JPH0337010B2 - - Google Patents
Info
- Publication number
- JPH0337010B2 JPH0337010B2 JP57212429A JP21242982A JPH0337010B2 JP H0337010 B2 JPH0337010 B2 JP H0337010B2 JP 57212429 A JP57212429 A JP 57212429A JP 21242982 A JP21242982 A JP 21242982A JP H0337010 B2 JPH0337010 B2 JP H0337010B2
- Authority
- JP
- Japan
- Prior art keywords
- load
- intake
- low
- passage
- 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 - Lifetime
Links
- 230000006835 compression Effects 0.000 claims description 30
- 238000007906 compression Methods 0.000 claims description 30
- 230000010349 pulsation Effects 0.000 claims description 30
- 238000004891 communication Methods 0.000 claims description 16
- 230000000644 propagated effect Effects 0.000 claims description 5
- 230000000694 effects Effects 0.000 description 64
- 230000002093 peripheral effect Effects 0.000 description 6
- 239000000446 fuel Substances 0.000 description 4
- 230000003111 delayed effect Effects 0.000 description 3
- 238000013461 design Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000002347 injection Methods 0.000 description 3
- 239000007924 injection Substances 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 239000003054 catalyst Substances 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 238000004880 explosion Methods 0.000 description 2
- 238000000746 purification Methods 0.000 description 2
- 230000004044 response Effects 0.000 description 2
- 238000011144 upstream manufacturing Methods 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 230000002238 attenuated effect Effects 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 238000010790 dilution Methods 0.000 description 1
- 239000012895 dilution Substances 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000002441 reversible effect Effects 0.000 description 1
- 238000004904 shortening Methods 0.000 description 1
- 230000001052 transient effect Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
- F02B53/04—Charge admission or combustion-gas discharge
- F02B53/08—Charging, e.g. by means of rotary-piston pump
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- 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の2系統
の独立した吸気通路を備えた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
の中回転域から高回転域に亘つて過給効果を得る
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, to a side intake port type two-cylinder rotary piston engine having two independent intake passages for low load and high load. This invention relates to an engine that uses intake pressure waves generated in an intake passage to obtain a supercharging effect from a medium rotation range to a high rotation range of an engine.
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
れたケーシング内にそれぞれ配設された略三角形
状のロータが、エキセントリツクシヤフトに支承
され該シヤフトの回転角で180゜の位相差を持つて
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上記低負
荷用吸気通路よりも通路面積の大きい高負荷用吸
気通路とが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、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
程を順次行うものである。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
て通路面積の狭い低負荷用吸気通路のみから吸気
を供給することにより、吸気流速を速めて燃焼安
定性を向上させる一方、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であ
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。 Generally, such a two-system side intake port type two-cylinder rotary piston engine is arranged in a casing formed by a rotor housing having a two-section trochoidal inner peripheral surface and side housings located on both sides of the rotor housing. A substantially triangular rotor is supported on an eccentric shaft and rotates planetarily with a phase difference of 180 degrees at the rotation angle of the shaft, and a low-load intake passage is provided with a low-load throttle valve. A high-load intake passage, which is equipped with a high-load throttle valve and has a larger passage area than the low-load intake passage; The high-load intake port opens into the working chamber, and while maintaining the above 180° phase difference between both cylinders, each cylinder receives intake, compression, explosion, expansion, and exhaust air as the rotor rotates. The steps are performed sequentially. 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, which has a narrow passage area, thereby increasing the intake flow rate and improving combustion stability. When the engine is under high load, the so-called dual induction system is designed to open the high-load throttle valve and supply intake air from the high-load intake passage as well, thereby increasing charging efficiency and increasing output. It is called. 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) 吸気ポートの吸気開始により吸気通路内に膨
張波が発生すること
を知見した。このことから、一方の気筒での上記
(i)の閉口時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
しめれば効果的にに過給効果が得られること(以
下、吸気干渉効果という)および各気筒での上記
(ii)の膨張波を圧縮波に反転させて該各気筒の全閉
直前の吸気ポートに作用せしめれば過給効果が得
られること(以下、吸気個有脈動効果という)を
見い出したのである。そのうち、上記排気干渉効
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エンジン排圧が高
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 are generated in the intake port area, and (ii) expansion waves are generated in the intake passage when the intake port starts inhaling. From this, the above for one cylinder
A supercharging effect can be effectively obtained by applying the closing compression wave of (i) to the intake port of the other cylinder, especially just before fully closing, where the intake air blowback occurs (hereinafter referred to as intake interference effect). and the above for each cylinder
We discovered that a supercharging effect can be obtained by inverting the expansion wave (ii) into a compression wave and applying it to the intake port of each cylinder just before it is fully closed (hereinafter referred to as the intake-specific pulsation effect). . Among these, the above-mentioned exhaust interference effect is remarkable because, as mentioned above, in recent years, engine exhaust pressure has been increased due to the installation of catalyst devices for exhaust purification in engine exhaust systems.
そして、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
は、上記排気干渉効果および吸気個有脈動効果を
得るに当つて、高負荷用吸気通路と低負荷用吸気
通路との各々独立した2系統の吸気通路を有する
ことから、各々の吸気系統で上記効果を得ること
ができる。そのうち、高負荷用吸気通路は低負荷
用吸気通路よりも通路面積が大きいことから、圧
力波を可及的に減衰させることなく伝播できて上
記効果を有効に発揮できるので、高出力を要する
エンジン高負荷用回転時に高負荷用吸気系統で過
給効果の強い排気干渉効果を得ることが効果的で
あり、低負荷用吸気系統で吸気個有脈動効果をエ
ンジン中回転域に得ることが好ましい。 In the two-system side intake port type two-cylinder rotary piston engine as described above, in order to obtain the above-mentioned exhaust interference effect and intake unique pulsation effect, the high-load intake passage and the low-load intake passage are Since there are two independent intake passages, each intake system can achieve the above effects. Among them, the intake passage for high loads has a larger passage area than the intake passage for low loads, so pressure waves can be propagated without attenuation as much as possible, and the above effect can be effectively exerted, so it is suitable for engines that require high output. It is effective to obtain an exhaust interference effect with a strong supercharging effect in the high-load intake system during high-load rotation, and it is preferable to obtain an intake-specific pulsation effect in the engine mid-speed range in the low-load intake system.
