JPS6258020A - Circular rotary piston motion type prime mover - Google Patents

Circular rotary piston motion type prime mover

Info

Publication number
JPS6258020A
JPS6258020A JP19828385A JP19828385A JPS6258020A JP S6258020 A JPS6258020 A JP S6258020A JP 19828385 A JP19828385 A JP 19828385A JP 19828385 A JP19828385 A JP 19828385A JP S6258020 A JPS6258020 A JP S6258020A
Authority
JP
Japan
Prior art keywords
turbine
casing
intake
annular cylinder
exhaust
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
JP19828385A
Other languages
Japanese (ja)
Inventor
Takeshi Umemoto
武 梅本
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 JP19828385A priority Critical patent/JPS6258020A/en
Publication of JPS6258020A publication Critical patent/JPS6258020A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To manufacture a prime mover excellent in efficiency in a simple manner, by installing an outputting center shaft in the center of a casing, while installing an annular cylinder along an outer circumference of the casing, and also installing two pistons slidably between these elements. CONSTITUTION:An outputting center shaft 4 is supported on the center of a slit type casing 2 via a bearing 3, and a sectional rectangular, annual cylinder 5 is installed along an outer circumference of the casing 2. And, a base end is pivotally supported on the center shaft 4 via one-way clutches 8 and 9, and the tip end is slidably fitted in the annular cylinder 5 via an airtight member 10, installing each of first and second pistons 6 and 7. In addition, a suction port 14, an exhaust port 15 and a fuel injection port 21 are all installed on the outer circumference of the annular cylinder 5, while there are provided with a rocking type stopper 23, a spark plug 24 and a radial stopper 25. Also there are provided with a suction turbine 11, an exhaust turbine 17 and an injection turbine 18, while a pulley type power transmission mechanism is installed among these turbines.

Description

【発明の詳細な説明】 [産業上の利用分野] この発明は、石油燃料を利用した原動機の分野に関する
ものである。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to the field of prime movers that utilize petroleum fuel.

[従来の技術1 石油燃料を利用した原動機としては、ロータリーピスト
ンエンジンがあるが、加工に超高度の技術を要する欠点
があった。
[Prior art 1] A rotary piston engine is a prime mover that uses petroleum fuel, but it has the drawback of requiring extremely advanced technology for processing.

1発明が解決しようとする問題点1 この発明は超高度の製作技術を要することなく、効率の
よい原動機を提供しようとするものである。
1 Problems to be Solved by the Invention 1 This invention aims to provide an efficient prime mover without requiring ultra-sophisticated manufacturing technology.

1問題点を解決するための手段] 図面に基いて説明する。1. Means to solve problem] The explanation will be based on the drawings.

この発明に係る内回転ピストン運動型原動機は、ボルト
ナラ1−1a、lbによって締付は可能な2つ割型ケー
シング2、ケーシング2の中心に軸受3.3を介して支
承された出力用中心軸4、ケーシング2の外周に沿って
設けた断面長方形の環状シリンダー5、 全体としてはスコップ状の形状をしており、握部に当る
基端を一方向クラッチ8.9を介して中心軸4に軸支し
且つ掬部に当る先端を環状シリンダー5に各種気密材1
0を介して滑動可能に嵌合した第1及び第2ピストン6
.7、 環状シリンダー5の外周上に略120度の範囲に亙って
順次配置した吸気弁13付き吸気口14、排気弁16付
き排気口15、燃料注入弁20付き燃料注入口21、ス
プリング22付き揺動型ストッパー23、点火プラグ2
4、ポール26とばね27と調整ポルト28からなる半
径方向ストッパー25、 吸気弁13の通路の前方に続けて順次配置した空気圧力
タンク12及び吸気タービン11、排気弁16の通路の
後方に配置した排気タービン17、 燃料注入弁20の通路の前方に続けて順次配置した燃料
圧力タンク19及び注入タービン18、中心軸4と吸気
タービン11.排気タービン17、注入タービン18と
の間には巻掛式動力伝達機構29,30.31が配置さ
れている。
The internally rotating piston motion type prime mover according to the present invention includes a two-split casing 2 that can be tightened with bolt nuts 1-1a and lb, and an output central shaft supported at the center of the casing 2 via a bearing 3.3. 4. An annular cylinder 5 with a rectangular cross section provided along the outer periphery of the casing 2, has a scoop-like shape as a whole, and its base end, which corresponds to the grip, is connected to the central shaft 4 via a one-way clutch 8.9. Various airtight materials 1 are attached to the annular cylinder 5 at the tip which is pivoted and corresponds to the scooping part.
The first and second pistons 6 are slidably fitted together via the
.. 7. An intake port 14 with an intake valve 13, an exhaust port 15 with an exhaust valve 16, a fuel injection port 21 with a fuel injection valve 20, and a spring 22, which are arranged in sequence over a range of approximately 120 degrees on the outer circumference of the annular cylinder 5. Swing type stopper 23, spark plug 2
4. A radial stopper 25 consisting of a pawl 26, a spring 27, and an adjustment port 28, an air pressure tank 12 successively placed in front of the passage of the intake valve 13, an intake turbine 11, and a radial stopper 25 placed behind the passage of the exhaust valve 16. Exhaust turbine 17, fuel pressure tank 19 and injection turbine 18, which are arranged successively in front of the passage of fuel injection valve 20, central shaft 4 and intake turbine 11. Wrap-type power transmission mechanisms 29, 30, and 31 are arranged between the exhaust turbine 17 and the injection turbine 18.

