JPS58131320A - Disc engine - Google Patents
Disc engineInfo
- Publication number
- JPS58131320A JPS58131320A JP57014150A JP1415082A JPS58131320A JP S58131320 A JPS58131320 A JP S58131320A JP 57014150 A JP57014150 A JP 57014150A JP 1415082 A JP1415082 A JP 1415082A JP S58131320 A JPS58131320 A JP S58131320A
- Authority
- JP
- Japan
- Prior art keywords
- compression
- shaft
- combustion
- shutter
- pressure
- 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
-
- 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)
- Output Control And Ontrol Of Special Type Engine (AREA)
- Supercharger (AREA)
Abstract
Description
【発明の詳細な説明】
本発明のジスクエンジンは、シャノタージスク、及び、
出力、圧縮両口−ターをはじめ、その全運動系を総て、
二重反転の百円運動として、全運動系の慣性マスを完全
に相殺して、その運転を極めて静粛円滑なものとし、シ
ャッターゲートの開閉速度を単板ジスクの２倍にアップ
して、適切な圧縮比設定を容易にし、また、エンジンの
１回転中における、吸銀、圧縮、燃熔、排気の各作動角
を、それぞれ、３００°以１−１とじて吸排気効率をア
ップし、更に、燃焼圧を的接回転トルクに変換して、従
来の一般エンジンに比し、比容積出力を２倍以上にアッ
プし、かつ、比出力重量をイ以ｌ下に軽減する、ジスク
エンジンを得ることを目的とするものである。DETAILED DESCRIPTION OF THE INVENTION The disc engine of the present invention includes a shanotar disc, and
The entire motion system, including the output and compression both ends,
As a double-rotating 100-circle motion, the inertia mass of the entire motion system is completely canceled out, making the operation extremely quiet and smooth, and the opening and closing speed of the shutter gate is twice as fast as that of a single plate disc, making it suitable for use. In addition, the operating angles of silver absorption, compression, combustion, and exhaust during one rotation of the engine are set to 1-1 at 300° or more to improve intake and exhaust efficiency. To obtain a disc engine that converts combustion pressure into tangential rotational torque, increases the specific volume output by more than twice that of conventional general engines, and reduces the specific output weight to less than 1. The purpose is to
次に本実施例の構成を図面について説明すれば、第１図
に示すように、シャノターシスク軸４２を中心に、燃焼
室２８と圧縮室２９が放射状に配置され、燃焼室にはケ
ーシング側板によって、回転自在に支承された出力軸２
２が在り、該軸上に出力ローター３０が、軸方向のスラ
スト許容の状態にスプライン嵌合されている、圧縮室に
は側板によって支承された受動軸２３が在って、該軸上
に圧縮ローター３１がスプライン嵌合されている。Next, the configuration of this embodiment will be explained with reference to the drawings. As shown in FIG. 1, the combustion chamber 28 and the compression chamber 29 are arranged radially around the cylinder shaft 42, and the combustion chamber is surrounded by a casing side plate. Rotatably supported output shaft 2
2, on which the output rotor 30 is spline-fitted to allow thrust in the axial direction.In the compression chamber, there is a passive shaft 23 supported by a side plate, on which compression The rotor 31 is spline fitted.
第５図に示すように、出力ローター３０の周而（−に突
出して受圧板３８が設けられている、該受圧板基部の【
］−ター周而と、その−側面に油叡［１３２が開［１し
ている″、圧縮ローター３１の周面１−にも受圧板３９
が在って、該受圧根基部のローター周面と、その−側面
に３Ｍ気口３３が開ＩＸＩ ｌている。As shown in FIG. 5, a pressure receiving plate 38 is provided projecting around the output rotor 30.
The pressure receiving plate 39 is also located on the circumferential surface of the compression rotor 31.
There is a 3M air port 33 open on the rotor circumferential surface of the pressure receiving root base and the side surface thereof.