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
開口しているので上記の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、本発明の目的は、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、高負荷用および低負荷用吸気
ポートの各開口期間、各吸気の高負荷用吸気通路
同志を連通する連通路の位置および低負荷用吸気
通路内に発生した膨張波を圧縮波に反転するため
の拡大室の位置、並びに両気筒の高負荷用吸気ポ
ート間の通路長さおよび上記拡大室から低負荷用
吸気ポートまでの通路長さを適切に設定すること
により、高出力を要する5000〜7000rpmのエンジ
ン高回転時、高負荷用吸気統での排気干渉効果に
より過給効果を得るとともに、それよりも低回転
側で低負荷用吸気系統での吸気個有脈動効果によ
り過給効果を得、よつて過給機等を用いることな
く既存の吸気系の僅かな設計変更による簡単な構
成によつてエンジンの中回転域から高回転域に亘
つて充填効率を高めて出力向上を有効に図らんと
するものである。 That is, an object of the present invention is to provide a two-system side intake port type two-cylinder rotary piston engine as described above, in which the high-load intake passages of each intake are connected to each other during each opening period of the high-load and low-load intake ports. The position of the communicating passage, the position of the expansion chamber for reversing the expansion wave generated in the low-load intake passage into a compression wave, the length of the passage between the high-load intake ports of both cylinders, and the distance from the expansion chamber to the high-load intake port of both cylinders. By appropriately setting the passage length to the low-load intake port, at high engine speeds of 5000 to 7000 rpm, which require high output, a supercharging effect can be obtained through the exhaust interference effect in the high-load intake system, and the The supercharging effect is obtained by the intake pulsation effect in the low-load intake system on the lower rotation side than the engine speed, and therefore, it is possible to achieve a supercharging effect by simply changing the design of the existing intake system without using a supercharger etc. Therefore, it is an attempt to effectively improve the output by increasing the charging efficiency from the medium rotation range to the high rotation range of the engine.
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
成される各ケーシング内にそれぞれ配設された略
三角形状のロータが、エキセントリツクシヤフト
に支承され該シヤフトの回転角で180゜の位相差を
持つて遊星回転運動し、かつ低負荷用吸気通路と
上記低負荷用吸気通路よりも通路面積の大きい高
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
とによつて作動室に開口する2気筒ロータリピス
トンエンジンにおいて、
a 高負荷用吸気ポートの開口期間θs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 低負荷用吸気ポートの開口期間θpをエキセ
ントリツクシヤフトの回転角で230〜290゜の範
囲内に設定すること、
c 各気筒の高負荷用吸気通路を絞り弁下流にお
いて連通路で連通すること、
d 各気筒の低負荷用吸気通路の絞り弁下流に拡
大室を設けること、
e 上記連通路およびその下流の高負荷用吸気通
路によつて形成される両気筒の高負荷用吸気ポ
ート間の通路長さLsを、5000〜7000rpmのエン
ジン高回転時、一方の気筒の高負荷用吸気ポー
ト開口時に高負荷用吸気通路内に発生する開口
時圧縮波を上記高負荷用連通路を介して他方の
気筒の全閉直前の高負荷用吸気ポートに伝播さ
せるように0.57〜1.37mの範囲内に設定するこ
と、
f 上記拡大室から低負荷用吸気ポートまでの低
負荷用吸気通路の通路長さlpを、上記5000〜
7000rpmの間で設定された回転数よりも
1000rpm以上低回転側の3500〜5000rpmのエン
ジン中回転時、各気筒の低負荷用吸気ポートの
吸気開始により低負荷用吸気通路内に発生する
膨張波を上記拡大室で反転して反射した圧縮波
の2次脈動波を各気筒の全閉直前の低負荷用吸
気ポートに伝播させるように0.37〜0.78mの範
囲内に設定すること
の条件のもとで、各気筒の全閉直前の低負荷用お
よび高負荷用吸気ポートにそれぞれ伝播した圧縮
波により過給を行うようにし、よつて高負荷用吸
気系統におけるエンジン高回転時の排気干渉効果
および低負荷用吸気系統におけるエンジン中回転
時の吸気個有脈動効果によりエンジン中回転域か
ら高回転域に亘つ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 disposed in each casing, which is formed by a rotor housing having a nodular trochoidal inner circumferential surface and side housings located on both sides of the rotor housing, and is supported by an eccentric shaft, and the rotation of the shaft is supported by an eccentric shaft. A low-load intake passage and a high-load intake passage having a larger passage area than the low-load intake passage are independently provided in each side housing, and each side housing has a planetary rotation movement with a phase difference of 180° at the corner. In a two-cylinder rotary piston engine that opens into the working chamber through a low-load intake port and a high-load intake port, (b) Set the opening period θp of the low-load intake port within the range of 230 to 290 degrees in rotation angle of the eccentric shaft; (c) Set the high-load intake passage of each cylinder downstream of the throttle valve. (d) providing an enlarged chamber downstream of the throttle valve in the low-load intake passage of each cylinder; (e) increasing the height of both cylinders formed by the above-mentioned communication passage and the high-load intake passage downstream thereof; The passage length Ls between the load intake ports is determined by the compression wave generated in the high-load intake passage when the high-load intake port of one cylinder is opened at high engine speeds of 5000 to 7000 rpm. Set within the range of 0.57 to 1.37 m so that the high-load intake port of the other cylinder is propagated through the communication passage to the high-load intake port just before fully closing. The passage length of the intake passage is 5000~
than the set rotation speed between 7000rpm
When the engine rotates at medium speeds of 3,500 to 5,000 rpm on the low-speed side of 1,000 rpm or more, the expansion wave generated in the low-load intake passage by the start of intake at the low-load intake port of each cylinder is reversed and reflected by the expansion chamber, resulting in a compression wave. Under the condition that the secondary pulsation wave of each cylinder is set within the range of 0.37 to 0.78 m to propagate to the low-load intake port immediately before fully closing each cylinder, Supercharging is performed by compression waves that propagate to the intake ports for high-load and high-load intakes, thereby reducing the exhaust interference effect at high engine speeds in the high-load intake system and the intake air at medium engine speeds in the low-load intake system. The unique pulsation effect effectively increases the charging efficiency from the middle to high engine speed range.
