JPH01195919A - Engine provided with pressure wave supercharger - Google Patents

Engine provided with pressure wave supercharger

Info

Publication number
JPH01195919A
JPH01195919A JP2169788A JP2169788A JPH01195919A JP H01195919 A JPH01195919 A JP H01195919A JP 2169788 A JP2169788 A JP 2169788A JP 2169788 A JP2169788 A JP 2169788A JP H01195919 A JPH01195919 A JP H01195919A
Authority
JP
Japan
Prior art keywords
pressure wave
rotor
intake
wave supercharger
engine
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP2169788A
Other languages
Japanese (ja)
Inventor
Toshihiro Kamimura
敏浩 上村
Kiyomi Kimura
清美 木村
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mazda Motor Corp
Original Assignee
Mazda Motor Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mazda Motor Corp filed Critical Mazda Motor Corp
Priority to JP2169788A priority Critical patent/JPH01195919A/en
Publication of JPH01195919A publication Critical patent/JPH01195919A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B3/00Engines characterised by air compression and subsequent fuel addition
    • F02B3/06Engines characterised by air compression and subsequent fuel addition with compression ignition
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Landscapes

  • Supercharger (AREA)

Abstract

PURPOSE:To improve scavenge efficiency and to improve misfire through reduction of internal EGR by providing a variable pulley unit for lowering the rotary ratio of a pressure wave supercharger with respect to an engine output shaft and a control means therefor. CONSTITUTION:Output shaft, i.e. crankshaft 2, of a Diesel engine is coupled with the rotor shaft 7a of a pressure wave supercharger 6 through crank pulley and belt 4 and a rotor pulley 5. A variable pulley unit 2 for lowering the rotary ratio of a pressure wave supercharger 6 with respect to the crankshaft 2 is further provided. A control means for operating a variable pulley unit 21 under high rotation zone in low load region is also provided. The control means comprises a spring 33 and a flyweight 26. By such arrangement, scavenge efficiency is improved and internal EGR is reduced resulting in the improvement of misfire.

Description

【発明の詳細な説明】 (産業上の利用分野) この発明は、排気ガスの圧力波エネルギを吸気に伝達し
、吸気を圧縮して過給を行なう圧力波過給機付エンジン
に関する。
DETAILED DESCRIPTION OF THE INVENTION (Industrial Application Field) The present invention relates to an engine with a pressure wave supercharger that transmits pressure wave energy of exhaust gas to intake air, compresses the intake air, and performs supercharging.

(従来技術) 従来、上述例の圧力波過給機付エンジンとしては、例え
ば第5図に示ず如き構造のディーゼルエンジンがある。
(Prior Art) Conventionally, as the above-mentioned pressure wave supercharged engine, there is a diesel engine having a structure as shown in FIG. 5, for example.

すなわち、ディーゼルエンジン51のクランク軸52に
ブーりおよびベルト(図示せず)を介して可回動なロー
タ53を設け、このロータ53に多数の小室としてのセ
ル54を形成する多数の隔壁55(第5図においてはロ
ータ53の回転を下方移動に置換した状態で示している
)を放射状に配設すると共に、上述のロータ53の一端
側のエアケーシング56には吸気導入口57および吸気
吐出口58を形成し、また上述のロータ53の他端側の
ガスケーシング59には排気導入口6oおよび排気吐出
口61を形成し、かつ上述の吸気吐出口58に吸気マニ
ホルド62を、排気導入口60に排気マニホルド63を
それぞれ接続した圧力波過給機付エンジンである。
That is, a rotor 53 is provided on a crankshaft 52 of a diesel engine 51 and is rotatable via a boob and a belt (not shown), and this rotor 53 is provided with a large number of partition walls 55 ( In FIG. 5, the rotation of the rotor 53 is replaced with downward movement) are arranged radially, and the air casing 56 at one end of the rotor 53 has an intake inlet 57 and an intake outlet. 58, an exhaust inlet 6o and an exhaust outlet 61 are formed in the gas casing 59 at the other end of the rotor 53, an intake manifold 62 is connected to the intake outlet 58, and an exhaust inlet 60 is connected to the exhaust inlet 60. This is an engine equipped with a pressure wave supercharger, in which an exhaust manifold 63 is connected to the exhaust manifold 63.

