TW470809B - Inner rotor engine with pairs of compression plates - Google Patents

Inner rotor engine with pairs of compression plates Download PDF

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Publication number
TW470809B
TW470809B TW088120575A TW88120575A TW470809B TW 470809 B TW470809 B TW 470809B TW 088120575 A TW088120575 A TW 088120575A TW 88120575 A TW88120575 A TW 88120575A TW 470809 B TW470809 B TW 470809B
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TW
Taiwan
Prior art keywords
compression
center
compression plate
inner rotor
rotor
Prior art date
Application number
TW088120575A
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Chinese (zh)
Inventor
Tian-Sheng Jou
Original Assignee
Tian-Sheng Jou
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Publication date
Application filed by Tian-Sheng Jou filed Critical Tian-Sheng Jou
Priority to TW088120575A priority Critical patent/TW470809B/en
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Publication of TW470809B publication Critical patent/TW470809B/en

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    • 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

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  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)

Abstract

The design of this invention comprises that a concentric rotor installed with four curved blades evenly separated in a cylindrical cylinder; a compression plate is provided in the concave part of each curved blade respectively; the small end of the compression plate is the pivotal point, while the large end is the moving point; and pulleys are provided on both sides of the large end, and move inwardly and outwardly along the curved guiding groove on the cylinder head, to form motions of the intake, compression, explosion and exhaust, so as to obtain four power source can be obtained in one revolution for a single cylinder set. This invention can be also designed to have an intake inlet or exhaust outlet in sequence for every 90 DEG. Therefore, there will be two intakes for each compression plate in one rotation, to make eight intakes in one rotation for a single cylinder set.