[作用] 第6図の状態において、室Aに臨む点火プラグ24が着
火すると、排気弁16は開き、第1ビス1〜ン6が半径
方向ストッパー25のばね27に抗して反時計方向に回
転し第7図の状態になり、室13の燃焼済ガスは排出さ
れる。
[Operation] In the state shown in FIG. 6, when the spark plug 24 facing the chamber A ignites, the exhaust valve 16 opens and the first screws 1 to 6 move counterclockwise against the spring 27 of the radial stopper 25. It rotates to the state shown in FIG. 7, and the burned gas in the chamber 13 is discharged.

第7図の状態になると、吸気弁13が開き、室13内は
新空気で充たされ第8図の状態になる。
When the state shown in FIG. 7 is reached, the intake valve 13 is opened and the interior of the chamber 13 is filled with fresh air, resulting in the state shown in FIG. 8.

第8図の状態になると、吸気弁13及び排気弁16が閉
しると共に、燃焼注入弁20が開き、第2ピストン7が
回転を初め第9図の状態を経て第10図の状態になる。
When the state shown in FIG. 8 is reached, the intake valve 13 and the exhaust valve 16 are closed, the combustion injection valve 20 is opened, and the second piston 7 begins to rotate, passing through the state shown in FIG. 9 and reaching the state shown in FIG. 10. .

第10図の状態になると、第2ピストン7が半径方向ス
トッパー25により停止される。
When the state shown in FIG. 10 is reached, the second piston 7 is stopped by the radial stopper 25.

第10図の状態になると第1ピストン6が更に回転し、
揺動型ストッパー23を通過し、第6図の最初の状態に
戻る。
When the state shown in FIG. 10 is reached, the first piston 6 rotates further,
It passes through the swing type stopper 23 and returns to the initial state shown in FIG.

[実施例] 図面を参考にして説明する。[Example] This will be explained with reference to the drawings.