この圧力波過給機付エンジンは、上述のロータ53のエ
ンジン回転数に応じた回転に伴い、吸気導入口57から
ロータ53のセル54に吸入した吸気に対して、排気導
入口60から該セル54に排気を流入させ、排気の圧力
波エネルギを吸気に伝達して、吸気を圧縮、加速して吸
気吐出口58から過給吐出させる一方、上述のセル54
内に残る排気を排気吐出口61から排出させると共に、
吸気導入口57から上述のセル54内に吸気を導入する
ことにより掃気を行うことを繰返す゛。
In this pressure wave supercharged engine, as the rotor 53 rotates according to the engine speed, intake air drawn into the cells 54 of the rotor 53 from the intake port 57 is transferred from the exhaust port 60 to the cells 54 of the rotor 53. 54, the pressure wave energy of the exhaust gas is transmitted to the intake air, the intake air is compressed and accelerated, and is supercharged and discharged from the intake air outlet port 58.
The exhaust gas remaining inside is discharged from the exhaust outlet 61, and
Scavenging is repeated by introducing intake air into the cell 54 described above from the intake air introduction port 57.

しかし、上述の圧力波過給機付エンジンにおいては低負
荷域におけるエンジン高回転時に失火する問題点があっ
た。
However, the pressure wave supercharged engine described above has the problem of misfire at high engine speeds in a low load range.

すなわち、音速で伝播される排気の圧力波は固定端で圧
力波として反射し、開放端で膨張波として反転して、通
常は回転数と各ボート57,58゜60.61とのタイ
ミングが合致して第5図に点線aに示すような吸入エア
と排気ガスとの理想的な境界線が形成されるが、低負荷
域の高回転時においては、ロータ53の回転が〒くなり
すぎて、上述のタイミングが不一致となり、また排気の
圧力が例えば約1,3barと低くなるため、セル54
内の圧力が低くなり、排気ガスの放出圧力が低下して、
排気ガスがセル54内に残り、吸入エアと排気ガスとの
境界線が第5図の点線すの如くなり、セル54内に残っ
た排気ガスが第4図の特製図と点線βで示すようにEG
Rとなって吸気側に還流されるので、失火が生ずる問題
点があった。
In other words, the exhaust pressure wave propagating at the speed of sound is reflected as a pressure wave at the fixed end and reversed as an expansion wave at the open end. As a result, an ideal boundary line between the intake air and the exhaust gas is formed as shown by the dotted line a in FIG. , due to the above-mentioned timing mismatch and also because the exhaust pressure is low, for example about 1.3 bar, the cell 54
The internal pressure decreases, and the exhaust gas release pressure decreases,
The exhaust gas remains in the cell 54, and the boundary line between the intake air and the exhaust gas becomes as shown by the dotted line in FIG. to EG
Since the fuel becomes R and is recirculated to the intake side, there is a problem in that a misfire occurs.

このような圧力波過給機付エンジンにおいて、従来、例
えば実開昭61−36131号公報に記載の如く、上述
の圧力波過給機をエンジンで駆動するブーり比を可変に
するブーり圧可変装置と、エンジンの負荷状態を検出す
る負荷検出手段と、該負荷検出手段の出力を受け、低負
荷域程上記ブーり比が大になるように上記プーリ比可変
装置を制御する制御手段とを設けて、エンジン回転数に
対する回転比を可変してNOxおよび燃費を改善すべく
構成した圧力波過給機付エンジンがあるが、前述の低負
荷域における高回転域の失火の改善を図ることはできな
い。
In such an engine with a pressure wave supercharger, as described in, for example, Japanese Utility Model Application Publication No. 61-36131, a boolean pressure system that changes the boolean ratio for driving the pressure wave supercharger with the engine has conventionally been used. a variable device, a load detection means for detecting the load state of the engine, and a control means for receiving the output of the load detection means and controlling the pulley ratio variable device so that the boolean ratio becomes larger in a lower load region. There is an engine equipped with a pressure wave supercharger that is configured to improve NOx and fuel efficiency by varying the rotation ratio with respect to the engine speed, but it is necessary to improve the misfire in the high rotation range in the low load range mentioned above. I can't.

