engine as described above, in which the opening period of each intake port, the communication position of at least one intake passage of each cylinder, and the communication position of at least one of each cylinder By appropriately setting the passage length between the intake ports, a supercharging effect can be obtained due to the exhaust interference effect in at least one intake system during high engine speeds of 5,000 to 7,000 rpm, and thus a supercharger etc. can be used. The purpose of this invention is to effectively improve the output by increasing the charging efficiency at high engine load and high rotation speeds through a simple configuration by simply changing the design of the existing intake system.

この目的を達成するため、本発明の構成は、2
節トロコイド状の内周面を有するロータハウジン
グとその両側に位置するサイドハウジングとで形
成されるケーシング内を、略三角形状のロータが
エキセントリツクシヤフトに支承されて遊星回転
運動し、かつ低負荷用絞り弁を備えた低負荷用吸
気通路と高負荷用絞り弁を備えた高負荷用吸気通
路とが各々独立して各サイドハウジングに設けた
低負荷用および高負荷用吸気ポートによつて作動
室に開口するものであつて、各ロータがエキセン
トリツクシヤフトの回転角で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 各吸気ポートの開口期間θをエキセントリツ
クシヤフトの回転角で270〜320゜の範囲に設定
すること、 b 各気筒の低負荷用および高負荷用吸気通路の
少なくとも一方の吸気通路を絞り弁下流におい
て連通路によつて連通すること、 c 該連通路およびその下流の吸気通路によつて
形成される両気筒の吸気ポート間の通路長さL
を0.57〜1.37mになるように設定すること の条件のもとで、少なくとも一方の吸気系統にお
いて、5000〜7000rpmのエンジン高回転時、一方
の気筒の吸気ポート開口時に吸気通路内に発生し
た圧縮波を上記連通路を介して他方の気筒の全閉
直前の吸気ポートに伝播させて過給を行うように
し、よつて少なくとも一方の吸気系統での気筒相
互間の排気干渉効果により吸気ポート全閉直前で
の吹き返しを抑えて充填効率を効果的に高めるよ
うにしたものである。
In order to achieve this objective, the configuration of the present invention is as follows:
A substantially triangular rotor is supported by an eccentric shaft and rotates planetarily within a casing formed by a rotor housing having a nodular trochoidal inner peripheral surface and side housings located on both sides of the rotor housing. A low-load intake passage equipped with a throttle valve and a high-load intake passage equipped with a high-load throttle valve are independently connected to the working chamber by low-load and high-load intake ports provided in each side housing. In a two-cylinder rotary piston engine in which each rotor has a phase difference of 180° with respect to the rotational angle of the eccentric shaft, a. 320°; b. At least one of the low-load and high-load intake passages of each cylinder is connected to the intake passage downstream of the throttle valve by a communication passage; c) The communication passage and its downstream Passage length L between the intake ports of both cylinders formed by the intake passage
is set to 0.57 to 1.37 m, the compression generated in the intake passage when the intake port of one cylinder is opened at high engine speed of 5000 to 7000 rpm in at least one intake system. Supercharging is performed by propagating the waves through the communication passage to the intake port of the other cylinder just before the fully closed state, and therefore the intake port is completely closed due to the exhaust interference effect between the cylinders in at least one intake system. This is designed to effectively increase filling efficiency by suppressing blowback immediately before the filling.

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5000〜7000rpm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領域
であつて高出力を要し、充填効率向上、出力向上
に有効な領域であることによる。
Here, the limitation of 5000 to 7000 rpm as the engine high speed to obtain the above exhaust interference effect is because the maximum output and maximum speed are generally set within this range. This is because it requires a lot of power and is an effective area for improving filling efficiency and power.

また、上記設定事項aでの各吸気ポート開口期
間θはその上限である320゜は、サイド吸気ポート
を介して先行作動室と後続作動室とが連通するの
を防止するためで、ロータ側面による実質的な開
口期間よりもサ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
ツ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えることに
より、サ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小間隙(通常200μ程
度)を介しての吸気作動室とそれに続く排気作動
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
ち込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、少なくとも開口期間をこれ以上に設定す
る必要がある。
In addition, the upper limit of the opening period θ of each intake port in setting item a above, 320°, is to prevent communication between the preceding working chamber and the succeeding working chamber via the side intake port, and is due to the side surface of the rotor. The opening period due to the side seal is approximately
40 degrees larger, and it is necessary to provide an interval of 40 degrees or more in order to avoid this side seal opening period lapping. By suppressing the opening period to less than this, communication between the intake working chamber and the subsequent exhaust working chamber is achieved through the minute gap (usually about 200μ) between the inner sliding surface of the side housing on the outside of the side seal and the rotor side surface. This prevents exhaust gas from entering the intake working chamber during low engine speeds and low loads, such as when idling, and ensures stable combustion. On the other hand, the lower limit of 270° is the minimum period of the geometrical intake stroke from top dead center (TDC) to bottom dead center (BDC). It is necessary to set the period longer than this.