Description

I 1 ' 丨一 五、發明説明( ㈠先前技術 、内燃引擎發明使用一百餘年來,始終停留在現今最廣 汎使用的往復式設計,因動力輪出與動力源呈度差而 造成大量動力損失,油氣爆炸提供⑽度動力,而要帶動 排、進、墨共540度之動力損失,無珐提高敫率,故於三 四十年前再由德國人發明内轉子引擎由林東洋公司^ 造’雖能降低動力損失,但基本設計密合不良,造成 浪費等嚴重問題。 I㈡發明目的 由於目前引擎技術,效率低、零件繁多、製造維修不 易’已不符未來環境要求,本發明利用小排氣量、高壓縮 比及較^的油氣比,較長的力距、密集動力,以達高效 率、低損失、低耗油、低污染等目的,更因零件少,製 雒修成本低廉。 ° ㈢技術重點 當各壓縮片支點中心達圖式一190度時完成排氣,隨 後開始進氣,到達275度時完成進氣,隨後開始壓縮,到 0度時完成壓縮並點火引爆油氣,高齡推動壓縮片順著 導向溝槽轉動至1〇5度時完成舒壓,隨後開始排氣,至 190度時完成排氣並隨即進氣延續下個循環。 每一缸組四壓縮片隨著内轉子轉動,囡導向溝槽關係 如圖式穴、七,其中一壓縮片在進氣時,順時鐘方向各壓 縮片則依序爲壓、爆、排。 ㈣動作説明 本紙張尺度適财@@家標準(,)A4驗(2獻297公釐) i¾-- f請先閱锖背面之注意事項再填寫本頁) -訂 經濟部智慧財產局員工消費合作社印製 經濟部智慧財產局員工消費合作社印製 A7 __ B7___ 五、發明説明(二) ①進氣:如圖式六所示,當壓縮片7A支點中心到達190 度時,該片滑輪正在導向溝槽270度端極點, i 壓縮片貼緊氣缸壁⑵,把前次廢氣完全排擠出 排氣口⑸,支點中心通過190 °後,壓縮片亦 通過進氣口⑷,又因滑輪組被導向溝槽遷引之 關係,壓縮片開始向内移動而形成吸進氣。 | |②壓縮:如圖式六所示,壓縮片7B支點中心到275度 | 時,滑輪組在導向溝槽0度端最低凹點,而形 成全開吸氣狀態,支點中心通過275度後,因 j j 滑輪組被導向溝槽導引,壓縮片開始往外擠壓 ! ,形成壓縮作用。 ③ 爆炸:如圖式七所示,壓縮片7C支點中心到達0度 時’滑輪組在導向溝槽右方最南極點壓縮片 氣缸壁預留1.5度燃燒空間,隨即點火引爆油 氣,高溫高壓氣體會擠壓壓縮片向内移動,而 滑輪組會順著導向溝槽帶著壓縮片及内轉子往 190度方向轉動,支點中心到達105度時完成 爆炸作用。 ④ 排氣:如圖式六所示,壓縮片7D支點中心通過105 度時,滑輪組在導向溝槽190度最内端開始往 270度端極點移動,7D之廢氣也通過排氣口⑸ ; ,壓縮片繼續向氣缸壁靠而將廢氣擠出排氣口 ,當支點中心到達190度時,壓縮片與氣缸壁 . | 完全密合,完全排出廢氣。 本紙張尺度適用中國國家標準(C^S ) Μ規格(210&gt;&lt;297公釐) — !-------裝 訂 冰 (請先聞讀背面之注意事項再填寫本頁) A7 B7 五、發明説明(三,) ⑤氣、液態壓縮機動作説明: 如圖式八所示,壓縮片通過進口,有9〇度時間進, 隨即進行90度壓縮排出,再90度進90度壓出,單壓 縮片循環360度進排,進排各二次,動作原理與本發 明引擎相同’只是增設一對進出口及每次進、排各爲 90度。 (請先閲讀背面之注意事項再填寫本頁) 經濟部智慧財產局員工消費合作社印製 本紙張尺度適用中國國家標準(CNS ) A4規格(210Χ:297公釐) 470809 A9 B9 C9 D9 圖式 圖式説明: 圖式一:引擎右侧視内部平面圖 向』—内轉子與壓縮片組裝立體圖 右引擎蓋平面圖 左引擎蓋平面圖 引擎主零件組裝立體圖 =片、崎子與右將蓋導向溝槽關係平面 ^片、内轉子輿右引擎蓋導向溝槽關係平面 氧、液態壓縮機右侧視内部平面圖 圖内數字説明: 1.引擎外體(水套) 2..氣缸 | 3.螺絲孔 | 4.進氣孔 i 經濟部智慧財產局員工消費合作社印製 圖式二 圖式三 圖式四 圖式五 圖式六 圖式七 圖式八 (請先閲讀背面之注意事項再行紛製} 丨5.排氣孔 6.内轉子 | Z壓縮片 | 8.壓縮片支點中心 ;9.壓縮片滑輪組 ία火星塞 | u.0度座標 l·2.右引擎蓋導向溝槽 丨13·中心軸承 i 14左引擎蓋導向溝槽 本紙張尺度適用中國國家橾举.(CNS〉M規格〈210x297公釐}I 1 '丨 15. Description of the invention (㈠The previous technology, the invention of the internal combustion engine has been used for more than a hundred years, and has always remained in the most widely used reciprocating design today. A large amount of power is caused by the poor degree of power wheels and power sources. The loss, the oil and gas explosion provides the power, and to drive a total of 540 degrees of power loss, exhaust, and ink, without enamel to increase the rate, so the inner rotor engine was invented by the Germans 30 to 40 years ago by Lin Dongyang Company ^ Although it can reduce the power loss, the basic design is not tight, causing serious problems such as waste. I. Purpose of the invention Because of the current engine technology, low efficiency, a large number of parts, and difficult manufacturing and maintenance, it is no longer in line with future environmental requirements. Gas volume, high compression ratio and relatively high oil and gas ratio, long force distance, dense power, in order to achieve high efficiency, low loss, low fuel consumption, low pollution and other purposes, but also because of fewer parts, the maintenance cost is low. ° ㈢Technical focus The exhaust is completed when the center of each fulcrum's fulcrum reaches pattern 190 degrees, and then the air intake is started. The air intake is completed when it reaches 275 degrees, and then the compression starts to 0 degrees. It compresses and ignites the oil and gas, and pushes the compression disc to rotate along the guide groove to 105 degrees to complete the relaxation pressure, and then starts to exhaust, and then exhausts to 190 degrees and then continues the next cycle of intake. As the inner rotor of the cylinder group rotates, the relationship between the guide grooves and the grooves is as shown in the figure, and when one of the compression plates is in the air intake, the compression plates in the clockwise direction are sequentially compressed, burst, and exhausted. Note that this paper size is suitable for financial @@ 家 标准 (,) A4 inspection (2 297 mm) i¾-- f Please read the notes on the back of the page before filling in this page)-Ordered by the Intellectual Property Bureau of the Ministry of Economic Affairs and Consumer Cooperatives Printed by A7 __ B7___ of the Consumer Cooperatives of the Intellectual Property Bureau of the Ministry of Economics and Economics 