JP2000064850A - Eccentric circular rotary diesel engine - Google Patents
Eccentric circular rotary diesel engineInfo
- Publication number
- JP2000064850A JP2000064850A JP10274201A JP27420198A JP2000064850A JP 2000064850 A JP2000064850 A JP 2000064850A JP 10274201 A JP10274201 A JP 10274201A JP 27420198 A JP27420198 A JP 27420198A JP 2000064850 A JP2000064850 A JP 2000064850A
- Authority
- JP
- Japan
- Prior art keywords
- chamber
- inner cylinder
- compressed air
- intake
- outer 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.)
- Pending
Links
Classifications
-
- 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
Abstract
Description
【0001】本発明は、前回の「特許願第110025
号」の、真円ロータリーエンジンの効率等の改善を目的
として考案したものです。The present invention is based on the previous "Patent Application No. 110025".
No. ”was designed for the purpose of improving the efficiency of a true circle rotary engine.
【0002】真円ロータリーエンジンの欠点の一つに、
可動回転翼の折れやすさがある。エンジンの外円筒と内
円筒が同軸にあるとき、可動回転翼の受ける折れ曲げの
力(回転方向への爆発圧とその逆向きの圧縮圧)は可動
回転翼の一点にかかるため、その部分で折れる可能性が
大きい。そこで、外円筒と内円筒の円の中心をOne of the drawbacks of a perfect circle rotary engine is
The movable rotor blade is easily broken. When the outer cylinder and the inner cylinder of the engine are coaxial, the bending force (explosive pressure in the rotation direction and compression pressure in the opposite direction) that the movable rotor receives is applied to one point of the movable rotor. It is likely to break. Therefore, the center of the circle of the outer cylinder and the inner cylinder
【図1】のようにずらす(偏心させる)ことで、可動回
転翼にかかる折れ曲げの力を分散させることが出来、可
動回転翼が折れにくくなる。また、こうすることで可動
回転翼の受ける爆発圧は、圧力の強いとき可動回転翼の
小さい面積で受け、爆発圧が小さくなるに従って大きい
面積で受けることとなり、折れ曲げの力も減少し、トル
ク変動も小さくなるという効果も出てくる。このよう
に、外円中心と内円中心をずらした真円ロータリーエン
ジンを偏心ロータリーエンジンと名付けました。By shifting (eccentricity) as shown in FIG. 1, the bending force applied to the movable rotor can be dispersed, and the movable rotor is less likely to break. Also, by doing so, the explosive pressure received by the movable rotor will be received by a small area of the movable rotor when the pressure is strong, and by a large area as the explosion pressure becomes smaller, the bending force will also decrease and the torque fluctuation There is also the effect of becoming smaller. In this way, the true circular rotary engine with the center of the outer circle and the center of the inner circle shifted is named the eccentric rotary engine.
【図1】[Figure 1]
【図2】[Fig. 2]
【図3】のエンジンともに偏心ロータリーエンジンの仲
間です。[Fig. 3] is a member of the eccentric rotary engine.
【0003】[0003]
【図1】[Figure 1]
【図2】[Fig. 2]
【図3】のエンジンともに、固定隔壁βを固定隔壁αの
対称位置から20度ほど吸気・圧縮室の方へずらしてい
ます。この結果、吸気・圧縮行程は短く、爆発・排気行
程は長くなり燃焼効率が向上するものと考えます。ただ
し、In both engines of [Fig. 3], the fixed partition β is shifted about 20 degrees from the symmetrical position of the fixed partition α toward the intake / compression chamber. As a result, the intake and compression strokes will be short, and the explosion and exhaust strokes will be long, improving combustion efficiency. However,
【図1】のエンジンでは吸気量が少なくなるので、リシ
ョルムコンプレッサー等の過給器の使用が望ましいと思
います。The engine of [Fig.1] has a small intake air volume, so I think it is desirable to use a turbocharger such as a Lisholm compressor.
【0004】[0004]
【図2】のエンジンは、過給器を使用しないで吸気量を
確保しようとしたものです。吸気・圧縮室の外筒を広げ
て偏円とします。過給器を使用するより、摩擦の上で有
利と考えます。このエンジンを偏円ロータリーエンジン
と呼ぶことにしました。The engine in [Fig. 2] is designed to secure intake air without using a supercharger. Expand the outer cylinder of the intake / compression chamber to form an eccentric circle. I think it is more advantageous in terms of friction than using a supercharger. I decided to call this engine a circular rotary engine.
【0005】[0005]
【図3】のエンジンは、圧縮空気副室を爆発室の副室と
して使用するものです。可動隔壁が爆発排気行程・吸気
圧縮行程の3/4ほど進んだとき(点線で記入)燃焼ガ
スを残したまま11の圧縮空気副室の押出弁を閉じ、1
0の圧縮空気副室の吸入弁を開き、副室に圧縮空気を押
し込みます。可動隔壁が10の弁にかかるとき10の弁
を閉じ、可動隔壁が11の弁を過ぎたとき、副室に燃料
を噴射して燃焼を起こすと同時に11の弁を開きます。
副室に燃料を噴射すると、副室に残っていた燃焼ガス残
気の熱と断熱圧縮による圧縮空気の温度で自然発火しま
す。燃料は軽油を想定していますが、自然発火可能なら
メタノールでもLPG等でもかまわないわけです。The engine shown in Fig. 3 uses the compressed air sub chamber as the sub chamber of the explosion chamber. When the movable bulkhead advances about 3/4 of the explosive exhaust stroke / intake compression stroke (marked with a dotted line), the extruding valve of the compressed air subchamber 11 is closed while leaving the combustion gas, 1
Open the suction valve of the compressed air subchamber 0 and push the compressed air into the subchamber. When the movable bulkhead touches the 10th valve, the 10th valve is closed, and when the movable bulkhead passes the 11th valve, fuel is injected into the sub chamber to cause combustion and simultaneously the 11th valve is opened.
