JPH01216029A - Engine - Google Patents

Engine

Info

Publication number
JPH01216029A
JPH01216029A JP63042680A JP4268088A JPH01216029A JP H01216029 A JPH01216029 A JP H01216029A JP 63042680 A JP63042680 A JP 63042680A JP 4268088 A JP4268088 A JP 4268088A JP H01216029 A JPH01216029 A JP H01216029A
Authority
JP
Japan
Prior art keywords
hole
piston
bearing
crank shaft
connecting rod
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
JP63042680A
Other languages
Japanese (ja)
Inventor
Saburo Shirayanagi
白柳 三郎
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to JP63042680A priority Critical patent/JPH01216029A/en
Publication of JPH01216029A publication Critical patent/JPH01216029A/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
    • F02B75/00Other engines
    • F02B75/32Engines characterised by connections between pistons and main shafts and not specific to preceding main groups
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B41/00Engines characterised by special means for improving conversion of heat or pressure energy into mechanical power
    • F02B41/02Engines with prolonged expansion
    • F02B41/04Engines with prolonged expansion in main cylinders
    • 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

Abstract

PURPOSE:To enable fetching of a power, generated by an engine, with high efficiency, by a method wherein a horizontal and arcuate hole is formed in the end part on the crankshaft side of a connecting rod through which a piston and a crank shaft are intercoupled, and a crank pin is inserted in and supported to the hole. CONSTITUTION:In a connecting rod 2 through which a piston 3 reciprocatively engagedly inserted in a cylinder 1 and a crank shaft 4 are intercoupled, an end part on the crank shaft 4 side forms a large part, and a hole 7 is formed therein. The hole 7 is formed with a left part containing a hole part in the same arc of a circle as that drawn by a bearing 5 engaged with a crank pin 6 through rotation of the crank shaft 4 and a right horizontal part connected to the left hole part, and a bearing 5 is slidably engaged with the hole 7. This constitution improves energy efficiency in a way that the crank shaft 4 is rotated in a state in which the piston 3 is located in a highmost position (during completion of a compression stroke) and thereafter an expansion stroke is started.

Description

【発明の詳細な説明】 従来のエンジンは、上死点では、クランクシャフトを回
転させる為の、エネルギー効率はゼロであり、上死点か
らクランクシャフトが回転して行くと、クランクシャフ
トを回転させる為の、エネルギー効率が次第に良くなっ
て!?き、上死点と下死点の中間が、クランクシャフト
を回転させる為のエネルギー効率が最も良い、一方、爆
発圧が最も強い爆発行程開始が上死点で、爆発行程でピ
ストンが下行して行(と、爆発圧は次第に弱くなって行
く。
[Detailed Description of the Invention] In a conventional engine, the energy efficiency for rotating the crankshaft at top dead center is zero, and as the crankshaft rotates from top dead center, the energy efficiency for rotating the crankshaft is zero. The energy efficiency is gradually improving! ? The energy efficiency for rotating the crankshaft is highest between top dead center and bottom dead center.On the other hand, top dead center is the start of the explosion stroke where the explosion pressure is strongest, and the piston moves downward during the explosion stroke. The explosion pressure gradually weakens.

従ってエネルギー効率が悪い。Therefore, energy efficiency is poor.

本発明は新形のコンロッドにより、ピストンが最も高い
位置(圧縮行程完了時)の状態で、クランクシャフトが
回転して行き、従来の上死点から離れた位置に未てから
、爆発行程を開始させて、エネルギー効率を良くさせた
ものである。
The present invention uses a new type of connecting rod to rotate the crankshaft while the piston is at its highest position (completion of the compression stroke), and starts the explosion stroke after reaching a position far from the conventional top dead center. This improves energy efficiency.

また、本発明では、排気時間がより長い為、より多くの
排気が小米、従ってより良い燃焼、より強い爆発力、よ
りきれいな排ガスとなる様にしである。
Also, in the present invention, since the evacuation time is longer, more exhaust gas is consumed, thus resulting in better combustion, stronger explosive power, and cleaner exhaust gas.

図について説明すると、1はシリンダー、2はピストン
3に固着した新形のコンロッド、4はクランクシャフト
、5はクランクピン6にはめ込んだベアリング、7はコ
ンロッド2を(9貫いで出きた孔で、孔7の幅は、ベア
リング5の直径より僅かに広い、また、孔7の左半分は
、クランクシャフト4の回転によって、ベアリング5が
描く円弧と同じ円弧の部分と、その左側の水平の部分か
ら成っており、一方、孔7の右半分は水平である。
To explain the figures, 1 is the cylinder, 2 is the new connecting rod fixed to the piston 3, 4 is the crankshaft, 5 is the bearing fitted into the crank pin 6, 7 is the hole made by piercing the connecting rod 2, The width of the hole 7 is slightly wider than the diameter of the bearing 5, and the left half of the hole 7 is separated by the rotation of the crankshaft 4 from the same arc drawn by the bearing 5 and the horizontal part on the left side. The right half of the hole 7, on the other hand, is horizontal.

