JPS6093124A - Intake device of rotary piston engine - Google Patents
Intake device of rotary piston engineInfo
- Publication number
- JPS6093124A JPS6093124A JP58202304A JP20230483A JPS6093124A JP S6093124 A JPS6093124 A JP S6093124A JP 58202304 A JP58202304 A JP 58202304A JP 20230483 A JP20230483 A JP 20230483A JP S6093124 A JPS6093124 A JP S6093124A
- Authority
- JP
- Japan
- Prior art keywords
- pressure
- intake
- chamber
- throttle
- actuator
- 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
Links
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
- F02B53/04—Charge admission or combustion-gas discharge
-
- 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
- F02B53/06—Valve control therefor
-
- 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)
- Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)
Abstract
Description
【発明の詳細な説明】
(産業上の利用分野)
本発明はロータリビス[−ンエンジンの吸気装置−1−
に関し、どくにり゛−シングに軽負荷用吸気ボー1へお
よび高負荷用吸気ボートを間口させて、ダイヤフラム式
のアクヂコエータで作動される開閉弁ににす上記高負荷
用吸気ボートを高負荷時に開くようにした吸気装置の改
良に関するものである。Detailed Description of the Invention (Field of Industrial Application) The present invention relates to an intake system for a rotary rev engine. The present invention relates to an improvement in an intake device in which the intake boat for high loads is opened at high loads by widening the boat and using an on-off valve operated by a diaphragm type actuator.
(従来技術)
従来、ロータリピストンエンジンにおいては、全運転域
で作動室に吸気を供給する軽負荷用吸気ボー1〜と高負
荷時にのみ作動室に吸気を供給する高負荷用吸気ボー1
−とを作動室に間口させ、軽負荷域における燃費性と高
負荷域における出力性能を同時に満足するようにした装
置が知られている。(Prior art) Conventionally, in a rotary piston engine, there are two intake bows 1 to 1 for light loads that supply intake air to the working chamber in all operating ranges and intake bows 1 for high loads that supply intake air to the working chamber only during high loads.
- is opened into the working chamber, and a device is known that simultaneously satisfies fuel efficiency in a light load range and output performance in a high load range.
例えば持分tlr(5749735弓公報tこ示された
装置では、上記両吸気ボートを備えるとともに、ざらに
中負荷域以上で作動室に吸気を供給する中負荷用吸気ボ
ー1−を設け、各運転域に応じた適切な吸気が行われる
ようにしている。この秤の吸気装置では、ロータの回転
に伴って高負荷用吸気ボートが軽負荷用吸気ポー1−よ
りも遅れて閉じるようにするとともに、上記高負荷用吸
気ボートが、−2−
ダイA7フラム式のアクチュエータで作動される開閉弁
によって高負荷時にのみ間かれるようになっ−Cいる。For example, the device shown in the 5749735 bow publication is equipped with both of the above-mentioned intake boats, and is provided with a medium-load intake boat 1- which supplies intake air to the working chamber in the medium-load range or above, and In the intake system of this scale, the intake boat for high load closes later than the intake port 1 for light load as the rotor rotates. The above-mentioned high-load intake boat is connected only at high loads by an on-off valve operated by a die A7 flam type actuator.
つまり、エンジン負荷および回転数に応じて圧力が変化
する排気ガス等の圧力流体を上記アクヂコ丁−夕の圧力
室に導入し、この圧ノ)室内の圧力が設定値未満のとき
には上記開閉弁を閉じ、上記圧力が設定値Jス上のどき
には開閉弁を聞< 、lうにしている。そして上記圧力
の設定値はアクチュエータに具[6されたスプリング等
で予め調整され、この用台に負荷がかなり高くなっても
高負荷用吸気ボー1〜が聞かれ4「ければ出力不足が生
じ、また不必要に負荷お」:び回転数が低いときから高
負荷用吸気ボーi〜が聞かれても、吹き返し等により充
填率が低下づるので、これらの点を考慮して上記設定値
は出力面で最適な値に調整される。In other words, a pressure fluid such as exhaust gas whose pressure changes depending on the engine load and rotation speed is introduced into the pressure chamber of the above-mentioned acupuncture chamber, and when the pressure inside this pressure chamber is less than a set value, the above-mentioned on-off valve is turned on. When the pressure is above the set value, the on-off valve is turned on. The set value of the above pressure is adjusted in advance using a spring etc. attached to the actuator, so that even if the load on this table becomes quite high, if the high load intake bow is 1 to 4, the output will be insufficient. In addition, even if high-load intake air is heard at low rotational speeds, the filling rate will decrease due to blowback, etc., so the above setting values are set with these points in mind. Adjusted to the optimal value on the output side.