ここにおいて、上記高負荷用吸気系統で排気干
渉効果を得るエンジン高回転時としての5000〜
7000rpmの基準回転数Nh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
領域であることに依る。また、低負荷用吸気系統
で吸気個有脈動効果を得るエンジン中回転時とし
ての3500〜5000rpmの回転数Nlの設定は、一般
に最大トルクがこの範囲に設定されていること、
また低回転域では脈動による過給効果も得にくい
こと、さらに上記基準回転数Nhで排気干渉効果
を得た場合、その効果(過給効果)は基準回転数
Nhを中心にNnよりも1000rpm高低回転側に及ぶ
ので、上記基準回転数Nhよりも少なくとも
1000rp以上低回転側(Nl≦Nh−1000rpm)で吸
気個有脈動効果を得ることが全体的に出力向上を
図ることができることに依る。 Here, 5000 ~
The limitation of the standard rotational speed Nh to 7000 rpm is because the maximum output and maximum speed are generally set within this range, so the engine is in the high load, high rotation range and requires high output, and is therefore useful for improving charging efficiency and output. It depends on being a valid area. In addition, the setting of the rotation speed Nl of 3500 to 5000 rpm during engine mid-speed to obtain the intake individual pulsation effect in a low-load intake system generally requires that the maximum torque is set within this range.
In addition, it is difficult to obtain a supercharging effect due to pulsation in the low rotation range, and furthermore, if the exhaust interference effect is obtained at the reference rotation speed Nh, the effect (supercharging effect) will be lower than the reference rotation speed.
Centered on Nh, it extends to 1000 rpm higher and lower rotation than Nn, so it is at least higher than the reference rotation speed Nh above.
Obtaining the intake-specific pulsation effect on the low rotation side (Nl≦Nh−1000rpm) above 1000rp makes it possible to improve the overall output.
また、上記設定事項aでの高負荷用吸気ポート
の開口期間θs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ので、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 θs of the high-load intake port in setting item a above is 320° to prevent communication between the preceding working chamber and the following working chamber via the side intake port. , the opening period due to the side seal is approximately 40° larger than the actual opening period due to the rotor side surface, and it is necessary to provide an interval of 40° or more in order to avoid this side seal opening period lapping, so the opening period less than this is required. By suppressing the opening period, communication between the intake working chamber and the subsequent exhaust working chamber is prevented 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. This prevents exhaust gas from entering the intake working chamber during low engine speeds and low loads, such as when idling, thereby ensuring stable combustion. On the other hand, the lower limit of 270° is
This is the minimum period of the geometric intake stroke from intake top dead center (TDC) to bottom dead center (BDC), and in order to perform effective intake, it is necessary to set at least the opening period longer than this. .
この高負荷用吸気ポートの開閉時期の設定にあ
たつては、開時期を上死点よりも、また、閉時期
を下死点よりも遅らせる必要がある。これは、高
負荷用吸気ポートが主として受け持つ高回転域で
は吸入空気量の慣性によつて幾何学的な吸気行程
の効果が遅れ側にずれること、加えて、サイド吸
気ポートではその開時期を上死点側に近ずけると
サイドシールの回転側先端がポートに落ち込むた
め上死点後約30゜以降に設定しなければならない
ことによつている。 When setting the opening/closing timing of this high-load intake port, the opening timing must be delayed from the top dead center, and the closing timing must be delayed from the bottom dead center. This is because the effect of the geometrical intake stroke is delayed due to the inertia of the intake air amount in the high rotation range, which is mainly handled by the high-load intake ports, and in addition, the opening timing of the side intake ports is increased. This is because the tip of the rotating side of the side seal falls into the port as it approaches the dead center, so it must be set at about 30 degrees or more after the top dead center.
これに対し、低負荷用吸気ポートは、吸入空気
量が少なく慣性が小さい低回転域を主に受け持つ
ため、閉時期を下死点後約50゜以前にし吸気の吹
き返しを防ぐ一方、少なくともその開口期間を
230゜以上とることによつて必要な吸気の確保を行
う必要がある。従つて、低負荷用吸気ポートの開
口期間θpは、設定事項bのように230〜290゜に設
定される。 On the other hand, low-load intake ports are mainly responsible for the low-speed range where the amount of intake air is small and the inertia is small. period
It is necessary to secure the necessary intake air by setting the angle to 230° or more. Therefore, the opening period θp of the low-load intake port is set to 230 to 290 degrees as in setting item b.
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中・高
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 on the outside of the side seal has no substantial effect on the generation and propagation of effective pressure waves in the medium and high rotation ranges, which is the problem of the present invention.
また、上記設定事項cでの連通路および上記設
定事項dでの拡大室の絞り弁下流位置設定は、高
負荷用および低負荷用絞り弁の存在が圧力波の伝
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, the downstream position of the throttle valve of the communication path in the above setting item c and the expansion chamber in the expansion chamber in the above setting item d should be adjusted because the presence of the high load and low load throttle valves acts as resistance to the propagation of pressure waves. This is to avoid this, and to reduce the attenuation of the pressure waves so that they can propagate effectively.
