JPH0337011B2 - - Google Patents
Info
- Publication number
- JPH0337011B2 JPH0337011B2 JP57217318A JP21731882A JPH0337011B2 JP H0337011 B2 JPH0337011 B2 JP H0337011B2 JP 57217318 A JP57217318 A JP 57217318A JP 21731882 A JP21731882 A JP 21731882A JP H0337011 B2 JPH0337011 B2 JP H0337011B2
- 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 - Lifetime
Links
- 230000006835 compression Effects 0.000 claims description 29
- 238000007906 compression Methods 0.000 claims description 29
- 238000004891 communication Methods 0.000 claims description 26
- 230000000644 propagated effect Effects 0.000 claims description 7
- 230000000694 effects Effects 0.000 description 57
- 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
- 230000008859 change Effects 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 230000009977 dual effect Effects 0.000 description 2
- 238000004880 explosion Methods 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 230000006698 induction Effects 0.000 description 2
- 238000000034 method 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
- 239000003054 catalyst Substances 0.000 description 1
- 238000010790 dilution Methods 0.000 description 1
- 239000012895 dilution Substances 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
- 238000000746 purification Methods 0.000 description 1
- 230000009467 reduction Effects 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
-
- 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
- F02B2053/005—Wankel engines
-
- 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, one for low load and one for high load. The present invention relates to an engine in which a supercharging effect is obtained from a medium speed range to a high speed range of an engine by utilizing intake pressure waves generated in an intake passage.
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た低負荷
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、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 low-load intake passage equipped with a high-load throttle valve opens into the working chamber through low-load and high-load intake ports provided independently in each of the side housings downstream of the low-load throttle valve. The intake, compression, explosion, expansion, and exhaust strokes are sequentially performed in each cylinder as the rotor rotates while maintaining the above-mentioned 180° phase difference between the two cylinders. 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 to increase charging efficiency and improve 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吸気の慣性により吸気
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
を知見した。このことから、一方の気筒での上記
(i)の閉口時の圧縮波を他方の気筒の特に吸気の吹
き返しが生じる全閉直前の吸気ポートにに作用せ
しめれば効果的に過給効果が得られること(以
下、吸気慣性効果という)、および一方の気筒で
の上記(ii)の開口時の圧縮波を他方の気筒の同じく
全閉直前の吸気ポートに作用せしめれば効果的に
過給効果が得られること(以下、排気干渉効果と
いう)を見い出したのである。 Therefore, when examining the intake characteristics of the side intake port in a rotary piston engine, the inventors found that (i) when the intake port is opened, the intake air is compressed due to the inertia of the intake air, and a compression wave is generated at the intake port portion in the intake passage; (ii) It was discovered that when the intake port opens, the intake air is compressed by the pressure of the residual exhaust gas in the working chamber, and a compression wave is generated in the intake port portion of the intake passage. From this, the above for one cylinder
(i) If the compression wave at the time of closing is applied to the intake port of the other cylinder, especially just before fully closing, where intake air blowback occurs, a supercharging effect can be effectively obtained (hereinafter referred to as intake inertia effect). , and that a supercharging effect can be effectively obtained by applying the compression wave at the time of opening of (ii) above in one cylinder to the intake port of the other cylinder just before it is fully closed (hereinafter referred to as exhaust interference effect). ).