ところで、通常このような装置では、1」1気ガス圧力
等の脈動にJ:って定常運転時にお【プるアクチュエー
タの作動が不安定になることを防止するため、」−記圧
力室への圧力流体導入通路に絞りを設c′Jでいる。こ
のJ:うにした場合、加速運転時には−3−
上記絞りより上流のjJl気ガス圧力が急激に変化する
のに対し、上記圧力室内の圧力はある程疫の遅れをもっ
て変化することとなるので、加速運転時と定常運転時と
で、上記アクチュエータにJ、るf7Fl閉弁作V]領
域にずれが生じ、上記両運転時のいずれにおいても最適
な開閉弁作動領域を与えるように設定して(b <こと
はグIIJ l、い。このため従来では、例えば加速時
の出力性能の要求を重視して、加速時に最適>’r聞閏
弁作動領域が(qられるように予め前記設定値を調整す
る等により、」上記の作動領域のヂれに対処していた。By the way, normally in such a device, in order to prevent the operation of the actuator from becoming unstable during steady operation due to pulsations such as 1 atmosphere gas pressure, the pressure chamber is A restriction is provided in the pressure fluid introduction passage c'J. In this case, during acceleration operation, the pressure in the pressure chamber upstream of the throttle changes rapidly, while the pressure in the pressure chamber changes with a certain delay. There is a difference in the valve closing operation range of the actuator between acceleration operation and steady operation, so the setting is made to give the optimum opening/closing valve operation area during both of the above operations. For this reason, in the past, for example, emphasis was placed on output performance requirements during acceleration, and the setting value was set in advance so that the optimal leap valve operating range during acceleration was set. The above-mentioned deviation in the operating range was addressed by making adjustments, etc.
(発明の目的)
本発明はこねらの事情に鑑み、高負荷用吸気ボートの開
閉弁を作動1−るアクチュエータへの圧力流体導入通路
に絞りを設けたしのにおいて、加速運転時と定常運転時
とにおける開閉弁作動領域のずれをなくし、上記の両運
転時のいずれにおいても良θTな出力性能を与えること
のできるロータリビス1ヘンエンジンの吸気装置を提供
づるものである。(Object of the Invention) In view of the above circumstances, the present invention provides a restriction in the pressure fluid introduction passage to the actuator that operates the on-off valve of the intake boat for high loads, and it is possible to reduce the pressure during acceleration operation and during steady operation. An object of the present invention is to provide an intake system for a rotary vis 1-hen engine that can eliminate deviations in the operating range of an on-off valve between different times and provide good θT output performance during both of the above-mentioned operations.
−4−
(発明の構成)
本発明は、ケーシングに軽負荷用吸気ボー1− A3に
び高負荷用吸気ボートを開口させ、ロータの回転に伴っ
て高(1荷用吸気ポートが軽負荷用吸気ボー l−J:
りも遅れて閉じられるJzうに上記両ボー1〜を配設4
るとともに、上記高負荷用吸気ボートを開閉するflt
l閉弁とこの開閉弁を高負荷時に開くグイ(/フラム式
のアクデーlエータとを装備し、このアクチュエータの
圧力室への圧力流体導入通路に絞り部を設(]たロロー
タリピストンエンジにおいて1.IZ記絞り部J:り上
流の圧力流体の圧力変化に対す゛るアクチュエータの作
動遅れを運転状態に応じて補正する補正手段を設けたも
のである。つまり」ニ記補正f段ににす、加速運転時の
開閉弁作動領域を定常運転時の作動領域とほぼ一致させ
るようにしたものである。なお、上記アクチュエータを
作動する圧力流体としては排気ガスあるいは吸気負圧等
を採用づることができる。-4- (Structure of the Invention) The present invention has the light load intake port 1-A3 and the high load intake boat opened in the casing, and as the rotor rotates, the high load intake port Intake bow l-J:
The above JZ sea urchin is also closed late, and the above two bows 1~4
At the same time, the flt opens and closes the high-load intake boat.
In a rotary piston engine that is equipped with a closed valve and a flam-type actuator that opens this on-off valve at high loads, and a throttle section is installed in the pressure fluid introduction passage to the pressure chamber of this actuator. 1. Restriction part J indicated by IZ: A correction means is provided to correct the delay in actuator operation in response to pressure changes in the upstream pressure fluid according to the operating condition. The operating range of the on-off valve during accelerated operation is made to almost match the operating range during steady operation.Exhaust gas or intake negative pressure may be used as the pressure fluid for operating the actuator. can.
(実流例)
第1図において、1はロータリピストンエンジー 5
−
ンのケーシングであ−〕で、トロコイド状の内周面を有
ηるロータハウジング2とぞの両側に配設された1ノイ
ドハウジング3(一方の4ノイドハウジングは図示せず
)とで構成されている。このケーシング1内には、図外
の偏心軸に支承された多角形状のロータ4が装備されて
いる。このロータ4は頂辺がロータハウジング2の内周
面に摺接しつつM早回転運動し、ケーシング1内に作動
室5を区画形成している。(Actual flow example) In Figure 1, 1 is a rotary piston engine 5
- A rotor housing 2 having a trochoidal inner circumferential surface, and a 1-noid housing 3 (one 4-noid housing is not shown) disposed on both sides of the rotor housing 2. has been done. The casing 1 is equipped with a polygonal rotor 4 supported by an eccentric shaft (not shown). The rotor 4 rotates rapidly M while its top side is in sliding contact with the inner circumferential surface of the rotor housing 2, and defines a working chamber 5 within the casing 1.