さらに、上記設定事項eでの両気筒の高負荷用
吸気ポート間の通路長さLsは、エンジン回転数
が5000〜7000rpmの基準回転数Nhのときに排気
干渉効果を効果的に得るように設定されたもの
で、
Ls=(θs−180−θ0)
×(60/360Nh)
×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、θsは高負荷用吸気ポート開口期間で、
θs=270〜320゜であり、180゜は両気筒の位相差であ
り、またθ0は高負荷用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高
負荷用吸気ポート全閉直前の時期から全閉までの
期間とを合算した無効期間で、θ0≒20゜であり、
よつて(θs−180−θ0)は一方の気筒での開口時
圧縮波発生から他方の気筒の高負荷用吸気ポート
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、60/360Nh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、Ls
=0.57〜1.37mとなる。 Furthermore, the passage length Ls between the high-load intake ports of both cylinders in the setting e above is set to effectively obtain the exhaust interference effect when the engine speed is a reference rotation speed Nh of 5000 to 7000 rpm. This is the value obtained from the formula Ls=(θs−180−θ 0 )×(60/360Nh)×a (). That is, in the above formula, θs is the high-load intake port opening period,
θs = 270 to 320°, 180° is the phase difference between both cylinders, and θ 0 is the period from the opening of the high-load intake port until the compression wave is substantially generated at the time of opening, and the period for effective supercharging. θ 0 ≒ 20°, which is the ineffective period that is the sum of the period immediately before fully closing and the period immediately before fully closing the high-load intake port in which the opening compression wave is propagated in order to carry out this process.
Therefore, (θs-180-θ 0 ) represents the rotation angle of the eccentric shaft required from generation of the compression wave at opening in one cylinder to propagation to the high-load intake port of the other cylinder. Also, 60/360Nh represents the time (seconds) required to rotate 1°. 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, Ls
= 0.57 to 1.37m.
さらにまた、上記設定事項fでの拡大室と各気
筒の低負荷用吸気ポートとの間の通路長さlpは、
エンジン回転数が上記基準回転数Nh(5000〜
7000rpm)よりも1000rpm以上低回転側の3500〜
5000rpmのときに吸気個有脈動効果を効果的に得
るように設定されたもので、
lp=(θp−θl)×(60/360Nl)
×a×1/4 ……()
の式から求められた値である。すなわち、上記式
において、低負荷用吸気ポート開口期間θp=230
〜290゜であり、低負荷用吸気ポート開口から膨張
波が実質的に発生するまでの期間と効果的に過給
を行うために該膨張波を反転した圧縮波の2次脈
動波を伝播させる低負荷用吸気ポート全閉直前の
時期から全閉までの期間とを合算した無効期間で
あつて、θ1≒100゜であり、よつて(θp−θl)は膨
張波発生から圧縮波の2次脈動波伝播でに要する
エキセントリツクシヤフトの回転角度を表わす。
また、エンジン回転数Nl=3500〜5000rpmで、6
0/360ONlは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a=343m/s
(20℃で)である。さらに、1/4は脈動波の2次脈
動を利用するので2次脈動が2往復する行程の逆
数を表わす。よつて、これらの値から、lp=0,
37〜0.78mとなる。 Furthermore, the passage length lp between the expansion chamber and the low-load intake port of each cylinder in the above setting f is:
If the engine rotation speed is the above reference rotation speed Nh (5000~
7000rpm) 1000rpm or more on the low rotation side 3500~
It is set to effectively obtain the unique intake pulsation effect at 5000 rpm, and is calculated from the formula: lp = (θp - θl) x (60/360Nl) x a x 1/4 ... () This is the value. That is, in the above formula, the low load intake port opening period θp = 230
~290°, and propagates the secondary pulsating wave of the compression wave, which is the inversion of the expansion wave, in order to effectively supercharge the period from the opening of the low-load intake port until the expansion wave is substantially generated. This is the invalid period, which is the sum of the period immediately before fully closing the low-load intake port and the period when it is fully closed. It represents the rotation angle of the eccentric shaft required for the next pulsating wave propagation.
Also, at engine speed Nl = 3500 to 5000 rpm, 6
0/360 ONl represents the time (seconds) required to rotate 1°. Also, the propagation speed of pressure wave a = 343 m/s
(at 20℃). Furthermore, since 1/4 uses the secondary pulsation of the pulsating wave, it represents the reciprocal of the stroke in which the secondary pulsation goes back and forth twice. Therefore, from these values, lp=0,
It will be 37 to 0.78m.
尚、ここで、本発明において、吸気個有脈動効
果を得るに当つて2次脈動を用いる理由は、1次
脈動は上記効果が大である反面、通路長さlpが長
くなりすぎ、2次脈動の場合に対して2倍の長さ
となるので車載性が悪く、また吸気抵抗を増加さ
せる傾向がある。一方、3次脈動は通路長さlpが
2次脈動に対して2/3の長さに短かくなる反面、
2次脈動に対して上記効果が約15〜25%程度低下
し、また吸気抵抗がさほど変わらない。このこと
から、通路長さlpを可及的に短くしながら吸気個
有脈動効果を有効に発揮させるためである。 Here, in the present invention, the reason why secondary pulsation is used to obtain the intake-specific pulsation effect is that while primary pulsation has the above-mentioned effect, the passage length lp becomes too long. Since the length is twice as long as in the case of pulsation, it is not easy to install on a vehicle and tends to increase intake resistance. On the other hand, in the case of tertiary pulsation, the path length lp is shortened to 2/3 of that of secondary pulsation, but on the other hand,
The above effect is reduced by about 15 to 25% with respect to secondary pulsation, and the intake resistance does not change much. For this reason, the purpose is to effectively exhibit the intake-specific pulsation effect while shortening the passage length lp as much as possible.
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, in the above equations () and (), the influence of the flow of intake air on the propagation of pressure waves is ignored.
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.