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、上記吸気慣性効果および排気干渉効果を得る
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各効果を有効に得る
ことができる。 In the two-system side intake port type two-cylinder rotary piston engine as described above, in order to obtain the above-mentioned intake inertia effect and exhaust interference effect, the high-load intake passage and the low-load intake passage are independent of each other. Since there are two systems of intake passages, each of the above-mentioned effects can be effectively obtained in each 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、各吸気の高負荷用および低
負荷用吸気通路同志を連通する連通路の位置、並
びに両気筒の高負荷用吸気ポート間および低負荷
用吸気ポート間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、一方の吸気系統での吸気慣性効果に
より過給効果を得るとともに、それよりも低回転
側で他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, with each opening period of the high-load and low-load intake ports, and the high-load and low-load intake ports. By appropriately setting the position of the communication passage that connects the intake passages and the length of the passage between the high-load intake ports and the low-load intake ports of both cylinders, the engine speed of 5000 to 7000 rpm, which requires high output, can be improved. During rotation, a supercharging effect is obtained due to the intake inertia effect in one intake system, and a supercharging effect is obtained due to the exhaust interference effect in the other intake system at lower rotation speeds, and the supercharger etc. The aim is to effectively improve the output by increasing the charging efficiency from the mid-speed range to the high-speed range of the engine through a simple configuration by making slight design changes to 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 各気筒の低負荷用吸気通路同志および高負荷
用吸気通路同志を各々絞り弁下流において連通
路で連通すること、
d 上記一方の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Lp(s)を、5000〜7000rpmの間で設定
したエンジン高回転時、一方の気筒の吸気ポー
ト閉口時に吸気通路内に発生する閉口時圧縮波
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るように設定すること、
e 上記他方の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Ls(p)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、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るように設定す
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、よつて一方の吸気
系統におけるエンジン高回転時の吸気慣性効果お
よび他方の吸気系統におけるエンジン中回転時の
排気干渉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:
Approximately triangular rotors are disposed within a casing formed by a rotor housing having a nodular trochoidal inner circumferential surface and side housings located on both sides of the rotor housing, and are supported by an eccentric shaft to adjust the rotation angle of the shaft. The engine rotates planetarily with a phase difference of 180 degrees, and the low-load intake passage and the high-load intake passage are independently provided by low-load and high-load intake ports provided in each side housing. In a two-cylinder rotary piston engine that opens into the working chamber, a) the opening period θs of the high-load intake port should be set within the range of 270 to 320° in terms of the rotation angle of the eccentric shaft; b) the opening of the low-load intake port Set the period θp within the range of 230 to 290 degrees in rotation angle of the eccentric shaft, c. Connect the low-load intake passages and the high-load intake passages of each cylinder through a communication passage downstream of the throttle valve. (d) When the engine speed is high, with the passage length Lp (s) between the intake ports of both cylinders formed by one of the communicating passages and the intake passage downstream thereof being set between 5000 and 7000 rpm, one side setting so that a compression wave generated in the intake passage when the intake port of the cylinder is closed is propagated through the communication passage to the intake port of the other cylinder just before being fully closed, e. The passage length Ls (p) between the intake ports of both cylinders formed by the downstream intake passage is set to 3500 to 5000 rpm, which is at least 1000 rpm lower than the rotation speed set between 5000 and 7000 rpm. When the engine is running at medium speed, the compression wave generated in the intake passage when the intake port of one cylinder is opened is set so as to propagate through the communication passage to the intake port of the other cylinder just before it is fully closed. Under these conditions, supercharging is performed by compression waves that propagate to the low-load and high-load intake ports of each cylinder just before they are fully closed, thereby reducing the intake inertia effect at high engine speeds in one intake system. The exhaust interference effect in the other intake system during engine mid-speed rotation effectively increases the charging efficiency from the mid-engine speed range to the high-speed engine speed range.
ここにおいて、上記一方の吸気系統で吸気慣性
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、他方の吸気系統で
排気干渉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
大トルクがこの回転域で設定されていること、低
回転域で排気干渉効果が得にくいこと、さらに上
記基準回転数Nhで吸気慣性効果を得た場合、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)で排気干渉効果を得るこ
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 ~ 5000 at high engine speed to obtain the intake inertia effect with one of the intake systems mentioned above.
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, when the engine is running at mid-speed, the exhaust interference effect is obtained with the other intake system.
The setting of the rotation speed Nl from 3500 to 5000 rpm is because the maximum torque is generally set in this rotation range, the exhaust interference effect is difficult to obtain in the low rotation range, and the intake inertia effect is obtained at the above reference rotation speed Nh. In this case, the effect (supercharging effect) is Nn around the reference rotation speed Nh.