第２１図、２２図、２３図に示すように、通気［１３２
と３３とに重合ｆｆ１３ｆＥる部位の、ケーンング側板
に連通口３４が設けられている。As shown in FIGS. 21, 22, and 23, ventilation [132
A communication port 34 is provided in the caning side plate at a portion where ff13fE and ff13fE overlap.
第１図に示すように、出力軸２２の左端に受動軸反転用
の駆動ギヤー４５が一固定さ焦てぃて、受動軸２３の右
端に固定された受動キャー４６と、ケーンングによって
支持されたアイドルキャー４４を介して噛合している、
受動軸２３の１１丁端には、ツヤ、ターノスク駆動系の
駆動ピニオン２１が固定されている。As shown in FIG. 1, a driving gear 45 for reversing the passive shaft is fixed to the left end of the output shaft 22, and is supported by a passive carrier 46 fixed to the right end of the passive shaft 23 and a caning. are engaged via the idler carrier 44,
A drive pinion 21 of a gloss drive system is fixed to the 11th end of the driven shaft 23.
第２図に示すように、駆動ビニオン２１の右側に、ツヤ
、ターンスフ１騙Ｘ動用の受動ピニオ／１９が１１１１
・合され、該ピニオンは駆動スプロケｙ ｌ’ １７と
結合されている、また、駆動ピニオン２１の左側に、ノ
ヤノターンスク２駆動用の受動ピニオン２０が１ｌｉｌ
（合し、該ピニオンは駆動スプロケット１８と結合され
ている。As shown in Fig. 2, on the right side of the drive pinion 21, there is a passive pinio/19 1111 for gloss and turn 1 movement.
・The pinion is connected to the drive sprocket yl' 17. Also, on the left side of the drive pinion 21, there is a passive pinion 20 for driving the Noyano turn disk 2.
(The pinion is connected to the drive sprocket 18.)
第２図、３図に示すように、駆動スプロケット１７は、
チェーン２４を介して受動スプロケット１４を駆動し、
該スプロケットと一体の伝動スプロケット１２により、
チー−７２６’を介して、ノヤノタージスク軸スプロケ
ット６によって、シャノターシスク１が駆動される、ま
た、駆動スプロケット１８は、チェーン２５を介−−−
、！て受動スブロ’ｆ ｙ ｌ・１５を駆動し、該スプ
ロケットと一体の伝動スプロケット１３により、チ、−
ン２６を介して、シャノタージスク軸スプロケ、１・７
によって、シャ、ターソスク２を駆動する、シャノター
ジスク１と２は、シャノターシスク軸４２．４２’−Ｌ
に、それぞれ、軸方向ノスラスト許容の状態にスプライ
ン嵌合シテいる、シャノターソスク輔４２°は、シャ、
タージスク軸４２の左側將の外周ｌ−に在る。As shown in FIGS. 2 and 3, the drive sprocket 17 is
driving the passive sprocket 14 via the chain 24;
With the transmission sprocket 12 integrated with the sprocket,
The shaft sprocket 6 drives the shaft sprocket 1 through the chain 726', and the drive sprocket 18 is driven by the shaft sprocket 6 through the chain 25.
,! The transmission sprocket 13, which is integrated with the sprocket, drives the passive sprocket 'f y l.
Through the connection 26, the shaft sprocket, 1 and 7
Accordingly, the shafts 1 and 2 are driven by the shafts 42, 42'-L.
In each case, the spline fitting is in the axial no thrust permissible state.
It is located on the outer periphery l- of the left wing of the Tajsk axis 42.
第１図、３図に示すように、シャ、タージスク輔４２．
４２’は々−持アーム８の先端部によ−）て々゛持さね
、該支持端部の外周に、ガイドメタル１０が装着されて
いて、該メタルを介して々。As shown in Figures 1 and 3, Sha, Tajsk 42.
42' is held by the tip of the holding arm 8), and a guide metal 10 is attached to the outer periphery of the support end, and the guide metal 10 is held through the metal.