5. Description of the Invention (2) ① Intake: As shown in Figure 6, when the center of the 7A fulcrum of the compression plate reaches 190 degrees, the pulley is guiding the groove At the 270-degree pole, the i compression plate is pressed against the cylinder wall ⑵, and the previous exhaust gas is completely exhausted out of the exhaust port ⑸. After the center of the fulcrum passes through 190 °, the compression plate also passes through the air inlet ⑷. Relationship, the compressed film began to Moving the suction intake is formed. | | Compression: As shown in Figure 6, when the center of the fulcrum of the compression plate 7B reaches 275 ° |, the lowest depression of the pulley group at the 0 ° end of the guide groove forms a fully open suction state. After the center of the fulcrum passes 275 °, jj The pulley block is guided by the guide groove, and the compression piece starts to squeeze outward!, forming a compression effect. ③ Explosion: As shown in Figure 7, when the center of the 7C fulcrum of the compression plate reaches 0 degrees, the pulley block has 1.5 degrees of combustion space on the cylinder wall at the southmost pole of the compression groove on the right side of the guide groove, and then ignites the oil and gas. Squeeze the compressed piece to move inward, and the pulley block will follow the guide groove with the compressed piece and the inner rotor to rotate in the direction of 190 degrees. When the center of the fulcrum reaches 105 degrees, the explosion effect is completed. ④ Exhaust: As shown in Figure 6, when the center of the 7D fulcrum of the compression plate passes 105 degrees, the pulley block starts to move toward the 270-degree pole at the innermost end of the guide groove 190 degrees, and the exhaust gas of 7D also passes through the exhaust port ⑸; The compression plate continues to lean against the cylinder wall and pushes the exhaust gas out of the exhaust port. When the center of the fulcrum reaches 190 degrees, the compression plate is completely tight with the cylinder wall. | The exhaust gas is completely discharged. This paper size applies the Chinese National Standard (C ^ S) M specification (210 &gt; &lt; 297mm) —! ------- binding ice (please read the precautions on the back before filling this page) A7 B7 5. Description of the invention (3,) ⑤ Description of the operation of the gas and liquid compressors: As shown in Figure 8, the compressed tablet passes through the inlet and has 90 degrees of time to enter, and then 90 degrees of compression and discharge, and then 90 degrees of pressure into 90 degrees of pressure Out, the single compressed piece enters and discharges 360 degrees in a cycle, and enters and discharges twice each. The operating principle is the same as that of the engine of the present invention. (Please read the notes on the back before filling out this page) The paper size printed by the Employees' Cooperatives of the Intellectual Property Bureau of the Ministry of Economy applies the Chinese National Standard (CNS) A4 specification (210 ×: 297 mm) 470809 A9 B9 C9 D9 Schematic drawing Description of the formula: Figure 1: Internal plan view of the right side of the engine "-perspective view of the assembly of the inner rotor and the compression plate. Right hood plan view. Left hood plan view. Assembled perspective view of the main parts of the engine. ^ The inner rotor and the right hood guide grooves are related to the plane. Oxygen and liquid compressors are viewed from the right. The internal plan view shows the figures in the figure: 1. Engine outer body (water jacket) 2. Cylinder | 3. Screw holes | 4. Air inlet i Printed by the Consumer Cooperatives of the Intellectual Property Bureau of the Ministry of Economic Affairs, two plans, three plans, four plans, five plans, six plans, seven plans, eight (please read the precautions on the back before making changes) 丨 5 Exhaust hole 6. Inner rotor | Z compression disc | 8. Compression disc fulcrum center; 9. Compression disc pulley set ία Mars plug | u.0 degree coordinate l · 2. Right hood guide groove 丨 13 · center bearing i 14 left hood guide groove book Zhang Shu scale applicable Chinese national held. (CNS> M size <210x297 mm}