A rotor housing 2 having a rotor housing 2, and 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 provided with , 7 is the rotation angle of the 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.
上記両サイドハウジング5,5に対向して設け
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側面によつて開閉され、高負荷用吸気
ポート4の開口期間θs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お
り、低負荷用吸気ポート3の開口期間θ0は230〜
290゜の範囲に設定されている。また、上記高負荷
用吸気ポート4の開口時期は低負荷用吸気ポート
3の開口時期よりも早めるように設定されてお
り、作動室9からの排気ガスの吹き返しを高負荷
用吸気ポート4側に集中させることにより、高負
荷用吸気ポート4での開口時圧縮波を強く発生さ
せて強い排気干渉効果を得るとともに、低負荷用
吸気ポート3での膨張波を強く発生させて強い吸
気個有脈動効果を得るようにしている。また、高
負荷用吸気ポート4の閉口時期は低負荷用吸気ポ
ート3の閉口時期と同時期もしくは遅らせるよう
に設定されている。 Low-load and high-load intake ports 3 and 4 provided opposite to the above-mentioned both side housings 5 and 5
is opened and closed by the side surface of the rotor 7, and the opening period θs of the high-load intake port 4 is set in the range of 270 to 320 degrees based on the rotation angle of the eccentric shaft 8, and the opening period of the low-load intake port 3 θ 0 is 230~
It is set to a range of 290°. Furthermore, the opening timing of the high-load intake port 4 is set earlier than the opening timing of the low-load intake port 3, so that exhaust gas from the working chamber 9 is blown back to the high-load intake port 4 side. By concentrating them, a strong compression wave is generated at the time of opening at the high-load intake port 4 to obtain a strong exhaust interference effect, and a strong expansion wave is generated at the low-load intake port 3 to create a strong intake pulsation. I'm trying to get an effect. Further, the closing timing of the high-load intake port 4 is set to be the same as or later than the closing timing of the low-load intake port 3.
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の最小
通路面積Asは各低負荷用吸気通路20a,20
bの最小通路面積Apよりも大きく(As>Ap)
設定され、また各高負荷用吸気通路21a,21
bの通路長さlsは各低負荷用吸気通路20a,2
0b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によ
る排気干渉効果での圧縮波の伝播をその減衰を小
さくして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,20b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 minimum passage area As of each of the above-mentioned high-load intake passages 21a, 21b is
Larger than the minimum passage area Ap of b (As>Ap)
and each high-load intake passage 21a, 21
The passage length ls of b is for each low-load intake passage 20a, 2.
It is set shorter than the passage length lp of 0b (ls<lp), so that the compression wave propagation due to the exhaust interference effect by the high-load intake passages 21a and 21b is effectively carried out by reducing its attenuation. ing. In addition, the output (intake air amount) of the air flow meter 18 is provided in each of the low-load intake passages 20a and 20b.
Electromagnetic valve type fuel injection nozzles 24, 24 are provided whose fuel injection amount is controlled according to the fuel injection amount.
そして、上記主高負荷用吸気通路21の分岐部
は高負荷用絞り弁23下流に位置して、第1高負
荷用吸気通路21aと第2高負荷用吸気通路21
b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Acs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高負荷用吸気通路21a,21bの最小通路
面積Asと同等かそれ以上(Acs≧As)に設定さ
れている。 The branching portion of the main high-load intake passage 21 is located downstream of the high-load throttle valve 23, and includes a first high-load intake passage 21a and a second high-load intake passage 21.
It is constituted by an enlarged chamber 26 having a communication passage 25 communicating with b. The passage area Acs of the communication passage 25 is set so as to reduce attenuation of pressure waves (compression waves due to exhaust interference effect) and effectively transmit them.
It is set to be equal to or larger than the minimum passage area As of the second high-load intake passages 21a and 21b (Acs≧As).
また、上記主低負荷用吸気通路20の分岐部
は、同様に、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20b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。上記拡大室
28の容積は、エンジン排気量(単一作動室の排
気量×2)に対して0.5〜2倍に設定されており、
0.5倍未満では膨張波と圧縮波間の反転効果が得
られず、一方、2倍を越えると圧力波が拡散して
しまい吸気個有脈動効果が著しく低下することに
よるものである。また、上記各拡大室26,28
は、エンジンの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、燃料の良好な応
答性を確保するものである。 Further, the branch portion of the main low-load intake passage 20 is similarly located downstream of the low-load throttle valve 22 and communicates the first low-load intake passage 20a and the second low-load intake passage 20b. It is constituted by an expansion chamber 28 having a communication passage 27. The volume of the expansion chamber 28 is set to 0.5 to 2 times the engine displacement (displacement of a single working chamber x 2),
This is because if it is less than 0.5 times, the reversal effect between expansion waves and compression waves cannot be obtained, whereas if it exceeds 2 times, the pressure waves will be diffused and the unique pulsation effect of the intake air will be significantly reduced. In addition, each of the expansion chambers 26, 28
The tank functions as a surge tank during transient operations such as engine acceleration or deceleration, and ensures good fuel response.
さらに、上記両気筒1A,1Bの高負荷用吸気
ポート4,4間の通路長さLsは、連通路25の
通路長さlcsと該連通路25下流の第1、第2高
負荷用吸気通路21a,21bの各通路長さls,
lsとを加算したもの(Lp=lcs+2ls)となり、
5000〜7000rpm(基準回転数Nh)のエンジン高回
転時を基準として上記()式から、
Ls≒0.57〜1.37(m)
に設定されている。 Further, the passage length Ls between the high-load intake ports 4, 4 of the two cylinders 1A, 1B is the passage length LCS of the communication passage 25 and the first and second high-load intake passages downstream of the communication passage 25. Each passage length ls of 21a and 21b,
ls (Lp = lcs + 2ls),
Based on the above formula (), Ls is set to 0.57 to 1.37 (m) based on the high engine speed of 5000 to 7000 rpm (standard rotation speed Nh).