なお、ベアリング5は孔7の中に入っている。Note that the bearing 5 is placed in the hole 7.

本発明は以上の様な構造から成り、第1図の状!!(従
来のエンジンの上死点の位置)からクランクシャフト4
が矢印の方向に約8分の1回転した所(第3図の状態)
で爆発行程が開始される。このI’ll(第1図の状態
から#43図の状態までの闇)は、ベアリング5が孔7
の円弧の部分の中を、矢印の回転方向に動いて行くが、
この場合は孔7の円弧と、ベアリング5の動きで描(円
弧が同じである為、コンロフト2とピストン3は下行し
ない。
The present invention consists of the structure as described above, and has the structure shown in Fig. 1! ! (from the top dead center position of a conventional engine) to the crankshaft 4
has rotated about one-eighth in the direction of the arrow (as shown in Figure 3)
The explosion process begins. In this I'll (darkness from the state in Figure 1 to the state in Figure #43), the bearing 5 is in hole 7.
It moves in the direction of rotation of the arrow inside the arc of
In this case, it is depicted by the arc of the hole 7 and the movement of the bearing 5 (since the arcs are the same, the conloft 2 and piston 3 do not move down.

その後、ベアリング5が孔7の左半分の水平の部分に入
ると、(第3図の状態になると)爆発圧でベアリング5
が、コンロッド2に押されて、クランクシャフト4と共
に矢印の方向に回転し、第4図の状!!(従来のエンジ
ンの下死点の位W!t)で爆発行程が完了する。この間
(#43図の状態がら第4図の状態までの間)、ベアリ
ング5は孔7の左半分の水平の部分の中を、右端から左
端に動き、そして左端から右端に動いた後、孔7の円弧
の部分を通って第4図の位置に米る。その後、クランク
シャフト4の、矢印方向への約8分の5回転で、コンロ
ッド2が、ベアリング5に押し上げられると、ピストン
3も同様に押し上げられ、そして第1図の状態を通過し
て、第3図の状態で排気行程を終了する。このl1l(
第4図の状態から第3図の状態までの間)、ベアリング
5は、孔7の右半分の中を左端から右端に!!+き、そ
して右端から左端に動いた後、孔7の円弧の部分を通る
。この円弧の部分をベアリング5が通過する間は、爆発
行程と同じ様にコンロッド2とピストン3は下行しない
、この後、爆発行程と同じ様に、クランクシャフト4と
ベアリング5が回転してコンロッド2がベアリング5に
押し下げられ、同時にピストン3も下行し、第4図の状
態で吸入行程を終了する。
After that, when the bearing 5 enters the horizontal part of the left half of the hole 7, the explosion pressure causes the bearing 5 to
is pushed by the connecting rod 2 and rotates together with the crankshaft 4 in the direction of the arrow, resulting in the state shown in Fig. 4! ! The explosion stroke is completed at W!t (about the bottom dead center of a conventional engine). During this period (from the state shown in Figure #43 to the state shown in Figure 4), the bearing 5 moves in the horizontal portion of the left half of the hole 7 from the right end to the left end, and then from the left end to the right end. Pass through the arc of 7 to the position shown in Figure 4. Thereafter, when the connecting rod 2 is pushed up by the bearing 5 by about 5/8 rotations of the crankshaft 4 in the direction of the arrow, the piston 3 is also pushed up in the same way, passing through the state shown in FIG. The exhaust stroke ends in the state shown in Figure 3. This l1l(
Between the state shown in Fig. 4 and the state shown in Fig. 3), the bearing 5 moves from the left end to the right end inside the right half of the hole 7! ! +, and after moving from the right end to the left end, it passes through the arc of hole 7. While the bearing 5 passes through this arc, the connecting rod 2 and the piston 3 do not descend, just like in the explosion stroke.After this, the crankshaft 4 and the bearing 5 rotate, and the connecting rod 2 is pushed down by the bearing 5, and at the same time the piston 3 also moves down, completing the suction stroke in the state shown in FIG.