上記ケーシング1内には少なくとも軽負荷用吸気ボート
6と高負荷用吸気ボート8とが680し、図に示J実施
例では、一方のサイドハウジングに形成された軽負荷用
吸気ボート6と、他方のサイドハウジング3に形成され
た中負荷用吸気ボー1〜7および高負荷用吸気ボー1−
8の三つのボー]・が開口している。イして軽負荷用吸
気ボート6と中負荷用吸気ボー]〜7とはロータ4の回
転に伴って同じタイミングで開閉されるように両サイド
ハウジングの対応する位置に設けられ、高負荷用吸気ボ
ー1−8は軽負荷用おにび中負荷用の各吸気ボー−6−
1・6,7J:りもjYれて閉じる位置に設()られて
いる。上記性CJ vi用吸気ボート6は、全運転域で
作動する一次絞り弁10を備えた一次側吸気通路11に
接続され、中負荷用および高負荷用の各吸気ボー1〜7
.8は、中負荷域おJ:び高負荷域で聞かれる二次絞り
弁12を備えた二次側吸気通路13に接続されている。Inside the casing 1, there are at least a light load intake boat 6 and a high load intake boat 8 680, and in the J embodiment shown in the figure, the light load intake boat 6 formed in one side housing and the other Medium-load intake bows 1 to 7 and high-load intake bows 1- are formed on the side housing 3 of
The three bows of 8] are open. The intake boats 6 for light loads and the intake boats for medium loads] to 7 are provided at corresponding positions on both side housings so that they open and close at the same timing as the rotor 4 rotates. The bows 1-8 are provided in the closed positions of the intake bows 6-1, 6, and 7J for light loads and medium loads. The above-mentioned intake boat 6 for the CJ vi is connected to a primary side intake passage 11 equipped with a primary throttle valve 10 that operates in all operating ranges, and is connected to each intake boat 1 to 7 for medium load and high load.
.. 8 is connected to a secondary intake passage 13 equipped with a secondary throttle valve 12 which is heard in the medium load region and high load region.
また−Jl記高負荷用吸気ボー1−〇に(ま、この吸気
ボート8を高負荷時に開く開閉弁15が段(〕られてい
る。こうして、軽負荷域では軽負荷用吸気ボー1−6の
みから吸気が行われ、中負荷域以上では二次絞り弁12
が聞かれて中負荷用吸気ボー1−7からも吸気が行われ
、さらに高負荷時には上記開閉弁15が聞かれて高負荷
用吸気ボー1へ8からも吸気が行われるようにし、軽重
荷時の燃費性おJ:び高負荷時の出力性能の向上を図る
にうにしている。In addition, an opening/closing valve 15 that opens this intake boat 8 at high load is installed in the intake bow 1-0 for high load in Jl. Intake is performed only from the secondary throttle valve 12 in the middle load range and above.
is heard so that air is taken in from intake bows 1-7 for medium loads, and when the load is high, the on-off valve 15 is turned on so that air is also taken from intake bows 1 and 8 for high loads. The engine is designed to improve fuel efficiency and output performance under high loads.
上記開閉弁15は、円筒状に形成されて高負荷用吸気ボ
ー1−8に回転自在に挿入され、その周壁に聞1]部1
5aを有し、回転に伴って高角筒用吸気ボー1−8の作
動室側聞口部8aを開閉するJ:う−7−
になっている。そしてこの開閉弁15 tJ: 、ロッ
ド16、レバー17、リンク18およびシャツ1−19
を介してグイA7フラム式のアクチュエータ20で作動
されるにうにしている。The on-off valve 15 is formed into a cylindrical shape and is rotatably inserted into the high-load intake bow 1-8, and has a portion 1 attached to its peripheral wall.
5a, and opens and closes the working chamber side port 8a of the high-angle cylinder intake bow 1-8 as it rotates. And this on-off valve 15 tJ: , rod 16, lever 17, link 18 and shirt 1-19
It is designed to be actuated by a Gui A7 flam type actuator 20 via.