(発明の目的) この発明は、排気エネルギが少ない低負荷域の高回転時
において上述の如き失火をよ防止することができる圧力
波過給機付エンジンの提供を目的とする。
(Objective of the Invention) An object of the present invention is to provide an engine with a pressure wave supercharger that can better prevent misfires as described above at high rotation speeds in a low load range where exhaust energy is small.

(発明の構成) この発明は、ケース内に回転可能に支持され、多数の小
室を形成する多数の隔壁が放射状に配設されたロータと
、該ロータの一端側のエアケーシングに形成された吸気
導入口および吸気吐出口と上記ロータの他端側のガスケ
ーシングに形成された排気導入口および排気吐出口とを
有し、上記ロータの回転に伴い排気の圧力波エネルギを
吸気に伝達して、吸気の過給を行う圧力波過給機付エン
ジンであって、エンジン出力軸に対する圧力波過給機の
回転比を低下させる回転比低下手段と、低負荷域の高回
転域で上記回転比低下手段を作動させる制御手段とを佑
えた圧力波過給機付エンジンであることを特徴とする。
(Structure of the Invention) The present invention includes a rotor that is rotatably supported within a case and has a large number of partition walls that form a large number of small chambers arranged radially, and an air intake formed in an air casing at one end of the rotor. It has an inlet and an intake outlet, and an exhaust inlet and an exhaust outlet formed in the gas casing on the other end side of the rotor, and transmits the pressure wave energy of the exhaust to the intake as the rotor rotates, An engine with a pressure wave supercharger that supercharges intake air, the engine includes a rotation ratio reducing means for reducing the rotation ratio of the pressure wave supercharger to the engine output shaft, and a rotation ratio reduction means for reducing the rotation ratio in a high rotation range in a low load range. The present invention is characterized in that the engine is equipped with a pressure wave supercharger and includes a control means for activating the pressure wave supercharger.

(発明の効果) この発明によれば、上述の制御手段で低負荷域の高回転
時に回転比低下手段を作動させて、エンジン出力軸に対
する圧力波過給機の回転比を低下させ、この圧力波過給
機のロータの回転を低減するので、吸気導入口、吸気吐
出口、排気導入口および排気吐出口の各ボートの開閉タ
イミングと、圧力波伝播のタイミングとが略マツチング
し、吸入エアと排気ガスとの境界線が理想的な状態に近
づくので、上述のロータにおける小室内の残留ガス排出
つまり掃気効率が良好となって、内部EGRを低減させ
、失火を改善することができる効果がある。
(Effects of the Invention) According to the present invention, the above-mentioned control means operates the rotation ratio reducing means at high rotation speeds in a low load range to reduce the rotation ratio of the pressure wave supercharger to the engine output shaft, thereby reducing the pressure. Since the rotation of the rotor of the wave supercharger is reduced, the opening/closing timing of each boat of the intake inlet, intake outlet, exhaust inlet, and exhaust outlet almost matches the timing of pressure wave propagation, and the intake air and Since the boundary line with the exhaust gas approaches the ideal state, the residual gas discharge in the small chamber of the rotor, that is, the scavenging efficiency, becomes good, which has the effect of reducing internal EGR and improving misfires. .

(実施例) この発明の一実施例を以下図面に基づいて詳)ホする。(Example) An embodiment of the present invention will be described in detail below with reference to the drawings.

図面は圧力波過給機付エンジンを示し、第1図、第2図
において、ディーゼルエンジン1のエンジン出力軸とし
てのクランク軸2にはクランクプーリ3、ベルト4およ
びロータプーリ5を介して圧力波過給機6いわゆるプレ
ッシャーウェーブ・スーパーチャージャのロータシャフ
ト7aを連結している。
The drawings show an engine equipped with a pressure wave supercharger, and in FIGS. A feeder 6 is connected to a rotor shaft 7a of a so-called pressure wave supercharger.

上述の圧力波過給16は第1図にロータ7の回転を下方
移動に置換した状態で示す如く、ケースく図示せず)内
に上述の〇−タフを回転可能に支持している。
The above-mentioned pressure wave supercharging 16 rotatably supports the above-mentioned 0-tough in a case (not shown), as shown in FIG. 1 with the rotation of the rotor 7 replaced by downward movement.