ボルトナラ)1a、1bによって締付は可能な2つ割型
ケーシング2、 ケーシング2の中心に軸受3,3を介して支承された出
力用中心軸4、 う−一シング2の外周に沿って設けた断面長方形の環状
シリンダー5、 全体としてはスコップ状の形状をしており、握部に当る
基端を一方向クラッチ8,9を介して中心軸4に軸支し
且つ掬邪に当る先端を環状シリンダー5に各種気密材I
Oを介して滑動可能に嵌合した第1及び第2ピストン6
.7、 環状シリンダー5の外周上に略120度の範囲に亙って
順次配置した吸気弁13付き吸気口14、排気弁16付
き排気口15、燃焼注入弁20付き燃焼注入口21、ス
プリング22付き揺動型ストッパー23、点火プラグ2
4、ボール26とばね27と調整ボルト28からなる半
径方向ストッパー25、 吸気弁13の通路の前方、続けて順次配置した空気圧力
クンク12及び吸気タービン11、排気弁16の通路の
後方に配置した排気タービン17、燃料注入弁20の通
路の前方に続けて順次配置した燃料圧力タンク19及び
注入タービン18、 中心軸4と吸気タービン11.排気タービン17.注入
タービン18との間には巻掛式動力伝達機構29,30
.31が配置されている。32゜33はピストン6.7
のアームである。
A two-piece casing 2 that can be tightened with bolts 1a and 1b, a central output shaft 4 supported at the center of the casing 2 via bearings 3, and a central output shaft 4 provided along the outer periphery of the housing 2. An annular cylinder 5 with a rectangular cross section has a scoop-like shape as a whole, and the base end that is the grip part is pivotally supported on the central shaft 4 via one-way clutches 8 and 9, and the tip that is the scooper is supported on the central shaft 4 via one-way clutches 8 and 9. Various airtight materials I in the annular cylinder 5
The first and second pistons 6 are slidably fitted together via O.
.. 7. An intake port 14 with an intake valve 13, an exhaust port 15 with an exhaust valve 16, a combustion injection port 21 with a combustion injection valve 20, and a spring 22, which are arranged in sequence over a range of approximately 120 degrees on the outer circumference of the annular cylinder 5. Swing type stopper 23, spark plug 2
4. A radial stopper 25 consisting of a ball 26, a spring 27, and an adjustment bolt 28, arranged in front of the passage of the intake valve 13, successively arranged in sequence with the air pressure sensor 12, the intake turbine 11, and the rear of the passage of the exhaust valve 16. Exhaust turbine 17, fuel pressure tank 19 and injection turbine 18, which are sequentially arranged in front of the passage of fuel injection valve 20, central shaft 4 and intake turbine 11. Exhaust turbine 17. Wrap-type power transmission mechanisms 29 and 30 are provided between the injection turbine 18 and the injection turbine 18.
.. 31 are arranged. 32°33 is piston 6.7
It is the arm of

[発明の効果1 本発IJJ によれば、製作容易にして、効率のよい原
動機を得ることが出来る。
[Effect of the Invention 1] According to the IJJ of the present invention, it is possible to obtain an efficient prime mover that is easy to manufacture.

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

図面はごの発明の一例を示すもので、第1図は全体の垂
直切断正面図、第2図は全体の垂直切断側面図、第3図
は全体の正面図、第4図は全体の側面図、第5図は分解
した状態における正面図、第6図乃至第10図は作動説
明用正面図である。 1a    ポルト 1b     ナツト 2     ケーシング 3     軸受 4     中心軸 5     環状シリンダー 6     第1ピストン 7     第2ピストン 8    一方向クラッチ 9    一方向クラフチ 10    気密材 11     吸気タービン 12    空気圧力タンク 13    吸気弁 14    吸気口 15    排気口 16    排気弁 17    排気タービン 18    注入タービン 19    燃料圧力タンク 20    燃料注入弁 21    燃料注入口 22    スプリング 23    揺動型ストッパー 24    点火プラグ 25    半径方向ストッパー 26    ボール 27    ばね 28    調整ボルト 29    吸気タービンの巻掛式動力伝達機構30 
   排気タービンの巻掛式動力伝達機構31    
注入タービンの巻掛式動力伝達機構32    アーム 33    アーム
The drawings show an example of the invention, in which Fig. 1 is a vertically cut front view of the whole, Fig. 2 is a vertically cut side view of the whole, Fig. 3 is a front view of the whole, and Fig. 4 is a side view of the whole. , FIG. 5 is a front view in an exploded state, and FIGS. 6 to 10 are front views for explaining the operation. 1a Port 1b Nut 2 Casing 3 Bearing 4 Central shaft 5 Annular cylinder 6 First piston 7 Second piston 8 One-way clutch 9 One-way clutch 10 Airtight material 11 Intake turbine 12 Air pressure tank 13 Intake valve 14 Intake port 15 Exhaust port 16 Exhaust valve 17 Exhaust turbine 18 Injection turbine 19 Fuel pressure tank 20 Fuel injection valve 21 Fuel injection port 22 Spring 23 Swing type stopper 24 Spark plug 25 Radial stopper 26 Ball 27 Spring 28 Adjustment bolt 29 Wrap-type power transmission of intake turbine Mechanism 30
Wrap type power transmission mechanism 31 for exhaust turbine
Injection turbine wrap-type power transmission mechanism 32 Arm 33 Arm

Claims (1)