持端部は、ターノ／グのヴ持枠１１に嵌合サレ、軸は１
−ド方向のスラスト許容の状態に支持されている、支持
アームの軸支持端の一側に、発条２７が装着されていて
、ンヤ、タージスク１．２の外周面を、圧縮、出力１ｉ
１１１ ｏ−ターの周面（−に圧接させている、また、
支持アームの基部は、す／り９を介してター７７りに連
結されている。The holding end has a slit that fits into the holding frame 11 of the turn/g, and the shaft is 1
A spring 27 is attached to one side of the shaft support end of the support arm, which is supported in a state that allows thrust in the direction of
111 The circumferential surface of the o-tor (-, which is pressed against the
The base of the support arm is connected to the tar 77 via the support arm 9.
第１７図に示すように、燃焼室のツヤ、ターゲート４１
の右側に点火栓４０が装着されてふ・す、ケートの左側
には排気口３５が開口している、また、第２８図に示す
ように、圧縮室のソヤノターケ−１・４１の左側に、吸
気口３６が開１１シている。As shown in Figure 17, the gloss of the combustion chamber, the target 41
The spark plug 40 is installed on the right side of the housing, and the exhaust port 35 is opened on the left side of the housing.As shown in FIG. The intake port 36 is open.
次に本実施例の作動の状態を図面に従って詳述すれば、
第８図は、受圧板３８がシャノターケ−１・ｌ１ｉ１１
５°の位置で、受圧板排出側Ｖは排気を終ｒし、燃焼側
Ｅも燃・焼膨帳が終Ｊ’ している、同時に圧縮室は、
第７図の１うに受１Ｆ−板３９の進角により、その吸入
側（） Ｖｉ１１１６気［１３６から吸気作動中、圧縮
（ｌｌｌｌＣＶｉ前回叫人混合気の月：縮作動中である
、この位置で燃焼室のケートは、第６図のように、ツヤ
、ターシスク１と２の切欠き３と４の前縁Ａが、ゲート
の中間位置で一致してこれよりゲートが開き始める。Next, the operating state of this embodiment will be explained in detail according to the drawings.
In FIG. 8, the pressure receiving plate 38 is
At the 5° position, the pressure receiving plate discharge side V has finished exhausting, and the combustion side E has also finished its combustion expansion.At the same time, the compression chamber is
Due to the advance angle of the 1F plate 39 in Figure 7, the suction side () Vi1116 [from 136] during the intake operation, compression (llllCVi last time the air-fuel mixture is in the compression operation, at this position As shown in Fig. 6, the front edges A of the notches 3 and 4 of the combustion chamber gates 1 and 2 coincide at the middle position of the gate, and the gate begins to open from this point.
第１１図は、受圧板３８が、第８図の位１６から１５°
進角してケート直前に任って、ケートは第９図のように
、シャノタージスク１と２の切欠き３と４の前縁Ａが、
ターＩ・の両縁と一致してゲートを全開している、同時
に圧縮室は、第１０図のように、受圧板吸入側りは吸入
［１３６から吸気作動中、その圧縮側Ｃは、前同吸入混
合気の圧縮作動中である。FIG. 11 shows that the pressure receiving plate 38 is 15 degrees from the position 16 in FIG. 8.
Advance the angle and position the gate just before the gate, as shown in Figure 9, so that the front edges A of the notches 3 and 4 of the shafts 1 and 2 are
At the same time, as shown in FIG. The intake air-fuel mixture is being compressed.
第１４図は、受圧板３８がゲートを通過中であって、ゲ
ートは第１２図のように、シャノタージスク１と２の切
欠き３と４が全申合して、ケート開放中、同時に圧縮室
は、第１３図のように受１１：机３９の吸入側ＤＶｉ叫
似中であり、Ｆｌ・線側Ｃは曲同吸入混合免の圧縮作動
中である。FIG. 14 shows that the pressure receiving plate 38 is passing through the gate, and as shown in FIG. As shown in FIG. 13, the suction side DVi of the receiver 11: desk 39 is in operation, and the Fl/line side C is in the compression operation of the same suction mixture.
