TW200928077A - Seal for a rotary valve for an internal combustion engine - Google Patents

Seal for a rotary valve for an internal combustion engine Download PDF

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Publication number
TW200928077A
TW200928077A TW097138693A TW97138693A TW200928077A TW 200928077 A TW200928077 A TW 200928077A TW 097138693 A TW097138693 A TW 097138693A TW 97138693 A TW97138693 A TW 97138693A TW 200928077 A TW200928077 A TW 200928077A
Authority
TW
Taiwan
Prior art keywords
valve
gas
compression
engine
rotary valve
Prior art date
Application number
TW097138693A
Other languages
Chinese (zh)
Inventor
Gordon Mcnally
Original Assignee
Gordon Mcnally
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 Gordon Mcnally filed Critical Gordon Mcnally
Publication of TW200928077A publication Critical patent/TW200928077A/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L7/00Rotary or oscillatory slide valve-gear or valve arrangements
    • F01L7/02Rotary or oscillatory slide valve-gear or valve arrangements with cylindrical, sleeve, or part-annularly shaped valves
    • F01L7/021Rotary or oscillatory slide valve-gear or valve arrangements with cylindrical, sleeve, or part-annularly shaped valves with one rotary valve
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L7/00Rotary or oscillatory slide valve-gear or valve arrangements
    • F01L7/02Rotary or oscillatory slide valve-gear or valve arrangements with cylindrical, sleeve, or part-annularly shaped valves
    • F01L7/021Rotary or oscillatory slide valve-gear or valve arrangements with cylindrical, sleeve, or part-annularly shaped valves with one rotary valve
    • F01L7/024Cylindrical valves comprising radial inlet and axial outlet or axial inlet and radial outlet
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L7/00Rotary or oscillatory slide valve-gear or valve arrangements
    • F01L7/16Sealing or packing arrangements specially therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L2820/00Details on specific features characterising valve gear arrangements
    • F01L2820/01Absolute values
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N3/00Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
    • F01N3/08Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous
    • F01N3/10Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust
    • F01N3/24Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust characterised by constructional aspects of converting apparatus
    • F01N3/30Arrangements for supply of additional air
    • F01N3/32Arrangements for supply of additional air using air pump
    • 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
    • F02B75/02Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/027Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle four
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B21/00Engines characterised by air-storage chambers
    • F02B21/02Chamber shapes or constructions

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Valve-Gear Or Valve Arrangements (AREA)
  • Supercharger (AREA)

Abstract

A gas seal between a port 10, 12 of a rotary valve 7 and a port 8 in a combustion chamber 6 of a rotary valve engine, the seal comprising gas channel means 15 forming a turbo valve means 26 surrounding the port 8 in the combustion chamber and compression means 20, 21 for creating a pressure in the gas channel means greater than a pressure in the combustion chamber during a compression stroke and a power stroke of the engine.