また上述のロータ7には多数の小室としてのセル8・・
・を形成する多数の隔壁9・・・を放射状に配設すると
共に、上述のロータ7の一端側のエアケーシング10に
は吸気導入口11および吸気吐出口12を形成し、他端
側のガスケーシング13には排気導入口14および排気
吐出口15をそれぞれ形成している。
In addition, the rotor 7 has a large number of cells 8 as small chambers.
In addition, the air casing 10 at one end of the rotor 7 is provided with an intake inlet 11 and an intake outlet 12, and the gas at the other end is disposed radially. The casing 13 is formed with an exhaust inlet 14 and an exhaust outlet 15, respectively.

さらに、上述の吸気導入口11の前位にはエアクリーナ
を、また吸気吐出口12の後位には吸気マニホルド16
をそれぞれ接続すると共に、上述の排気導入口14の前
位には排気マニホルド17を、また排気吐出口15の後
位にはサイレンサをそれぞれ接続している。
Furthermore, an air cleaner is installed in front of the above-mentioned intake inlet 11, and an intake manifold 16 is installed in the rear of the intake outlet 12.
At the same time, an exhaust manifold 17 is connected to the front side of the exhaust gas introduction port 14, and a silencer is connected to the rear side of the exhaust gas discharge port 15.

なお、第゛1図における18はコンプレッションポケッ
ト、19はエキスパンションポケット、20はガスポケ
ットである。
In addition, 18 in FIG. 1 is a compression pocket, 19 is an expansion pocket, and 20 is a gas pocket.

そして、上述の圧力波過給機6は、上述のロータ7のエ
ンジン回転数に応じた回転に伴い、吸気導入口11から
ロータ7のセル8に吸入した吸気に対して、排気導入口
14から該セル8に排気を流入させ、音速で伝播される
排気の圧力波エネルギを吸気に伝達して、吸気を圧縮、
加速して吸気吐出口12から過給吐出させる一方、上)
木のセル8内に残る排気を排気吐出口15から排出させ
ると共に、吸気導入口11から上述のセル8内に吸気を
導入することにより、掃気を行なうことを繰返す。
The above-mentioned pressure wave supercharger 6 operates from the exhaust inlet 14 to the intake air taken into the cell 8 of the rotor 7 from the intake inlet 11 as the rotor 7 rotates according to the engine speed. The exhaust gas is caused to flow into the cell 8, and the pressure wave energy of the exhaust gas propagated at the speed of sound is transmitted to the intake air to compress the intake air.
While accelerating and supercharging from the intake/discharge port 12,
The scavenging process is repeated by discharging the exhaust gas remaining in the wood cell 8 from the exhaust outlet 15 and introducing intake air into the cell 8 from the intake inlet 11.

ところで、クランク軸2に対する圧力波過給機6の回転
比を低下させる回転比低下手段としての可変プーリ装置
21は第2図に示す如く構成している。
By the way, the variable pulley device 21 as a rotation ratio reducing means for lowering the rotation ratio of the pressure wave supercharger 6 to the crankshaft 2 is constructed as shown in FIG.

すなわち、ディーゼルエンジン1側のクランク軸2に固
定溝車22を嵌合固定すると共に、この固定溝車22に
対してフライウェイト23の遠心力により可動する移動
溝車24を設けて前述のクランクプーリ3を構成し、一
方、圧力波過給機6側のロータシャフト7aに固定溝車
25を嵌合固定すると共に、この固定溝車25に対して
フライウェイト26の遠心力により可動する移動溝車2
7を設けて前述のロータプーリ5を構成し、このロータ
プーリ5と上述のクランクプーリ3との間にベルト4を
張架して、上述の可変プーリ装@21いわゆるVベルト
式無段変速装置を構成している。
That is, a fixed groove wheel 22 is fitted and fixed to the crankshaft 2 on the side of the diesel engine 1, and a movable groove wheel 24 that is movable by the centrifugal force of the flyweight 23 is provided to the fixed groove wheel 22, so that the above-mentioned crank pulley On the other hand, a fixed groove wheel 25 is fitted and fixed to the rotor shaft 7a on the side of the pressure wave supercharger 6, and a movable groove wheel is movable with respect to the fixed groove wheel 25 by the centrifugal force of a flyweight 26. 2
7 to constitute the aforementioned rotor pulley 5, and a belt 4 is stretched between the rotor pulley 5 and the aforementioned crank pulley 3 to constitute the aforementioned variable pulley system@21 so-called V-belt type continuously variable transmission. are doing.