上記アクチュエータ20は、開閉弁作動用の圧力流体を
導入する圧力室21と、大気室22と、補正1段どして
動く減圧室23とを備え、これらの室21,22.23
が第1および第2のダイヤフラム24,25で仕切られ
た二重ダイヤフラム構造どなっており、上記圧力室21
と大気室22とを仕切る第1のダイヤフラム27Iに前
記シVlフ1〜19が連結されている。この第1のダイ
ヤフラム24は、大気室22に装備されたスプリング2
6により、大気室22と減圧室23どを仕切る第2のダ
イ(/フラム25に対しで弾性的に支持されて、前記n
H開閉弁5を閉じる方向に付勢されている。また第2の
ダイヤフラム25は減圧室23に装備されたスプリング
27により弾性的に支持され、このスプリング27は大
気室22に段(〕らねたスプリング26よりも弾発力が
強く設定されて−8−
いる。The actuator 20 includes a pressure chamber 21 that introduces pressure fluid for operating an on-off valve, an atmospheric chamber 22, and a decompression chamber 23 that moves in one correction step.
has a double diaphragm structure partitioned by first and second diaphragms 24 and 25, and the pressure chamber 21
The shields 1 to 19 are connected to a first diaphragm 27I that partitions the air chamber 22 and the air chamber 22. This first diaphragm 24 is connected to a spring 2 installed in the atmospheric chamber 22.
6 is elastically supported by the second die (/flamm 25) that partitions the atmospheric chamber 22 and the decompression chamber 23, etc.
The H on-off valve 5 is biased in the direction of closing. Further, the second diaphragm 25 is elastically supported by a spring 27 installed in the decompression chamber 23, and this spring 27 is set to have a stronger elastic force than the spring 26 which is parallel to the atmospheric chamber 22. 8- There is.
上記アクチュエータ20にA3ける圧力室21には図外
の排気通路から、JT力流体どしてのIノ+気ガスが圧
力流体導入通路28を介して導入され、この圧力流体導
入通路28には絞り2つが設けられ、圧力室21に導入
される排圧の脈動が上記絞り29によって吸収されるJ
:うにしている。大気室22には人気への間口部30が
設【ノられて、この室22内は常時大気圧に保たれてい
る。また減圧室23は、負圧導入通路31を介して一次
絞り弁10より下流の一次側吸気通路11に接続され、
上記で1圧導入通路31には三方電磁弁32が設けられ
ている。この三方電磁弁32は、エンジン回転数が所定
回転数(例えば250Orpm>以下のとぎに閉じる回
転数検出スイッチ33に電気的に接続され、所定回転数
以下のとぎは一次側吸気通路11内の吸気負圧を上記減
圧室23に導入し、所定回転数J:り高くなったとぎ負
圧導入通路31を閉じて大気を上記減圧v23に導入す
るようにしである。この三方電磁弁32と減圧室23ど
の−9−
間の通路31aには絞り34が設(〕られている。Input gas such as JT force fluid is introduced into the pressure chamber 21 in A3 of the actuator 20 from an exhaust passage (not shown) via a pressure fluid introduction passage 28. Two throttles are provided, and the pulsations of the exhaust pressure introduced into the pressure chamber 21 are absorbed by the throttle 29.
: I'm trying to do it. The atmospheric chamber 22 is provided with an opening 30, and the inside of this chamber 22 is always maintained at atmospheric pressure. Further, the decompression chamber 23 is connected to the primary side intake passage 11 downstream from the primary throttle valve 10 via a negative pressure introduction passage 31,
In the above, the one-pressure introduction passage 31 is provided with a three-way solenoid valve 32. This three-way solenoid valve 32 is electrically connected to a rotation speed detection switch 33 that closes when the engine rotation speed is below a predetermined rotation speed (for example, 250 rpm). Negative pressure is introduced into the decompression chamber 23, and when the predetermined rotational speed J is increased, the negative pressure introduction passage 31 is closed and the atmosphere is introduced into the decompression chamber 23.This three-way solenoid valve 32 and the depressurization chamber A throttle 34 is provided in the passage 31a between 23 and -9-.
なお、36は気化器の一次側ベンチコリ部、37は二次
側ベンチ1り部、3Bはフロー1〜室、39はメインジ
丁ツl−1/10はエアブリード、41は一次側メイン
ノズル(二次側は図示せず)である。In addition, 36 is the primary side bench stiffness part of the carburetor, 37 is the secondary side bench 1 part, 3B is the flow 1 to chamber, 39 is the main jet 1/10 is the air bleed, and 41 is the primary side main nozzle ( The secondary side is not shown).
第2図は、この吸1気装置において高負荷用吸気ボー1
〜8が閉じられている場合と開かれた場合とにつき、吸
気負圧(大気圧との圧力差)をパラメータとしてエンジ
ン回転数に対応づけた作動室内の平均有効圧力の特性を
曲線A1〜D171′3よびΔ2〜C2で示している。Figure 2 shows the high-load intake bow 1 in this intake system.
Curves A1 to D171 show the characteristics of the average effective pressure in the working chamber that corresponds to the engine speed using the intake negative pressure (pressure difference from atmospheric pressure) as a parameter, for when ~8 is closed and when it is opened. '3 and Δ2~C2.