Since the speed ranges from 1000rpm to high and low rotational speeds, obtaining the exhaust interference effect at least 1000rp or more lower than the reference rotational speed Nh (Nl≦Nh−1000rpm) can 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での各連通路の絞り弁下
流位置設定は、高負荷用および低負荷用吸気通路
の空気流量を制御する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 in each communication passage in setting item c above should be determined because the existence of the throttle valve that controls the air flow rate in the high-load and low-load intake passages acts as a 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dでの一方の吸気系統の
両気筒の吸気ポート間の通路長さLp(s)は、エ
ンジン回転数が5000〜7000rpmの範囲内で設定し
た基準回転数Nhのときに吸気慣性効果を効果的
に得るように設定されたもので、
Lp(s)=(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、180゜は両気筒の位相差であり、
またθ0は吸気ポートに閉口時圧縮波が実質的に発
生してから全閉までの期間と効果的に過給を行う
ために該閉口時圧縮波を伝播させる吸気ポート全
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(180−θ0)は
一方の気筒での閉口時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、Nh=
5000〜7000rpmであり、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。 Furthermore, the passage length Lp (s) between the intake ports of both cylinders in one intake system in the setting item d above is the same as that when the engine speed is the reference rotation speed Nh set within the range of 5000 to 7000 rpm. It is set to effectively obtain an inertial effect, and is a value obtained from the formula Lp(s)=(180−θ 0 )×60/360Nh)×a (). That is, in the above equation (), 180° is the phase difference between both cylinders,
In addition, θ 0 is the period from when the compression wave at the time of closing is substantially generated at the intake port until it is fully closed, and from the time just before the intake port is fully closed when the compression wave at the time of closing is propagated to effectively perform supercharging. The invalid period is the sum of the period when the cylinder is fully closed, and θ 0 ≒ 20°, so (180 − θ 0 ) is the propagation from the compression wave generated at the time of closing in one cylinder to the intake port of the other cylinder. It represents the rotation angle of the eccentric shaft required to reach Also, Nh=
5000 to 7000 rpm, and 60/360Nh 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.
さらにまた、上記設定事項eでの他方の吸気系
統の両気筒の吸気ポート間の通路長さls(p)は、
エンジン回転数が5000〜7000rpmの範囲内の基準
回転数Nhよりも1000rpm以上低回転側の3500〜
5000rpmの範囲内のNl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(p)=(θs(p)−180−θ1)
×(60/360Nl)
×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,θpは高負荷用および低負
荷用吸気ポート開口期間で、θs=270〜320゜、θp
=230〜290゜であり、180゜は両気筒間の位相差で
あり、またθ1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(p)
−180−θ1)は一方の気筒での開口時圧縮波発生
から他方の気筒の各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、60/360Nlは1゜回転するのに要する時間
(秒)を表わす。またa=343m/s(20℃で)で
ある。 Furthermore, the passage length ls(p) between the intake ports of both cylinders of the other intake system in the above setting e is:
The engine speed is 1000rpm or more lower than the standard rotational speed Nh within the range of 5000 to 7000rpm, from 3500 to 3500.
It is set to effectively obtain the exhaust interference effect when Nl is within the range of 5000 rpm, Ls (p) = (θs (p) - 180 - θ 1 ) × (60/360Nl) × a... ...This is the value obtained from the formula (). That is, in the above equation (), θs and θp are the intake port opening periods for high load and low load, θs = 270 to 320°, θp
= 230 to 290°, 180° is the phase difference between both cylinders, and θ 1 is the period from the opening of the intake port until the compression wave is substantially generated at the time of opening, and for effective supercharging. The ineffective period is the sum of the period from just before the intake port is fully closed to when the opening compression wave is propagated, and θ 0 ≒ 20°, so (θs(p)
−180−θ 1 ) represents the rotation angle of the eccentric shaft required from generation of the compression wave at opening in one cylinder to propagation to each intake port of the other cylinder. Also, 60/360Nl represents the time (seconds) required to rotate 1°. Also, a=343 m/s (at 20°C).
尚、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。 Note that 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θp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、高負荷用吸気ポート4からの開口時圧縮波を
共に強く発生させるようにしている。また、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 θp 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 a strong compression wave is generated when opening from the high-load intake port 4. I have to. Further, the opening timing of the high-load intake port 4 is set to be the same as or later than the opening 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。上記連通路
27の通路面積Acpは同じく圧力波を有効に伝達
するように第1、第2低負荷用吸気通路20a,
20bの最小通路面積Apと同等かそれ以上
(Acp≧Ap)に設定されている。尚、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 passage area Acp of the communication passage 27 is set such that the first and second low-load intake passages 20a,
It is set to be equal to or larger than the minimum passage area Ap of 20b (Acp≧Ap). Each of the enlarged chambers 26 and 28 functions as a surge tank during transient operation such as acceleration or deceleration of the engine, and ensures good fuel response.