また、上記設定事項bでの連通路の絞り弁下流
位置設定は、該絞り弁の存在が圧力波(圧縮波)
の伝播の抵抗となるのでそれを避けるためであ
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, when setting the downstream position of the throttle valve in the communication passage in setting item b above, the presence of the throttle valve causes a pressure wave (compression wave).
This is to avoid this as it becomes a resistance to the propagation of pressure waves, and to propagate the pressure waves effectively by reducing their attenuation.

さらに、上記設定事項cでの両気筒の吸気ポー
ト間の通路長さLは、5000〜7000rpmのエンジン
高回転時に排気干渉効果を得るように設定された
もので、 L=(θ−180−θ0)×(60/360N)×a ……() の式から求められた値である。すなわち、上記式
において、θは吸気ポート開口期間でθ=270〜
320゜であり、180゜は両気筒間の位相差であり、ま
たθ0は吸気ポート開口から開口時圧縮波が実質的
に発生するまでの期間と効果的に過給を行うため
に該開口時圧縮波を伝播させる吸気ポート全閉直
前から全閉までの期間とを合算した無効期間で、
θ0≒20゜であり、よつて(θ−180゜−θ0)は一方の
気筒での圧縮波発生から他方の気筒の吸気ポート
への伝播までに要するエキセントリツクシヤフト
の回転角度を表わす。また、Nはエンジン回転数
でN=5000〜7000rpmであり、60/360Nは1゜回転
するのに要する時間(秒)を表わす。また、aは
圧力波の伝播速度(音速)であつて、20℃でa=
343m/sである。よつて、これらの値から、L
=0.57〜1.37mとなる。
Furthermore, the passage length L between the intake ports of both cylinders in setting item c above is set to obtain an exhaust interference effect at high engine speeds of 5000 to 7000 rpm, and L = (θ-180-θ 0 )×(60/360N)×a...This is the value obtained from the formula (). That is, in the above formula, θ is the intake port opening period and θ=270~
320°, 180° is the phase difference between both cylinders, and θ 0 is the period from the opening of the intake port until a compression wave is substantially generated at the time of opening, and The invalid period is the sum of the period from just before the intake port is fully closed to when the time compression wave is propagated.
θ 0 ≈20°, and therefore (θ−180°−θ 0 ) represents the rotation angle of the eccentric shaft required from generation of a compression wave in one cylinder to propagation to the intake port of the other cylinder. Further, N is the engine rotational speed, N = 5000 to 7000 rpm, and 60/360N represents the time (seconds) required to rotate 1 degree. Also, a is the propagation velocity (sound velocity) of the pressure wave, and at 20°C a=
It is 343m/s. Therefore, from these values, L
= 0.57 to 1.37m.

尚、本発明の高負荷用および低負荷用吸気ポー
トの開口期間はロータ側面による吸気ポートの実
質的な開閉期間であつて、サ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小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 high-load and low-load intake ports of the present invention is the substantial opening/closing period of the intake ports by the side surface of the rotor, and is not due to the side seal. This is because the minute gap outside the side seal has no substantial effect on the generation and propagation of effective pressure waves in the high rotation range, which is the problem of the present invention.