When fuel is injected into the sub-chamber, the heat of the combustion gas residual air remaining in the sub-chamber and the temperature of the compressed air due to adiabatic compression cause spontaneous ignition. The fuel is assumed to be light oil, but methanol or LPG may be used as long as it can be spontaneously ignited.
【図3】のエンジンを偏円ロータリーディーゼルエンジ
ンと呼びます。The engine of [Fig.3] is called an eccentric rotary diesel engine.
【0006】偏円ロータリーディーゼルエンジンの動作
は、「回転翼で空気を圧縮し、圧縮された空気に燃料を
噴射し、燃焼ガスで回転翼を回します」。ところで、こ
の説明文はガスタービンエンジンの説明と全く同じもの
です。真円ロータリーエンジン群の欠点・実現の困難さ
は、シールの困難さにあります。最初からの発想は、熱
膨張のごく少ない材質で、隙間のあまりない構造で想定
していました。隙間があるものとし、シールするなら1
4カ所のシールが必要です。工夫しても10カ所。とに
かくシールがなかなか難しいのですが、このエンジンが
小型・低速回転型のガスタービンエンジンであると考え
れば、ほんの小さな隙間があっても効率のよいエンジン
になるのではないかとも思うのです。The operation of an eccentric rotary diesel engine is that "air is compressed by a rotor, fuel is injected into the compressed air, and the rotor is rotated by combustion gas." By the way, this description is exactly the same as the description of the gas turbine engine. The drawback of the perfect circle rotary engine group and the difficulty of realizing it are the difficulty of sealing. The idea from the beginning was to use a material with very little thermal expansion and a structure with no gaps. There is a gap, and 1 if you seal
Four seals are required. 10 places even if devised. Sealing is difficult anyway, but if you think that this engine is a small, low-speed rotation type gas turbine engine, I think that it will be an efficient engine even if there is a small gap.
【0007】ハイブリッド型エンジンや電気自動車・燃
料電池などが現実化している現在、内燃機関の効率向上
等は問題にならないように考えられがちだが、そうでは
ないと考えています。効率のよい発電器用のエンジン・
小型中型船舶用エンジン等、小型・高効率のエンジンの
必要性は今後も高いと考えています。特に中型船舶エン
ジンを発明のエンジンに使用できれば、振動のごく少な
い船が出来ます。Now that hybrid engines, electric vehicles, fuel cells, etc. are becoming a reality, it is often thought that improving the efficiency of internal combustion engines is not a problem, but I think that is not the case. Efficient generator engine
We believe that the need for small, highly efficient engines, such as small and medium-sized marine engines, will continue to grow. In particular, if a medium-sized ship engine can be used as the engine of the invention, a ship with minimal vibration can be created.
【図1】偏心ロータリーエンジンの構造Figure 1: Structure of eccentric rotary engine
【図2】偏円ロータリーエンジンの構造[Fig. 2] Structure of an elliptic rotary engine
【図3】偏円ロータリーディーゼルエンジンの構造[Fig. 3] Structure of an eccentric rotary diesel engine
「1 固定隔壁α」 「2 固定隔壁β」
「3 可動回転翼A」
「4 可動回転翼B」 「5 圧縮空気副室」
「6 吸気室」
「7 圧縮室」 「8 爆発膨張室」 「9
排気室」
「10 圧縮空気副室の吸入弁」 「11 圧縮
空気副室の押出弁」
「12 吸気管」 「13 吸気室開口部」
「14 排気室開口部」
「15 排気管」 「16 燃料噴射ポンプ」
「17 点火プラグ」
「O内 内円筒中心」 「O外 外円筒中心」"1 fixed bulkhead α""2 fixed bulkhead β"
"3 movable rotor A""4 movable rotor B""5 compressed air sub-chamber"
"6 Air intake chamber""7 Compression chamber""8 Explosion expansion chamber""9
Exhaust chamber "10 Suction valve for compressed air subchamber""11 Extrusion valve for compressed air subchamber""12 Intake pipe""13 Intake chamber opening"
"14 exhaust chamber opening""15 exhaust pipe""16 fuel injection pump"
"17 spark plug,""O within the cylindrical center""O outside the outside cylindrical center"
Claims (2)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP10274201A JP2000064850A (en) | 1998-08-20 | 1998-08-20 | Eccentric circular rotary diesel engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP10274201A JP2000064850A (en) | 1998-08-20 | 1998-08-20 | Eccentric circular rotary diesel engine |
Publications (1)
Publication Number | Publication Date |
---|---|
JP2000064850A true JP2000064850A (en) | 2000-02-29 |
Family
ID=17538452
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP10274201A Pending JP2000064850A (en) | 1998-08-20 | 1998-08-20 | Eccentric circular rotary diesel engine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2000064850A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20010079384A (en) * | 2001-07-10 | 2001-08-22 | 신철호 | Rotary engine with folded wings |
-
1998
- 1998-08-20 JP JP10274201A patent/JP2000064850A/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20010079384A (en) * | 2001-07-10 | 2001-08-22 | 신철호 | Rotary engine with folded wings |
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