すなわら、高負荷用吸気ボー1−〇が閉じられている場
合、種々の吸気負圧においてエンジン回転数と平均有効
圧力どの関係は曲線Δ1〜D1に示71 J:うになり
、高負荷用吸気ボー1−8が開かれた場合は、上記の曲
線Δ1〜C1で示寸特性がそれぞれ曲線A2〜C2に示
す特性に変化する。また同図において、一点鎖線E。In other words, when intake bow 1-0 for high load is closed, the relationship between engine speed and average effective pressure at various intake negative pressures is shown in curves Δ1 to D1. When the intake bows 1-8 are opened, the dimensional characteristics of the curves Δ1 to C1 described above change to those shown by the curves A2 to C2, respectively. Also, in the same figure, a dashed dotted line E.
「はそれぞれ排圧が300 mm l−l g、80m
m1l[Jのラインを示づ。そして、上記減圧室23内
のスプー 1〇 −
リング27【J族滅圧室23に作用J−る吸気負圧が−
200mm HQ以下(第2図のラインC1より上側)
で伸び、イれ以上(第2図のラインC1より下側)では
縮むJ、うにでのバネ力が設定されている。さらにII
IO20mm l−10のライン[と吸気負圧−200
mm HQのラインC1との交点にお(づる1292回
転数は上記回転数検出スイッチ33が閉じる回転数(2
50Orpm)と一致するように設定されている。この
図から解るJ:うに、特性曲線へ1 とA2 、B1
と82、C1とC2がそれぞれ交Z−りる点で高角?I
ム用吸気ボー1〜8を間<j;うにづることが出ノj的
に最も右利であって、これは排圧が【沫ぼ300 mm
11CJの場合に相当する。このような特(’lに基
づき、前記アクチュエータ20は、イの減圧室23が大
気圧となっている状態で圧力室21(、二所定値(30
0mm HQ )以上の排圧が導入されたとぎ、第1の
ダイヤフラム2/4が大気室22側に押されて前記開閉
弁15を開作動するように予め設定されている。また第
2図において、しは上記減圧室23に吸気負圧が導入さ
れる回転−11−
数領域、1−1は減圧室23に人気が4を人される回転
数領域を示(〕ている。"The exhaust pressure is 300 mm l-l g and 80 m, respectively.
m1l [J line is shown. Then, the intake negative pressure acting on the J group depressurization chamber 23 is
200mm HQ or less (above line C1 in Figure 2)
The spring force is set at J, which expands at 200 degrees and contracts at more than 200 degrees (below line C1 in Figure 2). Further II
IO20mm l-10 line [and intake negative pressure -200
mm At the intersection with line C1 of HQ (1292 rotation speed is the rotation speed (2
50Orpm). From this figure, you can understand J: sea urchin, characteristic curve 1, A2, B1
And 82, is the high angle at the point where C1 and C2 intersect each other? I
The most advantageous method is to set the air intake bows 1 to 8 between <j;
This corresponds to the case of 11CJ. Based on such a characteristic ('1), the actuator 20 operates to maintain the pressure chamber 21 (2) at a predetermined value (30
It is preset that when an exhaust pressure of 0 mm HQ or more is introduced, the first diaphragm 2/4 is pushed toward the atmospheric chamber 22 and opens the on-off valve 15. Furthermore, in FIG. 2, 1-1 indicates a rotation speed range in which intake negative pressure is introduced into the decompression chamber 23, and 1-1 indicates a rotation speed range in which the pressure reduction chamber 23 is popular. There is.
この吸気装胃におい−(は、エンジン回転数が所定回転
数(250Or l) m )以下であるどきアクヂ]
T−タ20のg圧923に三方電磁弁32を介して吸気
負圧が導入されており、この状態では第2のダイヤフラ
ノ\25が吸引されて、第1のダイ穐7フラム24に対
する支持力が弱められ、すなわち、スプリング26のバ
ネ力が弱められるため、上記開閉弁15を開作動するに
要する作動圧力が引下げられ、例えば前記圧力室21に
導入される排圧が80 mm l−4CI程度でも開閉
弁15が開作動されるしのであるが、このような低回転
域で低速運転されている場合は排圧も80 mm HQ
J:りも充分に低いため間開ブ↑151ま開作動され
ない。!Z il’、3、エンジン回転数が250Or
pm以下で、かつ排圧が80 mm l−I Q以−1
−の運転域では、吸気負圧が−200mm l−10以
下であるため、減圧室23のスプリング27のバネツノ
が吸気負圧に打勝ってダイヤフラム25は上方(fl’
flにあり、したがって、1)1圧−12−
が80mmNG以上であっても開閉弁15は聞かない。In this intake stomach, when the engine rotation speed is below the predetermined rotation speed (250Orl) m)
Intake negative pressure is introduced into the g pressure 923 of the T-tor 20 via the three-way solenoid valve 32, and in this state, the second diaphragm \25 is attracted and supports the first diaphragm 7 flam 24. Since the force is weakened, that is, the spring force of the spring 26 is weakened, the operating pressure required to open the on-off valve 15 is lowered, and for example, the exhaust pressure introduced into the pressure chamber 21 is reduced to 80 mm l-4CI. Although the on-off valve 15 will be opened even if the engine is running at such a low speed, the exhaust pressure will also be 80 mm HQ.