加えて、上記第1、第2低負荷用吸気通路20
a,20bの通路長さlp、つまり該各低負荷用吸
気通路20a,20bの拡大室28への開口端面
から作動室9への開口(低負荷用吸気ポート3)
までの通路長さlpは、上記5000〜7000rpmの基準
回転数Nhよりも1000rpm以上低回転側の3500〜
5000rpm(回転数Nl)のエンジン中回転時を基準
として上記()式から
Lp=0.37〜0.78(m)
に設定されている。 In addition, the first and second low-load intake passages 20
a, 20b passage length lp, that is, the opening from the opening end surface of each low-load intake passage 20a, 20b to the enlarged chamber 28 to the working chamber 9 (low-load intake port 3)
The passage length lp is 1000rpm or more lower than the standard rotational speed Nh of 5000 to 7000rpm, which is 3500 to 3500.
Based on the above equation (), Lp is set to 0.37 to 0.78 (m) based on the engine medium rotation of 5000 rpm (rotation speed Nl).
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、高負荷用絞り弁23の開作動によ
り第1、第2高負荷用吸気通路21a,21bが
開かれて各気筒1A,1Bの高負荷用吸気ポート
4,4からも低負荷用吸気ポート3,3とは独立
して吸気の供給を行つている。その際、一方の気
筒例えば第2気筒1Bの高負荷用吸気ポート4開
口時には残留排気ガスの圧力により吸気が圧縮さ
れて第2高負荷用吸気通路21b内の高負荷用吸
気ポート4部分に開口時圧縮波が発生する。この
閉口時圧縮波は、両気筒1A,1Bの高負荷用吸
気ポート4,4間の各通路長さLsを上記5000〜
7000rpmのエンジン高回転時を基準として上記
()式によりLs=0.57〜1.37mに設定したこと
により、第2高負荷用吸気通路21b→連通路2
5→第1高負荷用吸気通路21aを経て、180゜の
位相差を持つ第1気筒1Aの全閉直前の高負荷用
吸気ポート4に伝播する。その結果、この開口時
圧縮波により、吸気が第1気筒1Aの全閉直前の
高負荷用吸気ポート4より作動室9内へ押し込ま
れて強い過給が行われることになる。同様に、第
2気筒1Bにおいても、全閉直前の高負荷用吸気
ポート4に対して第1気筒1Aからの閉口時圧縮
波が伝播して強い過給効果が得られる。 Next, to explain the operation of the above embodiment with reference to FIG. 3, when the engine rotates at a high speed of 5,000 to 7,000 rpm, which requires high output, the high-load throttle valve 23 is opened to open the first and second high-load intake passages. 21a, 21b are opened, and intake air is supplied from the high-load intake ports 4, 4 of each cylinder 1A, 1B independently of the low-load intake ports 3, 3. At this time, when the high-load intake port 4 of one cylinder, for example, the second cylinder 1B, is opened, the intake air is compressed by the pressure of the residual exhaust gas and is opened to the high-load intake port 4 in the second high-load intake passage 21b. A time compression wave is generated. This compression wave at the time of closing causes each passage length Ls between the high-load intake ports 4 and 4 of both cylinders 1A and 1B to be
By setting Ls = 0.57 to 1.37m using the above formula () based on the engine high speed of 7000 rpm, the second high-load intake passage 21b → communication passage 2
5→The signal propagates through the first high-load intake passage 21a to the high-load intake port 4 of the first cylinder 1A, which has a phase difference of 180°, just before it is fully closed. As a result, this opening compression wave forces the intake air into the working chamber 9 from the high-load intake port 4 just before the first cylinder 1A is fully closed, resulting in strong supercharging. Similarly, in the second cylinder 1B, the compression wave at the time of closing from the first cylinder 1A propagates to the high-load intake port 4 immediately before fully closing, resulting in a strong supercharging effect.
一方、上記5000〜7000rpmの基準回転数Nhよ
りも1000rpm以上低回転側の3500〜5000rpmのエ
ンジン中回転時には、各気筒1A,1Bににおい
て、低負荷用吸気ポート3の吸気開始により第
1、第2低負荷用吸気通路20a,20b内には
膨張波が発生し、この膨張波は、該低負荷用吸気
ポート3と拡大室28との間の通路長さlpを上記
()式により0.37〜0.78mに設定したことによ
り、第1、第2低負荷用吸気通路20a,20b
→拡大室28(圧縮波に反転して反射)→第1、
第2低負荷用吸気通路20a,20b→低負荷用
吸気ポート3(膨張波に反転して反射)→第1、
第2低負荷用吸気通路20a,20b→拡大室2
8(圧縮波に反転して反射)→第1、第2低負荷
用吸気通路20a,20bを経て、圧縮波の2次
脈動波として各気筒1A,1Bの全閉直前の低負
荷用吸気ポート3に伝播して過給が行われる。 On the other hand, during engine rotation of 3500 to 5000 rpm, which is 1000 rpm or more lower than the reference rotation speed Nh of 5000 to 7000 rpm, in each cylinder 1A and 1B, the first and second 2 Expansion waves are generated in the low-load intake passages 20a and 20b, and these expansion waves cause the passage length lp between the low-load intake port 3 and the expansion chamber 28 to be 0.37 to 0.37 by the above formula (). By setting it to 0.78m, the first and second low-load intake passages 20a, 20b
→ Expansion chamber 28 (reflects the compression wave and reflects it) → 1st,
2nd low-load intake passages 20a, 20b → low-load intake port 3 (reflected by expansion wave) → 1st,
2nd low load intake passage 20a, 20b → expansion chamber 2
8 (reflected as a compression wave) → Passes through the first and second low-load intake passages 20a, 20b, and is transmitted as a secondary pulsating wave of the compression wave to the low-load intake port of each cylinder 1A, 1B just before fully closing. 3 and supercharging is performed.