第１７図は、受圧板３８がゲートを通過した位ｊ６で、
ノヤノターゲ−１・４１は、第１５図のように、ンヤ、
ターシスク１と２の切欠き３と４の後縁Ｂが、ケートの
両縁と一致して、これよりンヤ、１・開始となる。同時
に圧縮室は、第１６図のように、受圧板３９により吸気
と圧縮の作動中である。In FIG. 17, at j6, the pressure receiving plate 38 passes through the gate.
Noyano Target 1.41 is Nya, as shown in Figure 15.
The trailing edges B of the notches 3 and 4 of the tarsisks 1 and 2 coincide with both edges of the cage, and from this point on, the beginning of 1 begins. At the same time, the compression chamber is in the process of suction and compression by the pressure receiving plate 39, as shown in FIG.
第２０図は、受圧板３８がゲートから１５°進角した位
置で、ケートは第１８図のように、シャ、ターソスク１
と２の切欠き３と４の後縁Ｂが、ケートの中間位置で一
致してシャツＩ・される、この位［ｉ？で第１９図、２
０図のように、圧縮しｊ−グーの通気口３３、及び、出
力ローターの通気［１３２がグーソングの連通［１３４
と重合を始め、圧縮室の受圧板目−縮側Ｃど、燃焼室の
受圧仮燃焼側Ｅとの連通が始まり、圧縮混合気の売気が
開始される、また、この位置で燃焼室の受圧板排出側Ｆ
は、前回排気の排出を開始する、同時に圧縮室の受圧板
３９の吸入側りは吸気作動中である。Figure 20 shows the position where the pressure receiving plate 38 is advanced by 15 degrees from the gate, and the gate is positioned as shown in Figure 18.
The trailing edges B of notches 3 and 4 of 2 and 2 are aligned at the middle position of the shirt, and this is the point [i? Figure 19, 2
As shown in Figure 0, the compressed j-goo vent 33 and the output rotor's ventilation [132 are connected to the goo song's communication [134
The pressure-receiving plate of the compression chamber - compression side C, etc., begins to communicate with the pressure-receiving temporary combustion side E of the combustion chamber, and the sale of the compressed air-fuel mixture begins. Pressure plate discharge side F
At the same time, the suction side of the pressure receiving plate 39 of the compression chamber is in the suction operation.
第２３図は、第２０図の充気開始から受ＩＦ板３８が１
５°進角して、第２１図、２２図のように、圧縮ロータ
ーの通気口３３、及び、出力口−ターの通気口３２が、
連通［１３４と全重合して充気最頂時である、燃焼室の
受圧板排出側Ｆは、前回排気の排気作動中、圧縮室の受
圧板吸入側りは吸気続行中である。FIG. 23 shows that the receiving IF board 38 is 1 from the start of charging in FIG. 20.
With an advance angle of 5 degrees, as shown in FIGS. 21 and 22, the compression rotor vent 33 and the output port vent 32 are
The pressure receiving plate discharge side F of the combustion chamber, which is fully polymerized with the communication [134 and is at the peak of filling, is in the process of exhausting the previous exhaust, while the pressure receiving plate suction side of the compression chamber is continuing intake.
第２６図は、受圧板３８が、第２３図の位置から１５°
進角して、通気口３２と連通１１３４との重合が外れて
充気が終了する、この位置で点火栓４０によって圧縮混
合気に点火され、受圧仮燃焼側Ｅは、その燃焼圧を受け
て進角する、受圧板排出側Ｆは前回排気の排出作動中、
同時に圧縮室は、第２５図のように受圧板３９が、ケー
ト前１５°の位置に在って、通気１１３３と連辿口３４
との重合が外れて連通が断たれ、充気を終了すると共に
受汗抱叫入側りも吸気を終ｒする、そのゲートは第２４
図のように、シャ。FIG. 26 shows that the pressure receiving plate 38 is 15° from the position of FIG. 23.