この後、クランクシャフト4の矢印の方向への半回転で
、コンロッド2が、ベアリング5に押し上げられると、
ピストン3も同様に押し上げられ、第1図の状態で吸入
行程を終了する。この間(第4図の状態から第1図の状
態までの間)、ベアリング5は、孔7の右半分の中を左
端から右端に動き、そして右端に動く。
After this, when the connecting rod 2 is pushed up onto the bearing 5 by a half turn of the crankshaft 4 in the direction of the arrow,
The piston 3 is also pushed up in the same way, and the suction stroke ends in the state shown in FIG. During this period (from the state shown in FIG. 4 to the state shown in FIG. 1), the bearing 5 moves in the right half of the hole 7 from the left end to the right end, and then moves to the right end.

以上説明した様に本発明によれば、ピストン3最も高い
位II(圧縮行程完了時)の状態で、クランクシャフト
4が回転して、従来の上死点のから離れたクランクシャ
フトを回転させる為のエネルギー効率の良い位置に米で
から、最も爆発圧が強い爆発行程開始時となって、エネ
ルギー効率が良い。
As explained above, according to the present invention, the crankshaft 4 rotates when the piston 3 is at the highest position II (at the completion of the compression stroke), and rotates the crankshaft away from the conventional top dead center. Since the rice is placed in the most energy efficient position, the explosion pressure is strongest at the beginning of the explosion stroke, which is the most energy efficient position.

また、本発明では、排気時間がより長い為、より多くの
排気が小米、従ってより良い燃焼、より強い爆発力、よ
りきれいな排ガスとなる。
Also, in the present invention, since the evacuation time is longer, more exhaust gas is used, resulting in better combustion, stronger explosive power, and cleaner exhaust gas.

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

図面は本発明エンジンの一実施例で、第1図は一部を断
面とした圧縮行程完了時の状態を示す側面略図、第2図
は一部を断面としたwS1図の正面略図、第3図は一部
を断面とした爆発行程開始時または排気行程完了時、或
いは吸入行程開始時のそれぞれの状態を示す側面略図、
第4図は一部を断面とした爆発行程完了時または排気行
程開始時、或いは吸入行程完了時または圧縮行程開始時
のそれぞれの状態を示す側面略図である。
The drawings show one embodiment of the engine of the present invention, and FIG. 1 is a partially cross-sectional schematic side view showing the state at the completion of the compression stroke, FIG. 2 is a partially cross-sectional front schematic diagram of FIG. wS1, and FIG. The figure is a schematic side view showing the respective states at the start of the explosion stroke, the completion of the exhaust stroke, or the start of the suction stroke, with a part cut away;
FIG. 4 is a schematic side view, partially in cross section, showing the respective states at the completion of the explosion stroke or the start of the exhaust stroke, or at the completion of the suction stroke or the start of the compression stroke.

Claims (1)

【特許請求の範囲】[Claims] ピストンに固着したコンロッドに、水平方向、及び円弧
の形の孔をくり貫いた事を特徴とするエンジン。
An engine characterized by horizontal and arc-shaped holes cut into the connecting rod fixed to the piston.
JP63042680A 1988-02-24 1988-02-24 Engine Pending JPH01216029A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP63042680A JPH01216029A (en) 1988-02-24 1988-02-24 Engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP63042680A JPH01216029A (en) 1988-02-24 1988-02-24 Engine

Publications (1)

Publication Number Publication Date
JPH01216029A true JPH01216029A (en) 1989-08-30

Family

ID=12642746

Family Applications (1)

Application Number Title Priority Date Filing Date
JP63042680A Pending JPH01216029A (en) 1988-02-24 1988-02-24 Engine

Country Status (1)

Country Link
JP (1) JPH01216029A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130019835A1 (en) * 2010-04-07 2013-01-24 George Flenche Combustion engine
JP2014520988A (en) * 2011-06-30 2014-08-25 エクゾドゥス アール アンド ディー インターナショナル ピーティーイー. リミテッド Desmodronic shaft and yoke assembly for converting linear motion to rotational motion

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61241423A (en) * 1986-03-27 1986-10-27 Takeo Takagaki Crank rotational mechanism through aid of rocking bar

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61241423A (en) * 1986-03-27 1986-10-27 Takeo Takagaki Crank rotational mechanism through aid of rocking bar

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130019835A1 (en) * 2010-04-07 2013-01-24 George Flenche Combustion engine
CN102985638A (en) * 2010-04-07 2013-03-20 依达克斯研发国际私人有限公司 Improved combustion engine
JP2013524078A (en) * 2010-04-07 2013-06-17 エクゾドゥス アール アンド ディー インターナショナル ピーティーイー. リミテッド Improved internal combustion engine
US9188001B2 (en) 2010-04-07 2015-11-17 Exodus R&D International PTE, LTD. Combustion engine
JP2014520988A (en) * 2011-06-30 2014-08-25 エクゾドゥス アール アンド ディー インターナショナル ピーティーイー. リミテッド Desmodronic shaft and yoke assembly for converting linear motion to rotational motion

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