また、上記()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。
Furthermore, the above equation () 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、1Aおよび1B
は低負荷用と高負荷用との2系統のサイド吸気ポ
ート式の2気筒ロータリピストンエンジンにおけ
る第1気筒および第2気筒であつて、各気筒1
A,1Bは各々、2節トロコイド状の内周面2a
を有するロータハウジング2と、その両側に位置
し後述の低負荷用吸気通路20a,20bおよび
高負荷用吸気通路21a,21bが各々開口する
低負荷用吸気ポート3および高負荷用吸気ポート
4を備えたサイドハウジング5,5とで形成され
たケーシング6内を、略三角形状のロータ7が単
一のエキセントリツクシヤフト8に支承されて遊
星回転運動し、かつ各気筒1A,1Bのロータ
7,7はエキセントリツクシヤフト8の回転角で
180゜の位相差を持ち、上記各ロータ7の回転に伴
つてケーシング6内を3つの作動室9,9,9に
区画して、各々の気筒1A,1Bにおいて上記
180゜の位相差でもつて吸気、圧縮、爆発、膨張お
よび排気の各行程を順次行うものである。尚、1
0は各気筒1A,1Bにおいてロータハウジング
2に設けられた排気ポート、11および12はリ
ーデイング側およびトレーリング側点火プラグ、
13はロータ7の側面に装着されたサイドシー
ル、14はロータ7の各頂部に装着されたアペツ
クスシール、15はロータ7の各頂部両側面に装
着されたコーナシールである。
In Figures 1 and 2, 1A and 1B
are the first and second cylinders in a two-system side intake port type two-cylinder rotary piston engine, one for low load and one for high load.
A and 1B each have a two-section trochoidal inner peripheral surface 2a.
The rotor housing 2 includes a low-load intake port 3 and a high-load intake port 4 located on both sides of the rotor housing 2, in which low-load intake passages 20a, 20b and high-load intake passages 21a, 21b, which will be described later, open respectively. A substantially triangular rotor 7 is supported by a single eccentric shaft 8 and rotates planetarily within a casing 6 formed by side housings 5, 5, and rotors 7, 7 of each cylinder 1A, 1B. is the rotation angle of eccentric shaft 8.
With a phase difference of 180 degrees, the inside of the casing 6 is divided into three working chambers 9, 9, 9 as each rotor 7 rotates, and the above-mentioned
The intake, compression, explosion, expansion, and exhaust strokes are performed sequentially with a phase difference of 180°. Furthermore, 1
0 is an exhaust port provided in the rotor housing 2 in each cylinder 1A, 1B, 11 and 12 are leading side and trailing side spark plugs,
13 is a side seal attached to the side surface of the rotor 7; 14 is an apex seal attached to each top of the rotor 7; and 15 is a corner seal attached to both sides of each top of the rotor 7.

上記2つのサイドハウジング5,5にそれぞれ
対向して設けられた低負荷用および高負荷用吸気
ポート3,4はロータ7側面によつて実質的に開
閉され、両者の開閉時期は同じであり、各吸気ポ
ート3,4の開口期間θはエキセントリツクシヤ
フト8の回転角で270〜320゜の範囲に設定されて
いる。
The low-load and high-load intake ports 3 and 4 provided oppositely in the two side housings 5 and 5 are substantially opened and closed by the side surface of the rotor 7, and the opening and closing timings of both are the same, The opening period θ of each intake port 3, 4 is set within a range of 270 to 320 degrees based on the rotation angle of the eccentric shaft 8.

一方、16は一端がエアクリーナ17を介して
大気に開口して両気筒1A,1Bに吸気を供給す
るための主吸気通路であつて、該主吸気通路16
には、吸入空気量を検出するエアフローメータ1
8が配設されている。上記主吸気通路16はエア
フローメータ18下流において隔壁19によつて
主低負荷用吸気通路20と主高負荷用吸気通路2
1とに仕切られ、該主低負荷用吸気通路20に
は、エンジンの負荷の増大に応じて開作動し所定
負荷以上になると全開となるエンジン低負荷時の
吸入空気量を制御する低負荷用絞り弁22が配設
され、また上記主高負荷用吸気通路21には、エ
ンジン負荷が所定負荷以上になると開作動するエ
ンジン高負荷時の吸入空気量を制御する高負荷用
絞り弁23が配設されている。さらに、上記主低
負荷用吸気通路20は低負荷用絞り弁22下流に
おいて同形状寸法の第1および第2低負荷用吸気
通路20a,20bに分岐されたのち各気筒1
A,1Bの低負荷用吸気ポート3,3を介して作
動室9,9に連通し、また上記主高負荷用吸気通
路21は高負荷用絞り弁23下流において同形状
寸法の第1および第2高負荷用吸気通路21a,
21bに分岐されたのち各気筒1A,1Bの高負
荷用吸気ポート4,4を介して作動室9,9に連
通しており、よつて各気筒1A,1Bに対して、
低負荷用吸気通路20a,20bと高負荷用吸気
通路21a,21bとは低負荷用絞り弁22下流
において各々独立して作動室9に開口するように
構成されている。
On the other hand, 16 is a main intake passage whose one end opens to the atmosphere via an air cleaner 17 to supply intake air to both cylinders 1A and 1B.
is equipped with an air flow meter 1 that detects the amount of intake air.
8 are arranged. The main intake passage 16 is connected to a main low-load intake passage 20 and a main high-load intake passage 2 by a partition wall 19 downstream of the air flow meter 18.
1, and the main low-load intake passage 20 has a low-load intake passage that opens in response to an increase in engine load and fully opens when the load exceeds a predetermined load to control the amount of intake air when the engine is under low load. A throttle valve 22 is disposed, and the main high-load intake passage 21 is provided with a high-load throttle valve 23 that opens when the engine load exceeds a predetermined load and controls the amount of intake air during high engine loads. It is set up. Further, the main low-load intake passage 20 is branched downstream of the low-load throttle valve 22 into first and second low-load intake passages 20a and 20b having the same shape and dimensions, and then, each cylinder 1
The main high-load intake passage 21 communicates with the working chambers 9, 9 through the low-load intake ports 3, 3 of A and 1B, and the main high-load intake passage 21 is connected to the first and second intake passages of the same shape and size downstream of the high-load throttle valve 23. 2 High load intake passage 21a,
21b, and then communicates with the working chambers 9, 9 via the high-load intake ports 4, 4 of each cylinder 1A, 1B, and therefore, for each cylinder 1A, 1B,
The low-load intake passages 20a, 20b and the high-load intake passages 21a, 21b are configured to open independently into the working chamber 9 downstream of the low-load throttle valve 22.