J: Since the temperature is sufficiently low, the gap is not opened until ↑151. ! Z il', 3, engine speed is 250 Or
pm or less and the exhaust pressure is 80 mm l-I Q-1
In the - operating range, the intake negative pressure is less than -200 mm l-10, so the spring horn of the spring 27 of the decompression chamber 23 overcomes the intake negative pressure, and the diaphragm 25 moves upward (fl'
Therefore, even if 1) 1 pressure -12- is 80 mmNG or more, the on-off valve 15 is not heard.
そして所定回転数以上の運転域では」二記減圧室23に
大気圧が導入される。従って排圧の変動が緩史かな定常
運転状態では、排圧が前記所定値(300tnm I−
l (J )以−1−となったどき、この圧力がアクチ
ュエータ20の圧力室21に導入されることにより前記
開閉弁15が間かれ、高負荷用吸気ボーl〜8 ′/J
日ろ吸気が行われる。In the operating range above a predetermined rotation speed, atmospheric pressure is introduced into the decompression chamber 23. Therefore, under steady operating conditions in which exhaust pressure fluctuations are slow, the exhaust pressure is at the predetermined value (300 tnm I-
1 (J), this pressure is introduced into the pressure chamber 21 of the actuator 20, thereby closing the on-off valve 15, and the high-load intake ball l~8'/J
Hiro-inspiration is performed.
また排圧が急激に変化覆る加速運転時には、前記圧力流
体導入通路28に設けられた絞り29にJ:って圧力室
21内の圧力変化が遅らされるため、この較り29より
も上流側の排圧が前記所定値にjヱしても、圧力室21
内はこれにり低い圧力となる。一方、この加速運転時に
は絞り34により前記減圧室23内が大気圧になるまで
にも適度のjテれが生じ、つまり、所定回転数に達する
までは加速前の吸気負圧が上記減圧室23内に導入され
ており、所定回転数に達して前記三方電磁弁32が大気
導入状態に切替わってからち、三方電磁弁32と減圧室
23との間の絞り34によって大気が−13−
徐/Zに減圧室23に導入される。従って、排圧変化に
対する圧力室21内の圧力の応答遅れに見合う程度の期
間ば減圧室23に負圧が残存し、これににってアクチュ
エータ20の作動圧力が引下げられるため、定常時とほ
ぼ同様に排圧が所定値に達すれば聞1′!I弁15が開
作動される。このようにして加速時のアクチュエータ2
0の作動遅れが補正されることとなる。In addition, during acceleration operation in which the exhaust pressure changes rapidly, the pressure change in the pressure chamber 21 is delayed by the throttle 29 provided in the pressure fluid introduction passage 28. Even if the side exhaust pressure reaches the predetermined value, the pressure chamber 21
The pressure inside is lower than this. On the other hand, during this acceleration operation, a moderate amount of j-tangle occurs before the inside of the decompression chamber 23 reaches atmospheric pressure due to the throttle 34. In other words, until the predetermined rotational speed is reached, the intake negative pressure before acceleration is reduced to the decompression chamber 23. After the three-way solenoid valve 32 switches to the atmosphere introduction state upon reaching a predetermined rotational speed, the atmosphere is gradually reduced by the throttle 34 between the three-way solenoid valve 32 and the decompression chamber 23. /Z is introduced into the decompression chamber 23. Therefore, negative pressure remains in the decompression chamber 23 for a period corresponding to the response delay of the pressure in the pressure chamber 21 to changes in exhaust pressure, and this reduces the operating pressure of the actuator 20, so that it is almost equal to the normal state. Similarly, if the exhaust pressure reaches a predetermined value, it's 1'! I valve 15 is operated to open. In this way, actuator 2 during acceleration
0 actuation delay will be corrected.
なお、上記実施例において、負圧導入通路31にエンジ
ン回転数で制御される三方電磁弁を設()たのは、第2
図からも明らかなように、排圧が80〜300 mtn
HC1間でかつ吸気負圧が−200mmF+a以上の
定常運転時において開閉弁15が開くのを防止Jるため
である。In the above embodiment, the reason why the three-way solenoid valve controlled by the engine speed was provided in the negative pressure introduction passage 31 was due to the second
As is clear from the figure, the exhaust pressure is 80 to 300 mtn.
This is to prevent the opening/closing valve 15 from opening during steady operation between HC1 and when the intake negative pressure is -200 mmF+a or higher.