さらに、上記両気筒1A,1Bの低低荷用吸気
ポート3,3間の通路長さLpは、連通路27の
通路長さlcpと該連通路27下流の第1、第2低
負荷用吸気通路20a,20bの各通路長さlp,
lpとを加算したもの(Lp=lcp+2lp)となり、
5000〜7000rpmの範囲内の基準回転数Nhでのエ
ンジン高回転時を基準として吸気慣性効果を得る
ように上記()式から、
Lp≒1.31〜1.83(m)
に設定されている。 Further, the passage length Lp between the low and low load intake ports 3 and 3 of the above-mentioned cylinders 1A and 1B is the passage length lcp of the communication passage 27 and the first and second low load intake ports downstream of the communication passage 27. Each passage length lp of passages 20a and 20b,
It is the sum of lp and (Lp = lcp + 2lp),
From the above formula (), Lp is set to 1.31 to 1.83 (m) so as to obtain the intake inertia effect based on the engine high rotation at a reference rotation speed Nh within the range of 5000 to 7000 rpm.
加えて、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(Ls=lcs+2ls)となり、上
記5000〜7000rpmの基準回転数Nhよりも
1000rpm以上低回転側の3500〜5000rpmの範囲内
の回転数Nlでのエンジン中回転時を基準として
排気干渉効果を得るように上記()式から
Ls=0.80〜1.96(m)
に設定されている。 In addition, the passage length Ls between the high-load intake ports 4 and 4 of the two cylinders 1A and 1B is the passage length Lcs of the communication passage 25 and the first and second high-load intake ports downstream of the communication passage 25. Each passage length ls of passages 21a and 21b,
ls (Ls = lcs + 2ls), which is higher than the standard rotation speed Nh of 5000 to 7000 rpm above.
Based on the above formula (), Ls is set to 0.80 to 1.96 (m) in order to obtain the exhaust interference effect based on the engine rotation speed Nl in the range of 3500 to 5000 rpm on the low rotation side of 1000 rpm or more. .
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、エンジン高負荷時には、高負荷用絞り弁2
3の開作動により第1、第2高負荷用吸気通路2
1a,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
して、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閉口時には吸気の慣性によ
り吸気が圧縮されて第2低負低用吸気通路20b
内の低負荷用吸気ポート3部分に閉口時圧縮波が
発生する。この閉口時圧縮波は、両気筒1A,1
Bの低負荷用吸気ポート3,3間の通路長さLp
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Lp=1.31〜1.83mに設
定したことにより、第2低負荷用吸気通路20b
→連通路27→第1低負荷用吸気通路20aを経
て、180゜の位相差を持つ第1気筒1Aの全閉直前
の低負荷用吸気ポート3に伝播する。その結果、
この閉口時圧縮波により、吸気が第1気筒1Aの
全閉直前の低負荷用吸気ポート3より作動室9内
へ押し込まれて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3に対して第1気筒1Aからの閉口
時圧縮波が伝播して過給効果が得られる。 Next, the operation of the above embodiment will be explained with reference to FIG. 3. When the engine is under high load, the high load throttle valve 2
3 opens the first and second high-load intake passages 2.
1a and 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. When the engine rotates at a high speed of 5000 to 7000 rpm, which requires high output, when one cylinder, for example, the low-load intake port 3 of the second cylinder 1B, is closed, the intake air is compressed by the inertia of the intake air, and the second low-negative low-use intake passage 20b is compressed.
Compression waves occur in the low-load intake port 3 portion when the valve is closed. This compression wave at the time of closing occurs in both cylinders 1A and 1.
Passage length Lp between low load intake ports 3 and 3 of B
By setting Lp to 1.31 to 1.83 m using the above formula () based on the above engine high rotation of 5000 to 7000 rpm, the second low-load intake passage 20b
→The communication passage 27→The first low-load intake passage 20a is propagated to the low-load intake port 3 of the first cylinder 1A, which has a phase difference of 180 degrees and is just before fully closed. the result,
Due to this compression wave during closing, intake air is forced into the working chamber 9 from the low-load intake port 3 immediately before the first cylinder 1A is fully closed, and supercharging is performed. 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 3 immediately before fully closing, so that a supercharging effect is obtained.
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の高負荷
用吸気ポート4開口時に開口時圧縮波が発生し、
この開口時圧縮波は、両気筒1A,1Bの高負荷
用吸気ポート4,4間の通路長さLsを上記()
式によりLs=0.80〜1.96mに設定したことによ
り、連通路25を介して他方の気筒1A,1Bの
全閉直前の高負荷用吸気ポート4に伝播して過給
が行われる。 On the other hand, when the engine rotates in the middle range of 3500 to 5000 rpm, which is 1000 rpm or more lower than the reference rotation speed Nh of 5000 to 7000 rpm, a compression wave is generated when the high load intake port 4 of each cylinder 1A and 1B is opened.