上記各高負荷用吸気通路21a,21bの通路
面積Asは各低負荷用吸気通路20a,20bの
通路面積Apとほぼ等しく(As=Ap)設定され、
また各高負荷用吸気通路21a,21bの通路長
さlsは各低負荷用吸気通路20a,20bの通路
長さlpよりも短かく(ls<lp)設定されており、
高負荷用吸気通路21a,21bの吸気抵抗を小
さくして充填効率向上を有効に行うようにしてい
る。また、上記各低負荷用吸気通路20a,20
bにはそれぞれ上記エアフローメータ18の出力
(吸入空気量)に応じて燃料噴射量が制御される
電磁弁式の燃料噴射ノズル24,24が配設され
ている。
The passage area As of each of the high-load intake passages 21a, 21b is set to be approximately equal to the passage area Ap of each low-load intake passage 20a, 20b (As=Ap),
Further, the passage length ls of each high-load intake passage 21a, 21b is set shorter than the passage length lp of each low-load intake passage 20a, 20b (ls<lp).
The intake resistance of the high-load intake passages 21a and 21b is reduced to effectively improve filling efficiency. In addition, each of the above-mentioned low-load intake passages 20a, 20
Electromagnetic valve type fuel injection nozzles 24, 24 whose fuel injection amount is controlled according to the output (intake air amount) of the air flow meter 18 are respectively disposed at b.

そして、上記主低負荷用吸気通路20の分岐部
は、低負荷用絞り弁22下流に位置して、第1低
負荷用吸気通路20aと第2低負荷用吸気通路2
0bとを連通する連通路25を有する拡大室26
によつて構成されている。上記連通路25の通路
面積Acpは圧力波(排気干渉効果での圧縮波)を
その減衰を小さくして有効に伝達するように第
1、第2低負荷用吸気通路20a,20bの通路
面積Apと同等かそれ以上(Acp≧Ap)に設定さ
れている。また、上記主高負荷用吸気通路21の
分岐部も、同様に第1と第2の高負荷用吸気通路
21aと21bとを連通する連通路27を有する
拡大室28によつて構成されている。尚、上記拡
大室26,28はエンジン加速時又は減速時等の
過渡運転時でのサージタンクとして機能し、加速
時の息付きや減速時の燃料のオーバリツチによる
失火等を防止して良好な燃料応答性を確保するも
のであるとともに、各気筒1A,1Bの低負荷用
および高負荷用吸気ポート3,4による吸気開始
により低負荷用および高負荷用吸気通路20a,
20b,21a,21bが負圧となつて発生する
膨張波を、各吸気通路20a,20b,21a,
21bで独立して上記拡大室26,28で圧縮波
に反転して反射し、該圧縮波を各気筒1A,1B
の各吸気ポート3,4に伝播させて過給を行うよ
うにするものである。
The branch portion of the main low-load intake passage 20 is located downstream of the low-load throttle valve 22, and includes a first low-load intake passage 20a and a second low-load intake passage 2.
An enlarged chamber 26 having a communication path 25 communicating with 0b
It is composed of. The passage area Acp of the communication passage 25 is such that the passage area Ap of the first and second low-load intake passages 20a and 20b is such that pressure waves (compression waves due to exhaust interference effects) are effectively transmitted with less attenuation. is set to be equal to or greater than (Acp≧Ap). Further, the branching portion of the main high-load intake passage 21 is also constituted by an enlarged chamber 28 having a communication passage 27 that communicates the first and second high-load intake passages 21a and 21b. . The expansion chambers 26 and 28 function as surge tanks during transient operations such as when the engine accelerates or decelerates, and prevent misfires caused by breathing during acceleration or fuel overflow during deceleration, thereby ensuring a good fuel supply. In addition to ensuring responsiveness, the low-load and high-load intake passages 20a,
20b, 21a, 21b become negative pressure, and the expansion waves generated are transferred to the respective intake passages 20a, 20b, 21a,
21b independently inverts and reflects the compression wave in the expansion chambers 26 and 28, and the compression wave is transmitted to each cylinder 1A and 1B.
The supercharging is carried out by propagating the air to each of the intake ports 3 and 4.