また、ドライブ側(原動側)としての上述のクランク軸
2の軸端部には固定カバー28を取付け、この固定カバ
ー28に支点29.29を介して上述のフライウェイト
23.23を配設し、かつ上述の固定カバー28と移動
溝車24の筒軸部端面との間にはスプリング30を張架
している。
Further, a fixed cover 28 is attached to the shaft end of the above-mentioned crankshaft 2 serving as the drive side (driving side), and the above-mentioned flyweight 23.23 is disposed on this fixed cover 28 via a fulcrum 29.29. , and a spring 30 is stretched between the fixed cover 28 and the end surface of the cylindrical shaft portion of the movable grooved sheave 24.

一方、ドリブン側(従動側)としての上述のロータリシ
ャフト7aにおける移動溝車27の背面部位には固定円
板31を取付け、この固定円板31に支点32.32を
介して前述のフライウェイト26.26を配設し、かつ
上述の移動溝車27と前述の固定溝車25との対向面間
にはスプリング33を張架している。
On the other hand, a fixed disk 31 is attached to the back side of the movable groove wheel 27 on the above-mentioned rotary shaft 7a as the driven side (driven side), and the above-mentioned fly weight 26 is connected to the fixed disk 31 via a fulcrum 32.32. .26 is disposed, and a spring 33 is stretched between the facing surfaces of the movable groove sheave 27 and the fixed groove sheave 25 described above.

そして、このスプリング33と上述のフライウェイト2
6.26との両者により、低負荷域の高回転域で可変ブ
ーり装置21を作動させる制御手段を構成している。
Then, this spring 33 and the above-mentioned fly weight 2
6 and 26 constitute a control means for operating the variable boolean device 21 in a high rotation range of a low load range.

すなわち、上述のスプリング33の設定バネ力F1とし
、フライウェイト26.26の遠心力に起因するスラス
ト方向の力をF2とする時、第3図に示す如く高回転域
たとえば4300 rpmの時点以降でフライウェイト
26のスラスト力F2がスプリング33のバネ力F1を
上回って、上述の可変ブーり装@21を作動させて、ク
ランク軸2に対する圧力波過給機6の回転比を低下すべ
く構成している。
That is, when the setting spring force of the spring 33 mentioned above is F1, and the force in the thrust direction due to the centrifugal force of the flyweights 26.26 is F2, as shown in FIG. The configuration is such that when the thrust force F2 of the flyweight 26 exceeds the spring force F1 of the spring 33, the above-mentioned variable boob device @21 is operated to lower the rotation ratio of the pressure wave supercharger 6 with respect to the crankshaft 2. ing.

なお、この点に関してはスプリング30の設定バネ力と
、フライウェイト23の遠心力に起因するスラスト方向
の力にとの関係も同様に設定している。
Regarding this point, the relationship between the set spring force of the spring 30 and the force in the thrust direction caused by the centrifugal force of the flyweight 23 is similarly set.

図示実施例は上記の如く構成するものにして、以下作用
を説明する。
The illustrated embodiment is constructed as described above, and its operation will be explained below.

ディーゼルエンジン1の回転数が第3図に示すスプリン
グ3゛3の設定バネ力F1と、フライウェイト26.2
6のスラスト力F2との交点として予め設定した高回転
域、例えば、4300rpmに達すると、この時点で上
述の8力Fl、F2が等しくなり、エンジン回転数が上
述の4300rpm以上になると、フライウェイト26
.26のスラスト力F2がスプリング33の設定バネ力
F1を上回る。
The rotation speed of the diesel engine 1 is determined by the set spring force F1 of the spring 3'3 shown in FIG. 3 and the flyweight 26.2.
When reaching a preset high rotation range, for example 4300 rpm, as the point of intersection with the thrust force F2 of 6, the above-mentioned 8 forces Fl and F2 become equal at this point, and when the engine speed reaches the above-mentioned 4300 rpm or higher, the fly weight 26
.. The thrust force F2 of 26 exceeds the set spring force F1 of the spring 33.