At this position, the compressed air-fuel mixture is ignited by the ignition plug 40, and the pressure-receiving temporary combustion side E receives the combustion pressure. The advancing pressure plate discharge side F is in the process of discharging the previous exhaust gas.
At the same time, in the compression chamber, as shown in FIG.
The polymerization between the 24th gate and
As shown, Sha.
ターノスク１と２の切欠き３と５のＡｆ ＨＡが、ケー
トの中間（ｉ’／ ｉｉ／で一致して、開き始める。Af HA in notches 3 and 5 of turnosks 1 and 2 coincide at the middle (i'/ii/ of the kate) and begin to open.
第２９図は、受圧板３８の燃焼側Ｅが燃焼圧を受けて進
角中であり、その排出価Ｆは排気作動中である、同時に
圧縮室は、第２８図のように受圧板３９がゲート面前に
進み、ゲート４１は第２７図のように、シャツタージス
ク１と２の切欠き３と５の前縁Ａが、グー！・の前縁に
一致して全開されている、
第３１図は、受圧板３９がケートを通過中で、ケートは
第３０図のように、シャノタージスク１と２の切欠き３
と５が全重合して開放中である、同時に燃焼室は第３２
図のように、受圧板の燃焼側Ｅ４燃焼圧を受けて進角中
であり、受圧扱排出側Ｆは排気［］３５から排気作動中
。In FIG. 29, the combustion side E of the pressure receiving plate 38 is receiving combustion pressure and is advancing, and the exhaust value F is in the exhaust operation. As the gate surface moves forward, the front edges A of the notches 3 and 5 of the shirt targisks 1 and 2 are in contact with the gate 41 as shown in Fig. 27. In Fig. 31, the pressure receiving plate 39 is passing through the cage, and the cage is fully opened in line with the front edge of the cage, as shown in Fig. 30.
and 5 are fully polymerized and are being opened, and at the same time the combustion chamber is in the 32nd
As shown in the figure, the combustion side E4 of the pressure receiving plate is advancing in response to the combustion pressure, and the pressure receiving discharge side F is in exhaust operation from the exhaust [ ] 35.
第３４図は、受圧板３９がゲートを通過した位１６で、
ゲートは第３３図のように、シャ、タージスク１と２の
切欠き３と５の後縁Ｂが、ゲートの両縁と−Ｍしてシャ
ｙ Ｉ・が開始される、同時に燃焼室は、第３５図のよ
うに受圧板の燃焼側Ｅは燃焼圧を受けて進角中、受ＩＦ
板１１出側Ｆは排気口３５から前回排領を排気作動中。FIG. 34 shows the position 16 where the pressure receiving plate 39 has passed through the gate.
As shown in Fig. 33, the rear edges B of the notches 3 and 5 of the gates 1 and 2 are connected to both edges of the gate, and the combustion chamber is started. As shown in Fig. 35, the combustion side E of the pressure receiving plate receives combustion pressure and is advancing, and the receiving IF
The outlet side F of the plate 11 is in the process of exhausting the previous discharge from the exhaust port 35.
第３７図は、受圧板３９がケートから１５°ｊｉ（角し
た位置で、受圧板吸入側ＤＶｉ吸気１］３６から吸気を
開始すると同時に、その圧縮側Ｃでｉ；１回吸人混合気
の圧縮を開始する、そのケートは第３６図のように、シ
ャノタージスク１と２の切欠き３と５の後縁Ｂが、ケー
トの中間（、γＩＦ７で一致してシャットされる、同時
に燃焼室は、第３８図のように、受圧仮燃＃１１１１１
Ｅは燃焼膨張圧を受けて進角中であると共に、その排出
側Ｆは前回排気の排出作動中である。Fig. 37 shows that the pressure receiving plate 39 starts taking air from the intake port 15°ji (in the angular position, the pressure receiving plate suction side DVi intake 1) 36, and at the same time, the intake air is To start compression, the cane is closed as shown in Fig. 36, so that the trailing edges B of the notches 3 and 5 of the cylinder disks 1 and 2 coincide with each other at the middle of the cane (γIF7), and at the same time the combustion chamber is As shown in Fig. 38, pressure-receiving temporary combustion #11111
E is advancing in response to the combustion expansion pressure, and its exhaust side F is in the process of discharging the previous exhaust.