さらに、上記両気筒1A,1Bの低負荷用吸気
ポート3,3間の通路長さLpは、連通路25の
通路長さlcpと該連通路25下流の第1、第2低
負荷用吸気通路21a,21bの各通路長さls,
lpとを加算したもの(Lp=lcp+2lp)となり、
5000〜7000rpmのエンジン高回転時を基準として
上記()式から、 Lp≒0.57〜1.37(m) に設定されている。
Furthermore, the passage length Lp between the low-load intake ports 3 and 3 of the above-mentioned cylinders 1A and 1B is the passage length lcp of the communication passage 25 and the first and second low-load intake passages downstream of the communication passage 25. Each passage length ls of 21a and 21b,
It is the sum of lp and (Lp = lcp + 2lp),
Based on the above formula (), Lp is set to 0.57 to 1.37 (m) based on the high engine speed of 5000 to 7000 rpm.

尚、第2図中、29は排気ポート10に接続さ
れた排気通路、30は該排気通路29の途中に介
設された触媒装置(図示せず)を補助する排気浄
化用の拡大マニホールドである。
In FIG. 2, 29 is an exhaust passage connected to the exhaust port 10, and 30 is an enlarged manifold for exhaust purification that assists a catalyst device (not shown) interposed in the middle of the exhaust passage 29. .

次に、上記実施例の作用を第3図により説明す
るに、高出力を要する5000〜7000rpm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
低負荷用吸気ポート3開口時に第2低負荷用吸気
通路20b内に発生した圧縮波は、両気筒1A,
1Bの低負荷用吸気ポート3,3間の通路長さ
Lpを5000〜7000rpmのエンジン高回転時を基準
として上記()式により0.57〜1.37mに設定し
たことにより、第2低負荷用吸気通路20b→拡
大室26の連通路25→第1低負荷用吸気通路2
0aを経て、180゜の位相差をもつ第1気筒1Aの
全閉直前の低負荷用吸気ポート3に伝播される。
その結果、この圧縮波により、第1気筒1Aの全
閉直前の低負荷用吸気ポート3からの吸気の吹き
返しが抑制されて吸気が作動室9内に押し込ま
れ、つまり過給が行われることになる。続いて、
第1気筒1Aの低負荷用吸気ポート3開口時に発
生する圧縮波も同様に第2気筒1Bの全閉直前の
低負荷用吸気ポート3に伝播されて過給が行われ
る。以後同様にして、気筒1A、1B相互間の低
負荷吸気系統での排気干渉効果による過給効果に
より、第4図に示すようにエンジン高負荷高回転
時での充填効率が有効に高められて出力向上を効
果的に図ることができる。尚、第4図は、上記連
通路25を遮断して排気干渉効果のない従来例の
場合(破線で示す)に対して、本発明によりエン
ジン高回転時として6000rpmを基準として排気干
渉効果を得た場合(実線で示す)におけるエンジ
ンの出力トルク特性を示す。
Next, to explain the operation of the above embodiment with reference to FIG. 3, when the engine speed is high (5,000 to 7,000 rpm, which requires high output), when one cylinder, for example, the low-load intake port 3 of the second cylinder 1B, is opened, the second The compression wave generated in the load intake passage 20b is generated in both cylinders 1A,
Passage length between low load intake ports 3 and 3 of 1B
By setting Lp to 0.57 to 1.37 m using the above formula () based on the high engine speed of 5000 to 7000 rpm, the second low load intake passage 20b → the communication passage 25 of the enlarged chamber 26 → the first low load intake passage Intake passage 2
0a, it is propagated to the low-load intake port 3 of the first cylinder 1A, which has a phase difference of 180 degrees, just before it is fully closed.
As a result, this compression wave suppresses the blowback of intake air from the low-load intake port 3 immediately before the first cylinder 1A is fully closed, and forces the intake air into the working chamber 9, which results in supercharging. Become. continue,
The compression wave generated when the low-load intake port 3 of the first cylinder 1A is opened is similarly propagated to the low-load intake port 3 of the second cylinder 1B just before it is fully closed, thereby performing supercharging. Thereafter, in the same manner, due to the supercharging effect due to the exhaust interference effect in the low-load intake system between the cylinders 1A and 1B, the charging efficiency is effectively increased when the engine is under high load and high rotation speed, as shown in Fig. 4. Output can be effectively improved. In addition, FIG. 4 shows a case in which the exhaust interference effect is obtained with the present invention at a high engine rotation speed of 6000 rpm as compared to the conventional case (indicated by a broken line) in which there is no exhaust interference effect by blocking the communication passage 25. The output torque characteristics of the engine are shown in the case (shown by the solid line).