このため上述の高回転域ではフライウェイト26.26
のスラスト力F2により、ロータプーリ5の移動溝車2
7が第2図の矢印C方向に軸動して、ロータプーリ5の
プーリ径を大きくする。
Therefore, in the high rotation range mentioned above, the flyweight is 26.26.
Due to the thrust force F2, the movable groove wheel 2 of the rotor pulley 5
7 pivots in the direction of arrow C in FIG. 2 to increase the pulley diameter of the rotor pulley 5.

また、上述の高回転域ではクランク軸2側のフライウェ
イト23.23のスラスト力により、クランクプーリ3
の移動溝車24は第2図の矢印d方向に軸動して、クラ
ンクプーリ3のブーり径を小さくする。
In addition, in the above-mentioned high rotation range, the thrust force of the fly weight 23.23 on the crankshaft 2 side causes the crank pulley 3 to
The movable grooved sheave 24 is pivoted in the direction of arrow d in FIG. 2 to reduce the diameter of the bore of the crank pulley 3.

このためクランク軸2に対する圧力波過給機6のロータ
7の回転が、例えば、通常の約4倍から約3〜3.5倍
に低下する。
For this reason, the rotation of the rotor 7 of the pressure wave supercharger 6 with respect to the crankshaft 2 decreases, for example, from about 4 times the normal rotation to about 3 to 3.5 times.

このように低負荷域の高回転域で圧力波過給機6のロー
タ7の回転が低下するので、第1図に示す吸気導入口1
1、吸気吐出口12、排気導入口14、排気吐出口15
の各ボートの開閉タイミングと、圧力波伝播のタイミン
グとが略マツチングして、吸入エアと排気ガスとの境界
線が第1図に点線aで示す理想的な状態に近づくので、
上述のロータ7におけるセル8内の残留ガス排出、つま
り掃気効果が良好となって、第4図の特性図に実線αで
示すように内部EGRが低減し、この結果、失火を改善
することができる効果がある。
In this way, the rotation of the rotor 7 of the pressure wave supercharger 6 decreases in the high speed range of the low load range, so the intake inlet 1 shown in FIG.
1, intake outlet 12, exhaust inlet 14, exhaust outlet 15
The opening/closing timing of each boat and the timing of pressure wave propagation approximately match, and the boundary line between intake air and exhaust gas approaches the ideal state shown by dotted line a in Figure 1.
The discharge of the residual gas in the cell 8 of the rotor 7 described above, that is, the scavenging effect is improved, and the internal EGR is reduced as shown by the solid line α in the characteristic diagram of FIG. 4, and as a result, the misfire can be improved. There is an effect that can be done.

この発明の構成と、上述の実施例との対応において、 この発明の小空は、実施例のセル8に対応し、以下同様
に エンジン出力軸は、クランク軸2に対応し、回転転化低
下手段は、可変プーリ装置21に対応し、 制御手段は、スプリング33およびフライウェイト26
に対応するも、 この発明は、上述の実施例の構成のみに限定されるもの
ではない。
In the correspondence between the structure of the present invention and the above-described embodiment, the small space of the present invention corresponds to the cell 8 of the embodiment, the engine output shaft corresponds to the crankshaft 2, and the rotational conversion reducing means corresponds to the variable pulley device 21, and the control means includes the spring 33 and the flyweight 26.
However, the present invention is not limited to the configuration of the above-described embodiment.

例えば、クランク軸2、もしくはロータシャフト7aの
何れか一方に電磁クラッチを介設し、低負荷域の高回転
域において、上述の電磁クラッチをON、OFF制御す
ることで、クランク@2に対する圧力波過給Ia6の回
転比を低下させるように構成してもよい。
For example, by interposing an electromagnetic clutch on either the crankshaft 2 or the rotor shaft 7a and controlling the above-mentioned electromagnetic clutch ON and OFF in a low load range and high rotation range, pressure waves on the crank @2 can be generated. The configuration may be such that the rotation ratio of supercharging Ia6 is reduced.