第４０図は、受圧板３９の吸入側りは吸（（作動中であ
り、その圧縮側Ｃでは前同吸入混合気の圧縮作動中、同
時に燃焼室は第４１図のように、受圧仮燃焼側Ｅは膨張
カス圧を受けて進角すると共に、その排出側Ｆ Ｖｉｉ
ｉｒ回排気を排出中である、そのケートは第３９図のよ
うにンヤノタージスク２の切欠き５の重合によって開か
れているが、第４１図のようにシャ、ターソスク１によ
ってシャットされていて、ケートの気密は確保されてい
る、この位置から受圧板３８．３９はＪ４Ｅ角を続けて
、再び、第６図、７図、８図の位置に至りＩ−記の各作
動を連環する。Fig. 40 shows that the suction side of the pressure receiving plate 39 is in operation, and on the compression side C, the same suction mixture is being compressed, and at the same time the combustion chamber is undergoing pressure receiving preliminary combustion as shown in Fig. 41. The side E receives the expanded gas pressure and advances, and its discharge side F Vii
While the IR exhaust gas is being discharged, the gate is opened by the polymerization of the notch 5 of the Nyanotardisk 2 as shown in FIG. From this position, the pressure receiving plates 38 and 39 continue the J4E angle until they reach the positions shown in FIGS. 6, 7, and 8, and the operations described in I- are linked.
以１−のように、本ジスクエ／シンは、−回転中におけ
る、吸優、圧縮、燃焼、排気の各作動角が、それぞれ、
３００°以上である。As shown in 1- below, the present disk drive/shin has the following operating angles for suction, compression, combustion, and exhaust during rotation:
It is 300° or more.
第１図は本実施例の一部分断面側面図、第２図は一部分
断面側面図、第３図はシャノターシスク駆動系の・ド面
断面図、第４図は支持アームの斜視図、第５図は出力ロ
ーターの部分斜視図、第６図乃至第４１図は、本実施例
の説明図、第４２図はシャ、タージスク（１）の断面図
、第４３図はシャノタージスク（２）の断面図、第４・
４図は出力ローターの正面図、第４５図は圧縮ローター
のｉＥ ｌｉｉ図、各図の矢印は回転方向を示す。
１．２・・・・・・・・シャノタージスク、３．４，５
・・シスク切欠き、３０・・・・・・・・出力ローター
、３１・ 圧縮ローター、３８．３９・・・・・・・・
ローター受圧板、４１・・・・シャノターケ−１・、４
２．４２’・・−・・・シャノタージスク軸、
Ａ・・・・・・・シャノタージスク切欠き前縁、Ｂ ・
・・・シャ、ターシスク切欠き後縁、Ｃ受圧板圧線側、
Ｄ・・・・・・受圧板吸入側、Ｅ・・ 受圧根燃焼側、
Ｆ・・・・・・・・受圧板排出側、特許出願人 林
１１１ 八 ｒｉＩＬ茸４＋鎚
等５１鎚
算４０閣 蜂乎／図
＝１
手続補正書 （自発）
昭和５７年１２月１４日
特許庁長官
殿
１ 事件の表示 昭和５７年特許願第１４１５０号
２ 発明の名称 ジスクエンジン
３ 補正をする者
事件との関係 特許出願人
１３３−Fig. 1 is a partially sectional side view of this embodiment, Fig. 2 is a partially sectional side view, Fig. 3 is a cross-sectional view of the shaft drive system, Fig. 4 is a perspective view of the support arm, and Fig. 5 is a partially sectional side view of the present embodiment. FIGS. 6 to 41 are partial perspective views of the output rotor, and FIGS. 4.