その際、上記連通路25は低負荷用絞り弁22
下流に位置し、しかもその通路面積Acpを低負荷
用吸気通路20a,20bの通路面積Apより同
等以上としたので、上記低負荷用絞り弁22や連
通路25自身によつて圧力波(圧縮波)が減衰さ
れることがなく、上記排気干渉効果を有効に発揮
できる。
At that time, the communication path 25 is connected to the low load throttle valve 22.
It is located downstream, and its passage area Acp is equal to or larger than the passage area Ap of the low-load intake passages 20a and 20b, so the low-load throttle valve 22 and the communication passage 25 themselves generate pressure waves (compression waves) ) is not attenuated, and the above exhaust interference effect can be effectively exhibited.

また、上記排気干渉効果による過給効果は、低
負荷用吸気ポート3の開口期間、第1低負荷用吸
気通路20aと第2低負荷用吸気通路20bとを
連通する連通路25の位置、および両気筒1A,
1Bの低負荷用吸気ポート3,3間の通路長さ
Lpを上述の如く設定することによつて得られ、
過給機等を要さないので、既存の吸気系の僅かな
設計変更で済み、構造が極めて簡単なものであ
り、よつて容易にかつ安価に実施できる。
Further, the supercharging effect due to the exhaust interference effect depends on the opening period of the low-load intake port 3, the position of the communication passage 25 that communicates the first low-load intake passage 20a and the second low-load intake passage 20b, and Both cylinders 1A,
Passage length between low load intake ports 3 and 3 of 1B
Obtained by setting Lp as above,
Since a supercharger or the like is not required, only slight design changes to the existing intake system are required, and the structure is extremely simple, so it can be implemented easily and at low cost.

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5000〜7000rpmのエ
ンジン高回転時、低負荷用吸気系統で排気干渉効
果を得て出力向上を図るようにしたが、両気筒1
A,1Bの高負荷用吸気ポート4,4間の通路長
さLsを上記()式により0.57〜1.37mに設定す
ることにより高負荷用吸気系統で排気干渉効果を
得るようにしてもよい。また両吸気系統で共に排
気干渉効果を得るようにしてもよく、この場合、
2重の排気干渉効果により出力向上を図ることが
できる。
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, when the engine rotates at a high speed of 5,000 to 7,000 rpm, the low-load intake system is used to obtain an exhaust interference effect to improve output.
The exhaust interference effect may be obtained in the high-load intake system by setting the passage length Ls between the high-load intake ports 4, 4 of A and 1B to 0.57 to 1.37 m using the above equation (). Also, both intake systems may have an exhaust interference effect; in this case,
The output can be improved by the double exhaust interference effect.

また、上記実施例の如く低負荷用吸気系統で
5000〜7000rpmのエンジン高回転時に排気干渉効
果を得るように設定する一方、高負荷用吸気系統
において、上記基準回転数(5000〜7000rpm)よ
り1000rpm以上低回転側で排気干渉効果を得るよ
うに設定してもよく、エンジンの中回転域から高
回転域に亘つて出力向上を図ることができる。こ
の場合、例えば3000〜5000rpmで排気干渉効果を
得るには両気筒の高負荷用吸気ポート間の通路長
さLsを上記()式よりLs=0.82〜2.29mの範囲
内に設定すればよい。
In addition, in a low-load intake system as in the above example,
The exhaust interference effect is set to be obtained at high engine speeds of 5000 to 7000 rpm, while the exhaust interference effect is set to be obtained at 1000 rpm or more lower than the above reference rotation speed (5000 to 7000 rpm) in the high-load intake system. It is also possible to improve the output from the medium speed range to the high speed range of the engine. In this case, in order to obtain the exhaust interference effect at, for example, 3000 to 5000 rpm, the passage length Ls between the high-load intake ports of both cylinders may be set within the range of Ls = 0.82 to 2.29 m from the above equation ().