Claims (1)

=修正 *·** Α8 Β8 C8 DS 修k 手謗麵 ί R倉明 Άw 内 容 t? 4S 隹 r •fe l'/f M l 經濟部智慧財產局員工消費合作杜印製 、申請專利範圍 l一種内置對數壓縮片_子引擎,其構造為—個以上教 虹内置相同數目之同心_轉子,内轉 片 平分圓周肢,_子中心為動力輪㈣,與其他= 内轉子連接並貫穿_有互相對解向軸之側,作為 動力輪出,内轉子内置對數壓縮片,_片—端呈圓筒 狀,密合地箝人_子末端圓筒狀凹槽,作為壓縮片^ 支點;另-端貫穿-支軸,並於支軸兩姆置凸出壓縮 片之滑輪’滑輪在兩侧導向溝槽内,隨著導向溝槽與圓 ο心距離遠近而控讎制_筒蚊點為㈣心做離内 轉子圓心遠近之圓弧形動作;壓縮片外緣呈與氣缸内壁 —同弧’當壓縮片被導向溝槽控制推向離内轉子圓心最遠 時,壓縮片外緣與氣缸壁密合,形成完全壓縮及完全= 氣狀態;當壓縮片被導向溝槽控制至離内轉子圓心最近 時’壓縮片孤形面與氣缸形成一個空間體積,形成完全 進氣及氣爆後完全舒壓狀態。 2.如申請專利範圍内第一項所述之内置對數壓縮片式内轉 子引擎,其内轉子之一尖端運轉至進氣口後,後方之壓 縮片呈與氣缸密合狀態,完成排氣,隨後持續運轉中該 壓縮片被導向溝槽控制’逐漸向内轉子圓心移動,呈進 氣狀態。 3·如申請專利範圍内第一項所述之内置對數壓縮片式内轉 子引擎,其内轉子之一壓縮片完全進氣後,因内轉子持 續運轉而該壓縮片被導向溝槽控制開始往離内轉子圓心 最遠處移動,直炱與氣缸壁密合,形成壓縮狀態。 !____ _______ 本紙張尺度適用中國圃家標準(CNS〉Μ规捧(210x297公釐) ^-- f請先閱讀背面之注意事項再填寫本頁〕 訂.. 經濟部智慧財產局員工消費合作社印製 C8 D8 穴、申讀專利乾圍 4, 如申請專利範圍内第一項所述之内置對數壓縮片式内轉 子引擎,其内轉子之一壓縮片完成壓縮後,氣爆之壓力 完全加之予該壓縮片,而使該壓縮片順著兩侧導向溝槽 之曲線往内轉子圓心擠壓,直至該壓縮片離内轉子圓心 最近,完成舒壓動作,是該申請專利範圍之内置數對壓 縮片式内轉子引擎動力來源。 5, 如申請專利範圍内第一項所述之内置對數壓縮片式内轉 子引擎,其内轉子之一壓縮片完成氣爆後,該壓縮片迫 使内轉子運轉,而該壓縮片至與内轉子圓心最近後,該 壓縮片隨即順著順導向溝槽往離内轉子圓心最遠處移 動,過程經過排氣口,直至該壓縮片與氣缸壁密合,完 | 成排氣狀態。 (請先閱讀背面之注意事項再填窝本頁) 、1TI .峡! 本紙張尺度適用中國國家標準(CNS ) Α4规格(210X297公釐)= Amendment * · ** Α8 Β8 C8 DS Repairing hand 谤 R warehouse MingΆw Content t? 4S 隹 r • fe l '/ f M l Printing and application of patents for consumer cooperation of intellectual property bureau of the Ministry of Economic Affairs l A built-in logarithmic compression blade _ sub-engine, which is structured in that more than one teaching rainbow has the same number of concentric _ rotors, the inner rotor is divided equally into the circumferential limbs, _ the sub-center is the power wheel, and is connected with the other = the inner rotor and runs through. The side of the decoupling axis is opposed to each other as a power wheel. The inner rotor has a built-in logarithmic compression plate. The _piece-end is cylindrical and closely clamps the cylindrical groove at the end of the child to serve as a compression point. -The end runs through the fulcrum, and the sheaves of the compression pieces protruding on the two fulcrum of the fulcrum are placed in the guide grooves on both sides, and controlled as the distance between the guide groove and the center of the circle is controlled. The center of the cylinder performs an arc-shaped action at a distance from the center of the inner rotor; the outer edge of the compression plate is the same arc as the inner wall of the cylinder. 'When the compression plate is controlled to be pushed to the farthest distance from the center of the inner rotor by the guide groove, the outer edge of the compression plate and the cylinder The walls are tightly sealed, forming a fully compressed and fully = gaseous state; when the compressed sheet is guided Control from the tank to the center of the inner rotor recent 'compressed arc-shaped surface sheet formed with the cylinder volume of a space formed after the complete explosion of the intake air and completely diastolic pressure state. 