第3図は加速時のアクチュエータの作動遅れを補正する
補正手段の別の実施例を示す。この実施例に43いて、
高負荷用吸気ポートの開閉弁を作動するアクチュエータ
50は、圧力室51および大気室52どこれらを仕切る
ダイヤフラム53とを備え、このダイヤフラム53にシ
ャツ]へ19が連−14−
結され、人気室52にスプリング54が狡備されており
、これらの構造(J従来のこの秤吸気装置m(Jお【〕
るアクチコエー夕と同様で゛ある。ただIノ、ト配圧力
室51に対する圧力流体導入通路55の絞り56より−
に流と上記圧力室51との間に、絞りを有しないバイパ
ス通路57がH2tJられている。。FIG. 3 shows another embodiment of the correction means for correcting the delay in actuator operation during acceleration. In this example, there are 43
The actuator 50 that operates the on-off valve of the high-load intake port includes a pressure chamber 51 and an atmospheric chamber 52, and a diaphragm 53 that partitions them. 52 is equipped with a spring 54, and these structures (J)
It is similar to the actico air conditioner. However, from the throttle 56 of the pressure fluid introduction passage 55 to the distribution pressure chamber 51 -
A bypass passage 57 without a restriction is provided between the flow and the pressure chamber 51. .
そしてこのバイパス通路57に(J、この通路57を開
閉する電磁弁58が設(Jられ、この電磁弁58は加速
I〕/ザ59からの侶舅に応し、加速)T転時にのみ上
記バイパス通路57を開くようにしている。This bypass passage 57 is provided with a solenoid valve 58 that opens and closes this passage 57. The bypass passage 57 is opened.
この実施例にJ:ると、定常運転時に1.11.十記較
り56を通Iノて刊圧がアクチコエータの圧ノ〕室51
に導入されることにj二りj′)1圧の脈fj+が吸収
され、加速運転ONには上記バイパス通路57が間かれ
ることにj−リ、排圧が圧力室51内に速やかに導入さ
れ、加速時の作動遅れが防止されることとなる。In this example, 1.11. Through comparison 56, the pressure is the pressure of the acticoator chamber 51
When the acceleration operation is turned on, the bypass passage 57 is inserted, and the exhaust pressure is quickly introduced into the pressure chamber 51. This will prevent delays in operation during acceleration.
(発明の効果)
以上のように本発明【よ、高n荷用吸気ポー1〜を開閉
づるダイヤフラム式のアクチコエータに対し−15−
て圧力流体を導入づる圧力流体)9人通路に絞りを設け
たものにおいて、絞りより上流の圧力流体の圧力が怨激
に弯化したとき、これに伴うアクブコ]二一夕の作動遅
れが補正手段によって補正されるJ−うにしている。こ
のため、定常)T転時と加)*運転時とで上記開閉弁の
作動領域がずれることを防IVL、いずれの運転時にも
出力性OLを向上覆ることができるものである。(Effects of the Invention) As described above, the present invention [pressure fluid that introduces pressure fluid into the diaphragm type acticoator that opens and closes the intake port 1 for high loads] provides a restriction in the passage for nine people. In this system, when the pressure of the pressurized fluid upstream of the throttle increases sharply, the two-and-one-night delay in operation caused by this is compensated for by the compensation means. Therefore, it is possible to prevent the operating range of the on-off valve from shifting between the steady (T) rotation and the +) * operation, and to improve the output performance OL during either operation.
第1図11本発明の一実施例を示づ要部断面側面図、第
2図は吸気0圧J3よびTンジン回転数に応じた平均有
効圧ツノの特性図、第3図は補正手段の別の例を示す要
部の断面図である。
1・・・ロータリピストンTンジンのケーシング、6・
・・Vl負荷用吸気ボート、8・・・高角筒用吸気ボー
1−115・・・開閉弁、20.50・・・アクチユエ
ータ、21.51・・・圧力室、23・・・減圧室、2
8.55・・・圧力流体導入通路、29.56・・・絞
り、57・・・バイパス通路。
−16−
第 2 図
181″
ずり
肩 、/ ・ A・
讐7タ β7
カ
外
(竪μ さ
ダ \ ろ
#′
5;′
とl 、
・□
/°)
34? 虫
第 3 図
−11:16−Fig. 11 is a cross-sectional side view of essential parts showing an embodiment of the present invention, Fig. 2 is a characteristic diagram of the mean effective pressure horn according to the zero intake pressure J3 and the T engine rotation speed, and Fig. 3 is a diagram of the correction means. It is a sectional view of the principal part showing another example. 1...Rotary piston T engine casing, 6.