This compression wave at the time of opening causes the passage length Ls between the high-load intake ports 4 and 4 of both cylinders 1A and 1B to be
By setting Ls=0.80 to 1.96 m according to the formula, supercharging is carried out via the communication passage 25 to the high-load intake port 4 of the other cylinders 1A and 1B just before they are fully closed.
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低負荷用吸気系統で
の吸気慣性効果による過給効果と、エンジン中回
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,21a,21b
を各々独立させた従来例の場合(破線で示す)に
対し、6000rpmを基準に低負荷用吸気系統で吸気
慣性効果を得るとともに4000rpmを基準に高負荷
用吸気系統で排気干渉効果を得るようにした本発
明例の場合(実線で示す)におけるエンジンの出
力トルク特性を示す。 Therefore, between cylinders 1A and 1B, there is a supercharging effect due to the intake inertia effect in the low-load intake system during high engine speeds, and an exhaust interference effect in the high-load intake system during medium engine speeds. Due to the supercharging 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, the low-load and high-load intake passages 20a, 20b, 21a, 21b of each cylinder 1A, 1B are shown.
In contrast to the conventional example in which each is independent (shown by the broken line), the intake inertia effect is obtained in the low-load intake system based on 6000 rpm, and the exhaust interference effect is obtained in the high-load intake system based on 4000 rpm. 5 shows the output torque characteristics of the engine in the case of the present invention example (indicated by a solid line).
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吸気慣性効果を有
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 intake inertia effect in the above-mentioned high-load intake system can be effectively exerted. .
また、上記各連通路25,27は、各絞り弁2
2,23下流に位置し、しかも該各連通路25,
27の通路面積Acs、Acpを高負荷用および低負
荷用吸気通路21a,21b,20a,20bの
最小通路面積As,Apより同等以上としたもの
で、上記各絞り弁22,23や各連通路25,2
7自身によつて圧力波が減衰されることがなく上
記各吸気系統での吸気慣性効果および排気干渉効
果を有効に発揮できる。 Further, each of the communication passages 25 and 27 is connected to each throttle valve 2.
2, 23 downstream, and each communication path 25,
The passage areas Acs and Acp of No. 27 are equal to or greater than the minimum passage areas As and Ap of the high-load and low-load intake passages 21a, 21b, 20a, and 20b, and each of the above-mentioned throttle valves 22 and 23 and each communication passage 25,2
The pressure waves are not attenuated by 7 itself, and the intake inertia effect and exhaust interference effect in each intake system can be effectively exhibited.
さらに、上記実施例では、エンジン高回転時に
低負荷用吸気系統で吸気慣性効果を、エンジン中
回転時に高負荷用吸気系統で排気干渉効果をそれ
ぞれ得るように設定したので、逆の場合(エンジ
ン高回転時に高負荷用吸気系統で吸気慣性効果
を、エンジン中回転時に低負荷用吸気系統で排気
干渉効果を得る場合)に較べて高負荷用吸気通路
21a,21bの通路長さlsを可及的に短かくで
き、高負荷用吸気通路21a,21bのデユアル
インダクシヨン特性(充填効率向上)に適合でき
る。 Furthermore, in the above embodiment, the intake inertia effect was set to be obtained in the low-load intake system during high engine speeds, and the exhaust interference effect was obtained in the high-load intake system during medium engine speeds. The passage length ls of the high-load intake passages 21a and 21b can be made as large as possible compared to the case where the intake inertia effect is obtained in the high-load intake system during engine rotation, and the exhaust interference effect is obtained in the low-load intake system during mid-engine rotation. It can be shortened to suit the dual induction characteristics (improvement of filling efficiency) of the high-load intake passages 21a and 21b.
さらにまた、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側に集中して、該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ので、上記高負
荷用吸気系統での排気干渉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. Since a strong compression wave can be generated when the intake port 4 opens, the exhaust interference effect in the high-load intake system can be made even stronger.