また、吸気ポート閉口時には吸気の慣性により
吸気が圧縮されて圧縮波が吸気通路内の吸気ポー
ト部分に発生する。この閉口時圧縮波を他方の気
筒の全閉直前の吸気ポートに作用せしめれば過給
効果が得られる(以下、吸気慣性効果と呼ぶ)の
で、5000〜7000rpmのエンジン高回転時、一方の
吸気系統で上記の如き排気干渉効果を得る一方、
他方の吸気系統で第3図破線で示すように上記吸
気慣性効果を得るように設定してもよく、エンジ
ン高負荷高回転時の出力向上を大巾に図ることが
できる。この場合、吸気慣性効果を得るための通
路長さLは、 L=(180−θ1)×(60/360N)×a (θ1:無効期間で約20゜、その他は上記()式
と同様)の式から、L=1.31〜1.83mの範囲内に
設定すればよい。
Furthermore, when the intake port is closed, the intake air is compressed by the inertia of the intake air, and a compression wave is generated at the intake port portion in the intake passage. By applying this closing compression wave to the intake port of the other cylinder just before it is fully closed, a supercharging effect can be obtained (hereinafter referred to as the intake inertia effect). While obtaining the above exhaust interference effect in the system,
The other intake system may be set to obtain the above-mentioned intake inertia effect as shown by the broken line in FIG. 3, and the output can be greatly improved when the engine is under high load and at high speed. In this case, the passage length L to obtain the intake inertia effect is L = (180 - θ 1 ) x (60/360N) x a (θ 1 : about 20° in the invalid period, other than the above formula ()) From the equation (similar), L should be set within the range of 1.31 to 1.83 m.

また、上記実施例では、各吸気ポート3,4を
開口期間が固定の固定ポートで構成し、その開口
期間を270〜320゜としたが、開口期間が290゜以上
になると、エンジン低回転時、吸気の吹き返しが
生じるので、それを防止するために、吸気ポート
を制御弁によつて開口期間が変化する可変ポート
で構成し、エンジン高負荷高回転時のみにその開
口期間が270〜320゜となるようにすることが好ま
しい。
In addition, in the above embodiment, each intake port 3, 4 is configured as a fixed port with a fixed opening period, and the opening period is 270 to 320 degrees, but if the opening period becomes 290 degrees or more, In order to prevent intake air from blowing back, the intake port is configured with a variable port whose opening period is changed by a control valve, and the opening period is 270 to 320 degrees only when the engine is under high load and at high speeds. It is preferable to do so.

さらに、上記実施例では、低負荷用および高負
荷用吸気ポート3,4の開閉時期を同じにした
が、必要に応じてずらしてもよく、例えば排気干
渉効果を得る側の吸気ポートの開時期を早めるよ
うにすれば、開口時圧縮波が強く発生でき、排気
干渉効果を増大できるので好ましい。
Further, in the above embodiment, the opening and closing timings of the low-load and high-load intake ports 3 and 4 are made the same, but they may be shifted as necessary. For example, the opening timing of the intake port on the side that obtains the exhaust interference effect may be shifted. It is preferable to speed up the opening because it can generate a strong compression wave at the time of opening and increase the exhaust interference effect.

また、吸排気オーバラツプ期間はエキセントリ
ツクシヤフトの回転角で0〜20゜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、ダイ
リユーシヨンガスの持込み量を少なくして特にエ
ンジン低負荷時の失火の防止を図る上で好まし
い。
In addition, setting the intake/exhaust overlap period to a range of 0 to 20 degrees based on the rotation angle of the eccentric shaft improves charging efficiency and reduces the amount of dilution gas brought in, especially when the engine is under low load. This is preferable in order to prevent misfires.

さらに、上記実施例では低負荷用絞り弁22を
主低負荷用吸気通路20内に設けた型式のものに
ついて述べたが、低負荷用絞り弁22を、主低負
荷用吸気通路20と主高負荷用吸気通路21との
分岐部上流の主吸気通路16に設けた型式のもの
も採用可能である。
Further, in the above embodiment, the low load throttle valve 22 is provided in the main low load intake passage 20, but the low load throttle valve 22 is arranged between the main low load intake passage 20 and the main low load intake passage 20. A type provided in the main intake passage 16 upstream of the branching portion with the load intake passage 21 may also be adopted.

以上説明したように、本発明によれば、低負荷
用と高負荷用との2系統のサイド吸気ポート式の
2気筒ロータリピストンエンジンにおいて、5000
〜7000rpmのエンジン高回転時、少なくとも一方
の吸気系統での気筒相互間の排気干渉効果により
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
簡単な構成でもつて、エンジンの高負荷高回転時
での充填効率を高めて出力向上を有効に図ること
ができ、よつてロータリピストンエンジンの出力
向上対策の容易実施化およびコストダウン化に大
いに寄与できるものである。
As explained above, according to the present invention, in a side intake port type two-cylinder rotary piston engine with two systems for low load and high load, 5000
At high engine speeds of ~7000rpm, the supercharging effect is achieved through the exhaust interference effect between cylinders in at least one intake system, so there is no need for a supercharger, etc., and the design of the existing intake system can be simplified. Even with an extremely simple configuration through modification, it is possible to effectively improve output by increasing charging efficiency when the engine is under high load and high rotation, thereby making it easier to implement measures to improve the output of rotary piston engines and reducing costs. It can greatly contribute to