Figure 4 is a front view of the output rotor, Figure 45 is a diagram of the compression rotor, and the arrows in each figure indicate the rotation direction. 1.2・・・・・・Shanotazhsk, 3.4,5
... Sisk notch, 30... Output rotor, 31 Compression rotor, 38.39...
Rotor pressure receiving plate, 41...Shanotake-1, 4
2.42'...Shanotarjisk shaft, A......Shanotarjisk notch front edge, B.
...Sha, Tashisk notch rear edge, C pressure plate pressure line side,
D...Pressure plate suction side, E...Pressure root combustion side,
F・・・・・・Pressure plate discharge side, patent applicant Hayashi
111 8 riIL Mushroom 4 + Hammer etc. 51 Hammer Count 40 Kaku Bee / Diagram = 1 Procedural Amendment (Spontaneous) December 14, 1980 To the Commissioner of the Japan Patent Office 1 Indication of Case Patent Application No. 14150 of 1988 2 Invention Name Disk Engine 3 Relationship to the person making the amendment case Patent applicant 133-
Claims (1)
タージスクによって開閉する、ジスクエンジンにおいて
、本文に詳記し図面に示すように、シャノタージスク軸
上の、シャ、クージスク（１）と（２）を、二重反転構
造としたことを特徴とする、ジスクエンジン ２、 シャツタージスク（１）には、切欠き（３）を設
け、シャ、タージスク（２）には、切欠き（４）と（５
）を設けた、特許請求の範囲第１項記載の、ジスクエン
ジン[Scope of Claims] 1. In a disc engine in which the shaft target I of the combustion chamber and the compression chamber is opened and closed by a shaft disc, as described in detail in the main text and shown in the drawings, The disc engine 2 is characterized in that 1) and (2) have a counter-rotating structure.The shirt disc (1) is provided with a notch (3); Notch (4) and (5
), the disc engine according to claim 1 is provided with
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP57014150A JPS58131320A (en) | 1982-01-30 | 1982-01-30 | Disc engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP57014150A JPS58131320A (en) | 1982-01-30 | 1982-01-30 | Disc engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS58131320A true JPS58131320A (en) | 1983-08-05 |
Family
ID=11853115
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP57014150A Pending JPS58131320A (en) | 1982-01-30 | 1982-01-30 | Disc engine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS58131320A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0552119A (en) * | 1991-08-22 | 1993-03-02 | Osamu Ikeda | Rotary piston engine |
| WO2010095225A1 (en) * | 2009-02-19 | 2010-08-26 | Murata Makoto | Rotary internal combustion engine |
| JP5147134B2 (en) * | 2006-05-09 | 2013-02-20 | オカムラ有限会社 | Rotary fluid machine |
-
1982
- 1982-01-30 JP JP57014150A patent/JPS58131320A/en active Pending
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0552119A (en) * | 1991-08-22 | 1993-03-02 | Osamu Ikeda | Rotary piston engine |
| JP5147134B2 (en) * | 2006-05-09 | 2013-02-20 | オカムラ有限会社 | Rotary fluid machine |
| WO2010095225A1 (en) * | 2009-02-19 | 2010-08-26 | Murata Makoto | Rotary internal combustion engine |
| US20110107999A1 (en) * | 2009-02-19 | 2011-05-12 | Makoto Murata | Rotary Internal Combustion Engine |
| CN102325975A (en) * | 2009-02-19 | 2012-01-18 | 村田诚 | Rotary combustion engine |
| JP4918177B2 (en) * | 2009-02-19 | 2012-04-18 | 誠 村田 | Rotary internal combustion engine |
| US20120210973A1 (en) * | 2009-02-19 | 2012-08-23 | Makoto Murata | Rotary internal combustion engine |
| EP2511473A3 (en) * | 2009-02-19 | 2013-06-19 | Makoto Murata | Rotary internal combustion engine |
| US8528505B2 (en) | 2009-02-19 | 2013-09-10 | Makoto Murata | Rotary internal combustion engine |
| US8528506B2 (en) | 2009-02-19 | 2013-09-10 | Makoto Murata | Rotary internal combustion engine |
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