したがつて、このように気筒1A,1B相互間
においてエンジン高回転時の高負荷用吸気系統で
の排気干渉効果による過給効果と、エンジン中回
転時の低負荷用吸気系統での吸気個有脈動効果に
よる過給効果とによつて、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亘つて充填効率
の増大により出力を向上させることができる。
尚、第4図では、各気筒1A,1Bの低負荷用お
よび高負荷用吸気通路20a,20b,21bを
各々独立させた従来例の場合(破線で示す)に対
し、6000rpmを基準に高負荷用吸気系統で排気干
渉効果(実線で示す)を得るとともに4000rpmを
基準に低負荷用吸気系統で2次の吸気個有脈動効
果(一点鎖線で示す)を得るようにした本発明例
の場合におけるエンジンの出力トルク特性を示
す。 Therefore, between cylinders 1A and 1B, there is a supercharging effect due to the exhaust interference effect in the high-load intake system during high engine speeds, and an intake specific effect in the low-load intake system during medium engine speeds. Due to the supercharging effect due to the pulsation effect, as shown in FIG. 4, the output can be improved by increasing the charging efficiency from the middle speed range to the high speed range of the engine.
In addition, in FIG. 4, compared to the conventional example in which the low-load and high-load intake passages 20a, 20b, and 21b of each cylinder 1A and 1B are made independent (indicated by a broken line), high-load operation is performed with 6000 rpm as the standard. In the case of an example of the present invention, in which an exhaust interference effect (indicated by a solid line) is obtained in the air intake system for use, and a secondary intake individual pulsation effect (indicated by a dashed-dotted line) is obtained in the intake system for low load based on 4000 rpm. Shows the output torque characteristics of the engine.
また、その場合、特に高負荷用吸気通路21
a,21bは、低負荷用吸気通路20a,20b
よりも通路面積が大であり、しかも通路長さが短
かいので、圧力波(圧縮波)の伝播の抵抗が小さ
く、上記高負荷用吸気系統での排気干渉効果を有
効に発揮させることができる。 In that case, especially the high load intake passage 21
a, 21b are low load intake passages 20a, 20b
Since the passage area is larger and the passage length is shorter, there is less resistance to the propagation of pressure waves (compression waves), and the exhaust interference effect in the above-mentioned high-load intake system can be effectively exerted. .
また、上記各連通路25は、高負荷用絞り弁2
3下流に位置し、しかも該各連通路25の通路面
積Acsを高負荷用吸気通路21a,21bの最小
通路面積Asより同等以上としたので、上記高負
荷用絞り弁23や連通路25自身によつて圧力波
が減衰させることがなく上記排気干渉効果を有効
に発揮できる。また、上記拡大室28は低負荷用
絞り弁22下流に位置するので、同様に、吸気個
有脈動効果を有効に発揮できる。 In addition, each of the communication passages 25 is connected to the high load throttle valve 2.
3, and the passage area Acs of each communicating passage 25 is set to be equal to or larger than the minimum passage area As of the high-load intake passages 21a and 21b. Therefore, the pressure waves are not attenuated and the exhaust interference effect described above can be effectively exhibited. Furthermore, since the enlarged chamber 28 is located downstream of the low-load throttle valve 22, the intake-specific pulsation effect can be effectively exerted as well.
さらに、上記高負荷用吸気ポート4の開口時期
を低負荷用吸気ポート3よりも以早としたことに
より、排気ガスの吹き返しが高負荷用吸気ポート
4側に集中するので、高負荷用吸気ポート4での
開口時圧縮波を強く発生できるとともに、低負荷
用吸気ポート3での膨張波つまり2次脈動圧縮波
を強く発生でき、上記排気干渉効果および吸気個
有脈動効果による過給効果を一層強力なものとす
ることができる。 Furthermore, by opening the high-load intake port 4 earlier than the low-load intake port 3, the blowback of exhaust gas is concentrated on the high-load intake port 4 side. 4 can generate a strong compression wave when opening, and can also generate a strong expansion wave, that is, a secondary pulsating compression wave, at the low-load intake port 3, which further enhances the supercharging effect due to the exhaust interference effect and the intake unique pulsation effect. It can be made powerful.
また、上記排気干渉効果および吸気個有脈動効
果による過給効果は、低負荷用および高負荷用吸
気ポート3,4の開口期間θp,θs、第1高負荷用
吸気通路21aと第2高負荷用吸気通路21bと
を連通する連通路25の位置および低負荷用吸気
通路20a,20bの拡大室28の位置、並びに
両気筒1A,1Bの高負荷用吸気ポート4,4間
通路長さLsおよび上記拡大室28と低負荷用吸
気ポート3との間の通路長さ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。 In addition, the supercharging effect due to the exhaust interference effect and the intake individual pulsation effect is caused by the opening periods θp, θs of the low-load and high-load intake ports 3, 4, the first high-load intake passage 21a and the second high-load intake passage. The position of the communication passage 25 that communicates with the air intake passage 21b, the position of the enlarged chamber 28 of the low-load intake passages 20a and 20b, the passage length Ls between the high-load intake ports 4 and 4 of both cylinders 1A and 1B, and This can be achieved by setting the passage length lp between the expansion chamber 28 and the low-load intake port 3 as described above, and since a supercharger or the like is not required, the design of the existing intake system can be reduced. It requires only a few changes, has a very simple structure, and can therefore be implemented easily and inexpensively.
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、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。 It should be noted that the present invention is not limited to the above-mentioned embodiments, but also includes various other modifications. For example, setting the intake/exhaust overlap period to a range of 0 to 20 degrees in rotation angle of the eccentric shaft improves filling efficiency and
This is preferable in order to reduce the amount of dilution gas brought in and to prevent misfires, especially when the engine is under low load.