【特許請求の範囲】 ボルトナット(1a、1b)によつて締付け可能な2つ
割型ケーシング(2)、ケーシング(2)の中心に軸受
(3、3)を介して支承された出力用中心軸(4)、ケ
ーシング(2)の外周に沿つて設けた断面長方形の環状
シリンダー(5)、全体としてはスコップ状の形状をし
ており、握部に当る基端を一方向クラッチ(8、9)を
介して中心軸(4)に軸支し且つ掬部に当る先端を環状
シリンダー(5)に各種気密材(10)を介して滑動可
能に嵌合した第1及び第2ピストン(6、7)、 環状シリンダー(5)の外周上に略120度の範囲に亙
つて順次配置した吸気弁(13)付き吸気口(14)、
排気弁(16)付き排気口(15)、燃料注入弁(20
)付き燃料注入口(21)、スプリング(22)付き揺
動型ストッパー(23)、点火プラグ(24)、ボール
(26)とばね(27)と調整ボルト(28)からなる
半径方向ストッパー(25)、 吸気弁(13)の通路の前方に続けて順次配置した空気
圧力タンク(12)及び吸気タービン(11)、 排気弁(16)の通路の後方に配置した排気タービン(
17)、 燃料注入弁(20)の通路の前方に続けて順次配置した
燃料圧力タンク(19)及び注入タービン(18)、 中心軸(4)と吸気タービン(11)、排気タービン(
17)、注入タービン(18)との間に配置した巻掛式
動力伝達機構(29、30、31)とからなることを特
徴とする円回転ピストン運動型原動機。
[Claims] A two-part casing (2) that can be tightened with bolts and nuts (1a, 1b), an output center supported at the center of the casing (2) via bearings (3, 3). The annular cylinder (5) with a rectangular cross section is provided along the outer circumference of the shaft (4) and the casing (2), and the overall shape is scoop-like. First and second pistons (6) are pivotally supported on the central shaft (4) via a piston (9), and the tips corresponding to the scooping portion are slidably fitted into the annular cylinder (5) via various airtight materials (10). , 7), intake ports (14) with intake valves (13) arranged sequentially over a range of approximately 120 degrees on the outer periphery of the annular cylinder (5);
Exhaust port (15) with exhaust valve (16), fuel injection valve (20)
) with a fuel inlet (21), an oscillating stopper (23) with a spring (22), a radial stopper (25) consisting of a spark plug (24), a ball (26), a spring (27) and an adjusting bolt (28). ), an air pressure tank (12) and an intake turbine (11) successively arranged in front of the passage of the intake valve (13), and an exhaust turbine (
17), a fuel pressure tank (19) and an injection turbine (18) sequentially arranged in front of the passage of the fuel injection valve (20), a central shaft (4), an intake turbine (11), an exhaust turbine (
17) A circularly rotating piston motion type prime mover comprising a wrap-type power transmission mechanism (29, 30, 31) disposed between the injection turbine (18) and the injection turbine (18).
JP19828385A 1985-09-06 1985-09-06 Circular rotary piston motion type prime mover Pending JPS6258020A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP19828385A JPS6258020A (en) 1985-09-06 1985-09-06 Circular rotary piston motion type prime mover

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP19828385A JPS6258020A (en) 1985-09-06 1985-09-06 Circular rotary piston motion type prime mover

Publications (1)

Publication Number Publication Date
JPS6258020A true JPS6258020A (en) 1987-03-13

Family

ID=16388548

Family Applications (1)

Application Number Title Priority Date Filing Date
JP19828385A Pending JPS6258020A (en) 1985-09-06 1985-09-06 Circular rotary piston motion type prime mover

Country Status (1)

Country Link
JP (1) JPS6258020A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7441534B2 (en) * 2003-06-09 2008-10-28 Douglas Bastian Rotary engine system
JP2013137010A (en) * 2011-12-27 2013-07-11 Takeshi Hatanaka Rotary fluid machinery
KR101285096B1 (en) * 2012-07-05 2013-07-17 송정순 Rotary engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7441534B2 (en) * 2003-06-09 2008-10-28 Douglas Bastian Rotary engine system
JP2013137010A (en) * 2011-12-27 2013-07-11 Takeshi Hatanaka Rotary fluid machinery
KR101285096B1 (en) * 2012-07-05 2013-07-17 송정순 Rotary engine

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