また、上記吸気慣性効果および排気干渉効果に
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、高負荷用吸気通路21
a,21b同志および低負荷用吸気通路20a,
20b同志を連通する各連通路25,27の位
置、並びに両気筒1A,1Bの高負荷用吸気ポー
ト4,4間および低負荷用吸気ポート3,3間の
通路長さLs,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
気系統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 intake inertia effect and the exhaust interference effect is due to the opening period of the low-load and high-load intake ports 3 and 4, and the high-load intake passage 21
a, 21b and low load intake passage 20a,
The positions of the communication passages 25 and 27 that communicate with each other and the passage lengths Ls and Lp between the high-load intake ports 4 and 4 and between the low-load intake ports 3 and 3 of both cylinders 1A and 1B are determined as described above. Since it does not require a supercharger or the like, it requires only a slight design change to the existing intake system, 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、上記実施例と異なり、エンジン高回
転時に吸気慣性効果を低負荷用吸気系統で、エン
ジン中回転時に排気干渉効果を低負荷用吸気系統
で得るようにしてもよいのは勿論である。 It should be noted that the present invention is not limited to the above-mentioned embodiments, but also includes various other modifications. For example, unlike the above embodiment, it is of course possible to obtain the intake inertia effect in the low-load intake system when the engine is running at high speeds, and to obtain the exhaust interference effect in the low-load intake system when the engine is running at medium speeds.
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.
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、一方の吸気系統における気筒相互間の
吸気慣性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、他方の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 intake inertia effect between the cylinders in one intake system, and when the engine is running at mid engine speed of 3500 rpm to 5000 rpm, which is 1000 pm or more lower than the reference rotation speed of 5000 to 7000 rpm, the other intake system Since the supercharging effect is obtained by the exhaust interference effect between cylinders in the system,
Even with a simple configuration that requires only slight design changes to the existing intake system, without the need for a supercharger, it is possible to effectively improve output by increasing charging efficiency from the mid- to high-speed range of the engine. Therefore, it can greatly contribute to the easy implementation of measures to improve the output of rotary piston engines 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、27……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. 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, 27... communication passage.
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 各気筒の低負荷用吸気通路同志および高負荷
用吸気通路同志を各々絞り弁下流において連通
路で連通すること、 d 上記一方の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の間で設定したエン
ジン高回転時、一方の気筒の吸気ポート閉口時
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
播させるように設定すること、 e 上記他方の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、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、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るように設定すること、 によつて、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 shaft is supported by the shaft and rotates planetarily with a phase difference of 180 degrees at the rotation angle of the shaft, and a low-load intake passage and a high-load intake passage are independently provided in each side housing. In a two-cylinder rotary piston engine in which a high-load intake port opens into the working chamber, a) the opening period of the high-load intake port is set in the range of 270 to 320 degrees in rotation angle of the eccentric shaft; b. Set the opening period of the load intake port in the range of 230 to 290 degrees in rotation angle of the eccentric shaft, c. Connect the low-load intake passages and high-load intake passages of each cylinder downstream of the throttle valve. communicating through a passage; d; when the engine is running at high speed, when the passage length between the intake ports of both cylinders formed by one of the communication passages and the intake passage downstream thereof is set between 5000 and 7000 rpm; setting so that the compression wave generated in the intake passage when the intake port of the cylinder is closed is propagated through the communication passage to the intake port of the other cylinder just before it is fully closed, e. The length of the passage between the intake ports of both cylinders formed by the intake passage of
When the engine rotates at a medium speed of 5000 rpm, the compression wave generated in the intake passage when the intake port of one cylinder is opened is set so as to be propagated through the communication passage to the intake port of the other cylinder just before it is fully closed. Therefore, an intake system for a rotary piston engine is characterized in that supercharging is performed by compression waves propagated to the low-load and high-load intake ports of each cylinder immediately before they are fully closed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP57217318A JPS59105933A (en) | 1982-12-10 | 1982-12-10 | Intake apparatus of rotary piston engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP57217318A JPS59105933A (en) | 1982-12-10 | 1982-12-10 | Intake apparatus of rotary piston engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS59105933A JPS59105933A (en) | 1984-06-19 |
| JPH0337011B2 true JPH0337011B2 (en) | 1991-06-04 |
Family
ID=16702283
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP57217318A Granted JPS59105933A (en) | 1982-12-10 | 1982-12-10 | Intake apparatus of rotary piston engine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS59105933A (en) |
-
1982
- 1982-12-10 JP JP57217318A patent/JPS59105933A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS59105933A (en) | 1984-06-19 |
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