...Intake boat for Vl load, 8...Intake boat for high angle cylinder 1-115...Opening/closing valve, 20.50...Actuator, 21.51...Pressure chamber, 23...Decompression chamber, 2
8.55... Pressure fluid introduction passage, 29.56... Throttle, 57... Bypass passage. -16- No. 2 Fig. 181'' Shear shoulder, / ・ A・ enemy7ta β7 outside (vertical μ Sada \ ro#'5;' and l, ・□ /°) 34? Insect No. 3 Fig.-11: 16-
Claims (1)
用吸気ボートを開口させ、ロータの回転に伴って高負荷
用吸気ボートが軽負荷用吸気ボー1〜よりも遅れて閉じ
られるように上記両ポー1〜を配設りるとと−しに、上
記高負荷用吸気ボーl〜を開閉16開閉弁とこの開閉弁
を高負荷時に聞くダイヤフラム式のアクブ]■−夕とを
装備し、このアクチー1エータの圧力室への圧力流(4
導入通路に絞り部を設置シ1こロータリピストンエンジ
ンにおいて、」二記絞り部より上流の圧力流体の圧力変
化に対するアクヂ]−ュータの作動遅れを運転状態に応
じて補正する補正手段を饅Gプ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。1. Open the light-load intake boats 1 to J: and the high-load intake boats in the casing, so that the high-load intake boats close later than the light-load intake boats 1 to 1 as the rotor rotates. In addition, when both ports 1~ are installed, the high-load intake ball 1~ is equipped with an opening/closing valve 16 and a diaphragm-type opening/closing valve that listens to this opening/closing valve during high loads. Then, the pressure flow (4
In a rotary piston engine where a throttle part is installed in the introduction passage, a correction means for correcting the delay in the operation of the computer according to the operating condition is installed in the rotary piston engine. An intake system for a rotary piston engine characterized by:
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP58202304A JPS6093124A (en) | 1983-10-27 | 1983-10-27 | Intake device of rotary piston engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP58202304A JPS6093124A (en) | 1983-10-27 | 1983-10-27 | Intake device of rotary piston engine |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS6093124A true JPS6093124A (en) | 1985-05-24 |
Family
ID=16455322
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP58202304A Pending JPS6093124A (en) | 1983-10-27 | 1983-10-27 | Intake device of rotary piston engine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6093124A (en) |
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---|---|---|---|---|
US9828906B2 (en) | 2011-07-28 | 2017-11-28 | Pratt & Whitney Canada Corp. | Rotary internal combustion engine with variable volumetric compression ratio |
US9926842B2 (en) | 2011-07-28 | 2018-03-27 | Pratt & Whitney Canada Corp. | Rotary internal combustion engine with exhaust purge |
US10006358B2 (en) | 2011-07-28 | 2018-06-26 | Pratt & Whitney Canada Corp. | Rotary internal combustion engine with pilot subchamber |
US10041402B2 (en) | 2016-05-12 | 2018-08-07 | Pratt & Whitney Canada Corp. | Internal combustion engine with split pilot injection |
US10125676B2 (en) | 2011-07-28 | 2018-11-13 | Pratt & Whitney Canada Corp. | Rotary internal combustion engine with pilot subchamber |
US10145291B1 (en) | 2017-10-10 | 2018-12-04 | Pratt & Whitney Canada Corp. | Rotary engine and method of combusting fuel |
US10544732B2 (en) | 2011-07-28 | 2020-01-28 | Pratt & Whitney Canada Corp. | Rotary internal combustion engine with removable subchamber insert |
US10557407B2 (en) | 2011-07-28 | 2020-02-11 | Pratt & Whitney Canada Corp. | Rotary internal combustion engine with pilot subchamber |
US10801394B2 (en) | 2017-11-29 | 2020-10-13 | Pratt & Whitney Canada Corp. | Rotary engine with pilot subchambers |
-
1983
- 1983-10-27 JP JP58202304A patent/JPS6093124A/en active Pending
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9828906B2 (en) | 2011-07-28 | 2017-11-28 | Pratt & Whitney Canada Corp. | Rotary internal combustion engine with variable volumetric compression ratio |
US9926842B2 (en) | 2011-07-28 | 2018-03-27 | Pratt & Whitney Canada Corp. | Rotary internal combustion engine with exhaust purge |
US10006358B2 (en) | 2011-07-28 | 2018-06-26 | Pratt & Whitney Canada Corp. | Rotary internal combustion engine with pilot subchamber |
US10125676B2 (en) | 2011-07-28 | 2018-11-13 | Pratt & Whitney Canada Corp. | Rotary internal combustion engine with pilot subchamber |
US10138804B2 (en) | 2011-07-28 | 2018-11-27 | Pratt & Whitney Canada Corp. | Rotary internal combustion engine |
US10544732B2 (en) | 2011-07-28 | 2020-01-28 | Pratt & Whitney Canada Corp. | Rotary internal combustion engine with removable subchamber insert |
US10557407B2 (en) | 2011-07-28 | 2020-02-11 | Pratt & Whitney Canada Corp. | Rotary internal combustion engine with pilot subchamber |
US10578012B2 (en) | 2011-07-28 | 2020-03-03 | Pratt & Whitney Canada Corp. | Rotary internal combustion engine with pilot subchamber |
US10697365B2 (en) | 2011-07-28 | 2020-06-30 | Pratt & Whitney Canada Corp. | Rotary internal combustion engine with pilot subchamber |
US10041402B2 (en) | 2016-05-12 | 2018-08-07 | Pratt & Whitney Canada Corp. | Internal combustion engine with split pilot injection |
US10145291B1 (en) | 2017-10-10 | 2018-12-04 | Pratt & Whitney Canada Corp. | Rotary engine and method of combusting fuel |
US10801394B2 (en) | 2017-11-29 | 2020-10-13 | Pratt & Whitney Canada Corp. | Rotary engine with pilot subchambers |
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