また、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 installed in the main low load intake passage 20 and in 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系統の独立した吸気通路を備
えた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、高負荷用吸気系統における気筒相互間
の排気干渉効果により過給効果を得るとともに、
上記5000〜7000rpmの基準回転数よりも1000pm
以上低回転側の3500rpm〜5000rpmのエンジン中
回転時、低負荷用吸気系統における各気筒自身の
吸気個有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
な設計変更による簡単な構成でもつて、エンジン
の中回転域から高回転域に亘つて充填効率を高め
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 equipped with two independent intake passages for low load and high load, the engine speed is high at 5000 to 7000 rpm. At the same time, a supercharging effect is obtained due to the exhaust interference effect between the cylinders in the high-load intake system, and
1000pm higher than the standard rotation speed of 5000~7000rpm above
As mentioned above, when the engine rotates at medium speeds of 3500rpm to 5000rpm on the low-speed side, the supercharging effect is obtained by the intake pulsation effect of each cylinder itself in the low-load intake system, so there is no need for a supercharger etc. Even with a simple configuration that involves slight design changes to the intake system, it is possible to effectively improve the output by increasing the filling efficiency from the mid- to high-speed range of the engine, thereby improving the output of the rotary piston engine. This can greatly contribute to easier implementation of countermeasures and cost reduction.
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グラフであ
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、16…主吸気通
路、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、28……拡大
室。
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. 3 is a graph 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, 16...Main intake passage, 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 intake passage for high load, 21b... Second intake passage for high load, 22... Throttle valve for low load, 23...
High-load throttle valve, 25...communication passage, 28...expansion chamber.
Claims (1)
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にそれぞれ配設され
た略三角形状のロータが、エキセントリツクシヤ
フトに支承され該シヤフトの回転角で180゜の位相
差を持つて遊星回転運動し、かつ低負荷用吸気通
路と上記低負荷用吸気通路よりも通路面積の大き
い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2気筒ロータリピ
ストンエンジンにおいて、 a 高負荷用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゜の範囲に
設定すること、 b 低負荷用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230〜290゜の範囲に
設定すること、 c 各気筒の高負荷用吸気通路を絞り弁下流にお
いて連通路で連通すること、 d 各気筒の低負荷用吸気通路の絞り弁下流に拡
大室を設けること、 e 上記連通路およびその下流の高負荷用吸気通
路によつて形成される両気筒の高負荷用吸気ポ
ート間の通路長さを、5000〜7000rpmの間で設
定したエンジン高回転時、一方の気筒の高負荷
用吸気ポート開口時に高負荷用吸気通路内に発
生する圧縮波を上記連通路を介して他方の気筒
の全閉直前の高負荷用吸気ポートに伝播させる
ように0.57〜1.37mの範囲内に設定すること、 f 上記拡大室から低負荷用吸気ポートまでの低
負荷用吸気通路の通路長さを、上記5000〜
7000rpmの間で設定した回転数よりも1000rpm
以上低回転側の3500〜5000rpmのエンジン中回
転時、各気筒の低負荷用吸気ポートの吸気開始
により低負荷用吸気通路内に発生する膨張波を
上記拡大室で反転して反射した圧縮波の2次脈
動波を各気筒の全閉直前の低負荷用吸気ポート
に伝播させるように0.37〜0.78mの範囲内に設
定すること の条件のもとで、各気筒の全閉直前の低負荷用お
よび高負荷用吸気ポートにそれぞれ伝播した圧縮
波により過給を行うようにしたことを特徴とする
ロータリピストンエンジンの吸気装置。[Scope of Claims] 1. Approximately triangular rotors each disposed within a casing formed of a rotor housing having a two-bar trochoidal inner circumferential surface and side housings located on both sides of the rotor housing have eccentric shafts. The intake passage for low load and the intake passage for high load, which have a larger passage area than the intake passage for low load, are independent from each other. In a two-cylinder rotary piston engine that opens into the working chamber through low-load and high-load intake ports provided in each side housing, a. b. Set the opening period of the low-load intake port to a range of 230-290° based on the rotation angle of the eccentric shaft. c. Set the high-load intake passage of each cylinder to a throttle valve. d. Providing an enlarged chamber downstream of the throttle valve of the low-load intake passage of each cylinder; e. Both cylinders formed by the above-mentioned communication passage and the high-load intake passage downstream thereof. The compression wave generated in the high-load intake passage when the high-load intake port of one cylinder is opened at high engine speed when the passage length between the high-load intake ports is set between 5000 and 7000 rpm is as shown above. Set within the range of 0.57 to 1.37 m so that the high-load intake port of the other cylinder is propagated through the communication passage to the high-load intake port just before fully closing. Set the length of the intake passage to 5000~
1000rpm than the set rotation speed between 7000rpm
When the engine rotates at a low speed of 3,500 to 5,000 rpm, the expansion wave generated in the low-load intake passage by the start of intake at the low-load intake port of each cylinder is reversed and reflected by the expansion chamber, resulting in a compression wave. Under the condition that the secondary pulsation wave is set within the range of 0.37 to 0.78 m so that the secondary pulsation wave propagates to the low-load intake port just before each cylinder is fully closed, the low-load intake port just before each cylinder is fully closed An intake device for a rotary piston engine, characterized in that supercharging is performed by compression waves propagated to the intake port for high load and the intake port for high load.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP57212429A JPS59101546A (en) | 1982-12-02 | 1982-12-02 | Suction device of rotary piston engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP57212429A JPS59101546A (en) | 1982-12-02 | 1982-12-02 | Suction device of rotary piston engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS59101546A JPS59101546A (en) | 1984-06-12 |
| JPH0337010B2 true JPH0337010B2 (en) | 1991-06-04 |
Family
ID=16622443
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP57212429A Granted JPS59101546A (en) | 1982-12-02 | 1982-12-02 | Suction device of rotary piston engine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS59101546A (en) |
-
1982
- 1982-12-02 JP JP57212429A patent/JPS59101546A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS59101546A (en) | 1984-06-12 |
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