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

図面はこの発明の一実施例を示し、 第1図はロータの回転を下方移動に置換した状態で示す
圧力波過給機付エンジンの系統図、第2図は可変プーリ
装置の説明図、 第3図はエンジン回転数に対するスプリング力とフライ
ウェイトのスラスト力との関係を示す特性図、 第4図は無負荷時のEGR特性図である。 2・・・クランク軸    6・・・圧力波過給機7・
・・ロータ      8・・・セ ル9・・・隔 壁
      10・・・エアケーシング11・・・吸気
導入口   12・・・吸気吐出口13・・・ガスケー
シング 14・・・排気導入口15・・・排気吐出口 
  21・・・可変ブーり装置26・・・フライウェイ
ト 33・・・スプリング第2図 第3図
The drawings show an embodiment of the present invention; FIG. 1 is a system diagram of an engine equipped with a pressure wave supercharger in which rotation of the rotor is replaced with downward movement; FIG. 2 is an explanatory diagram of a variable pulley device; Fig. 3 is a characteristic diagram showing the relationship between spring force and flyweight thrust force with respect to engine speed, and Fig. 4 is an EGR characteristic diagram under no load. 2... Crankshaft 6... Pressure wave supercharger 7.
...Rotor 8...Cell 9...Partition wall 10...Air casing 11...Intake inlet 12...Intake discharge port 13...Gas casing 14...Exhaust inlet 15...・Exhaust outlet
21... Variable boolean device 26... Fly weight 33... Spring Figure 2 Figure 3

Claims (1)

【特許請求の範囲】[Claims] (1)ケース内に回転可能に支持され、多数の小室を形
成する多数の隔壁が放射状に配設さ れたロータと、 該ロータの一端側のエアケーシングに形成 された吸気導入口および吸気吐出口と 上記ロータの他端側のガスケーシングに形 成された排気導入口および排気吐出口とを 有し、 上記ロータの回転に伴い排気の圧力波エネ ルギを吸気に伝達して、吸気の過給を行う 圧力波過給機付エンジンであつて、 エンジン出力軸に対する圧力波過給機の回 転比を低下させる回転比低下手段と、 低負荷域の高回転域で上記回転比低下手段 を作動させる制御手段とを備えた 圧力波過給機付エンジン。
(1) A rotor that is rotatably supported within a case and has a number of partition walls arranged radially to form a number of small chambers, and an intake inlet and an intake outlet formed in an air casing at one end of the rotor. and an exhaust inlet and an exhaust outlet formed in the gas casing at the other end of the rotor, and supercharges the intake by transmitting the pressure wave energy of the exhaust to the intake as the rotor rotates. An engine with a pressure wave supercharger, comprising a rotation ratio reducing means for reducing the rotation ratio of the pressure wave supercharger to the engine output shaft, and a control means for operating the rotation ratio reducing means in a high rotation range in a low load region. An engine with a pressure wave supercharger.
JP2169788A 1988-01-30 1988-01-30 Engine provided with pressure wave supercharger Pending JPH01195919A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2169788A JPH01195919A (en) 1988-01-30 1988-01-30 Engine provided with pressure wave supercharger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2169788A JPH01195919A (en) 1988-01-30 1988-01-30 Engine provided with pressure wave supercharger

Publications (1)

Publication Number Publication Date
JPH01195919A true JPH01195919A (en) 1989-08-07

Family

ID=12062262

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2169788A Pending JPH01195919A (en) 1988-01-30 1988-01-30 Engine provided with pressure wave supercharger

Country Status (1)

Country Link
JP (1) JPH01195919A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010085483A2 (en) * 2009-01-22 2010-07-29 Orbital Traction, Ltd. Fluid movement systems including a continuously variable transmission
JP2011094550A (en) * 2009-10-30 2011-05-12 Toyota Motor Corp Supercharging device for internal combustion engine

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010085483A2 (en) * 2009-01-22 2010-07-29 Orbital Traction, Ltd. Fluid movement systems including a continuously variable transmission
WO2010085483A3 (en) * 2009-01-22 2010-09-16 Orbital Traction, Ltd. Fluid movement systems including a continuously variable transmission
US9464701B2 (en) 2009-01-22 2016-10-11 Orbital Traction, Ltd. Fluid movement systems including a continuously variable transmission
US10006526B2 (en) 2009-01-22 2018-06-26 Orbital Traction, Ltd. Fluid movement systems including a continuosly variable transmission
US10443692B2 (en) 2009-01-22 2019-10-15 Orbital Traction, Ltd. Fluid movement systems including a continuously variable transmission
JP2011094550A (en) * 2009-10-30 2011-05-12 Toyota Motor Corp Supercharging device for internal combustion engine

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