【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図は全体構
成説明図、第2図は全体概略図、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図である。 1A……第1気筒、1B……第2気筒、2……
ロータハウジング、2a……2節トロコイド状内
周面、3……低負荷用吸気ポート、4……高負荷
用吸気ポート、5……サイドハウジング、6……
ケーシング、7……ロータ、8……エキセントリ
ツクシヤフト、9……作動室、20……主低負荷
用吸気通路、20a……第1低負荷用吸気通路、
20b……第2低負荷用吸気通路、21……主高
負荷用吸気通路、21a……第1高負荷用吸気通
路、21b……第2高負荷用吸気通路、22……
低負荷用絞り弁、23……高負荷用絞り弁、25
……連通路。
The drawings show an embodiment of the present invention; FIG. 1 is an explanatory diagram of the overall configuration, FIG. 2 is an overall schematic 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 structure. FIG. 3 is a diagram showing output torque characteristics according to the invention. 1A...1st cylinder, 1B...2nd cylinder, 2...
Rotor housing, 2a...Two-section trochoidal inner peripheral surface, 3...Intake port for low load, 4...Intake port for high load, 5...Side housing, 6...
Casing, 7... Rotor, 8... Eccentric shaft, 9... Working chamber, 20... Main low load intake passage, 20a... First low load intake passage,
20b...Second low load intake passage, 21...Main high load intake passage, 21a...First high load intake passage, 21b...Second high load intake passage, 22...
Throttle valve for low load, 23... Throttle valve for high load, 25
...Communication path.

Claims (1)

【特許請求の範囲】 1 2節トロコイド状の内周面を有するロータハ
ウジングとその両側に位置するサイドハウジング
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ツクシヤフトに支承されて遊
星回転運動し、かつ低負荷用絞り弁を備えた低負
荷用吸気通路と高負荷用絞り弁を備えた高負荷用
吸気通路とが各々独立して各サイドハウジングに
設けた低負荷用および高負荷用吸気ポートによつ
て作動室に開口するものであつて、各ロータがエ
キセントリツクシヤフトの回転角で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 各吸気ポートの開口期間をエキセントリツク
シヤフトの回転角で270〜320゜の範囲内に設定
すること、 b 各気筒の低負荷用および高負荷用吸気通路の
少なくとも一方の吸気通路を絞り弁下流におい
て連通路によつて連通すること、 c 該連通路およびその下流の吸気通路によつて
形成される両気筒の吸気ポート間の通路長さ
を、5000〜7000rpmのエンジン高回転時、一方
の気筒の吸気ポート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他方の気筒の
全閉直前の吸気ポートに伝播させて過給を行う
ように0.57〜1.37mの範囲内に設定すること を特徴とするロータリピストンエンジンの吸気装
置。
[Claims] 1. A substantially triangular rotor is supported by an eccentric shaft in a casing formed by a rotor housing having a two-bar trochoidal inner circumferential surface and side housings located on both sides of the rotor housing. A low-load intake passage and a high-load intake passage that rotate and are equipped with a low-load throttle valve and a high-load intake passage equipped with a high-load throttle valve are independently provided in each side housing. In a two-cylinder rotary piston engine that opens into the working chamber through an intake port, and each rotor has a phase difference of 180° at the rotation angle of the eccentric shaft, a. The rotation angle of the shaft is set within the range of 270 to 320 degrees; b. At least one of the low-load and high-load intake passages of each cylinder is communicated with each other by a communication passage downstream of the throttle valve; c. The length of the passage between the intake ports of both cylinders formed by the communication passage and the intake passage downstream of it is determined by the length of the passage formed in the intake passage when the intake port of one cylinder is opened at high engine speeds of 5000 to 7000 rpm. The intake air of a rotary piston engine is set within a range of 0.57 to 1.37 m so that a compression wave is propagated through the communication passage to the intake port of the other cylinder just before fully closing to perform supercharging. Device.
JP57208149A 1982-11-27 1982-11-27 Intake apparatus for rotary piston engine Granted JPS5999031A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP57208149A JPS5999031A (en) 1982-11-27 1982-11-27 Intake apparatus for rotary piston engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP57208149A JPS5999031A (en) 1982-11-27 1982-11-27 Intake apparatus for rotary piston engine

Publications (2)

Publication Number Publication Date
JPS5999031A JPS5999031A (en) 1984-06-07
JPS6340251B2 true JPS6340251B2 (en) 1988-08-10

Family

ID=16551447

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57208149A Granted JPS5999031A (en) 1982-11-27 1982-11-27 Intake apparatus for rotary piston engine

Country Status (1)

Country Link
JP (1) JPS5999031A (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010234406A (en) * 2009-03-31 2010-10-21 Sc Pipe Solutions Co Ltd Pipe processing method

Also Published As

Publication number Publication date
JPS5999031A (en) 1984-06-07

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