2. According to the built-in logarithmic compression-type internal rotor engine described in the first item in the scope of the patent application, after the tip of one of the internal rotors runs to the air inlet, the rear compression plate is in close contact with the cylinder to complete the exhaust. During subsequent continuous operation, the compression plate is controlled by the guide groove to gradually move to the center of the inner rotor and assumes an air intake state. 3. According to the built-in logarithmic compression disc type internal rotor engine described in the first item in the scope of the patent application, after one of the internal rotor's compression fins is fully air-in, the compression fins are guided by the groove control to start the continuous movement of the internal rotor. It moves farthest from the center of the inner rotor circle, and the mullion is in close contact with the cylinder wall to form a compressed state. ! ____ _______ This paper size applies Chinese garden standards (CNS> M Regulations (210x297 mm) ^-f Please read the precautions on the back before filling out this page) Order: Printed by the Employees' Cooperatives of the Intellectual Property Bureau of the Ministry of Economic Affairs Make C8 D8 cavity, apply for patent dry-wall 4, as described in the first item in the scope of the patent application, the built-in logarithmic compression internal rotor engine, after the compression of one of the internal rotors, the pressure of the gas explosion is fully applied. The compression plate is pressed against the inner rotor circle center along the curve of the guide grooves on both sides until the compression plate is closest to the inner rotor circle center to complete the pressure relief action. It is a built-in pair of compressions within the scope of the patent application. The source of power for the internal rotor engine of the chip type. 5, as described in the first item of the patent application, the built-in logarithmic compression type internal rotor engine, one of the internal rotors of the internal compression rotor completes the gas explosion, the compression plate forces the internal rotor to run, After the compression plate is closest to the center of the inner rotor, the compression plate then moves along the guide groove to the farthest point from the center of the inner rotor, and passes through the exhaust port until the compression plate and the cylinder wall (Please read the notes on the back before filling in this page), 1TI. Gap! This paper size applies the Chinese National Standard (CNS) Α4 size (210X297 mm)
TW088120575A 1999-11-25 1999-11-25 Inner rotor engine with pairs of compression plates TW470809B (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
TWI494501B (en) * 2009-12-14 2015-08-01 Gotek Energy Inc Rotary, internal combustion engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
TWI494501B (en) * 2009-12-14 2015-08-01 Gotek Energy Inc Rotary, internal combustion engine

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