Description

200928077 九、發明說明: 【發明所屬之技術領域j 本發明係有關於一種供用於内燃機之旋轉閥的密封 件。 5 ❹ 10 . 15 Φ 20 【先前技術3 習知的市面上可買得到的内燃機自1892年至今已在原 則上作了些許的改變。雖然有許多不同種類的内燃機,但 它們均使用類似的原則。 一種習知的四行程内燃機包括一氣缸塊,該氣缸塊包 括至少一氣缸孔,一活塞可在其中往復地移動;一曲軸箱, 其可轉動地支持藉由一連桿連接至活塞的一曲柄轴;以及 包含一閥機構的一氣缸頭部,該閥機構包括開放至氣缸孔 的一進氣閥及一排氣閥。當該曲柄軸轉動時,該活塞在氣 缸孔内往復地移動。曲柄轴的轉動亦造成在氣缸頭部内的 一凸輪軸之轉動,因此,使用數個機構之一即可開關在氣 缸頭部中的進氣及排氣閥。 在誘導或進氣行程中,活塞以離開機構的方向沿著氣 缸孔移動’而進氣閥是打開的。形成在活塞及閥機構之間 的氣缸孔内的一内燃室中的一部份真空自譬如一化油器中 抽出霧化燃料及空氣混合物至氣缸孔中。 在一回復行程中,活塞沿著氣缸孔朝向進氣閥已關閉 的閥機構移動’因而壓縮位在活塞以及進氣及排氣閥定位 在其中的孔的一端之間的壓縮室中的氣體。 當活塞沿著氣缸孔朝向進氣閥及排氣閥而到達其往復 5 200928077 動作之後段時,發生了點火,點燃了壓縮燃料及空氣混合 物。如此產生了一動力行程,其以離開閥機構的一方向推 動活塞,進而轉動曲柄軸。 5 然後,活塞朝向閥機構移動,進而廢氣閥打開,迫使 5熱的廢氣自a缸及氣缸頭料出,並經由一廢氣路徑排出 内蟋機。 該四行程内燃機須要用以操作在氣缸頭部内的閥系統 之許多構件。這些構件增加了内燃機的成本。内燃機亦會 排出大量的廢氣形式下的有害氣體。 © 10 在過去,由於較適合的材料可被取得,已製造出較高 速且具可靠性的功能佳的内燃機。然而,人們仍然想要製 造其他種類的内燃機,且最流行的另一種已商業化的產品 為二行程内燃機。二行程内燃機與更流行的四行程内燃機 i5之不同在於其僅在活塞的兩個行程中完成相同的四個步驟 (進氣,壓縮,供給動力,排氣)。此種結果係藉由使用壓縮 . 行程之開始,以及供給動力行程之後段,分別執行排氣及 進氣的功能而達成。如此允許曲柄的每一週轉形成一供給 © 動力行程’而非如在一四行程内燃機中每兩次週轉方能形 成〜供給動力行程。因此,二行程内燃機備置高的效能, 因此較適於可攜式,重量輕的應用中。 然而’人們已提議以一旋轉閥替換習知内燃機的閥及 連椁,俾以供應氣體至内燃機的一氣缸,並自氣缸中排出 氣體。 美國專利4,852,532揭露用於一内燃機的一旋轉閥,該 6 200928077 内燃機具有一中空圓筒形轉子 傾斜的-體成型之障板,而纟^丁两有沿著其孔的一 草板而在該障板的兩側上借右檢曰 該等槔配置成可在備有埠,且 一窗相福兮結μ 得于轉動時,與在氣缸中的 固相通。該轉子為滾筒支持, 轉子的-π 而料滾筒支持在形成於 轉千的表面上的一凹槽中, 内表面上。數個密封料,氣紅頭部的-孔的 _对件^者該窗而備置, 的該等㈣件配置在縱向凹槽 #長條構成 3δΑβ6,2Ι . 等凹槽形成在氣缸200928077 IX. Description of the invention: [Technical field to which the invention pertains] The present invention relates to a seal for a rotary valve for an internal combustion engine. 5 ❹ 10 . 15 Φ 20 [Prior Art 3 The commercially available internal combustion engine has been slightly modified in principle since 1892. Although there are many different types of internal combustion engines, they all use similar principles. A conventional four-stroke internal combustion engine includes a cylinder block including at least one cylinder bore in which a piston is reciprocally movable, and a crankcase rotatably supporting a crank connected to the piston by a connecting rod a shaft; and a cylinder head including a valve mechanism, the valve mechanism including an intake valve and an exhaust valve open to the cylinder bore. When the crankshaft rotates, the piston reciprocates within the cylinder bore. The rotation of the crankshaft also causes rotation of a camshaft within the cylinder head, so that one of several mechanisms can be used to switch the intake and exhaust valves in the cylinder head. During the induction or intake stroke, the piston moves along the cylinder bore in the direction away from the mechanism and the intake valve is open. A portion of the vacuum in an internal combustion chamber formed in the cylinder bore between the piston and the valve mechanism extracts the atomized fuel and air mixture into the cylinder bore from a carburetor. During a return stroke, the piston moves along the cylinder bore toward the valve mechanism in which the intake valve is closed' thereby compressing the gas in the compression chamber between the piston and the end of the bore in which the intake and exhaust valves are positioned. When the piston reaches the intake and exhaust valves along the cylinder bore and reaches its reciprocating 5 200928077 action, ignition occurs, igniting the compressed fuel and air mixture. This produces a power stroke that pushes the piston in a direction away from the valve mechanism, thereby rotating the crankshaft. 5 Then, the piston moves toward the valve mechanism, and the exhaust valve opens, forcing 5 hot exhaust gas to be discharged from the a-cylinder and the cylinder head, and discharged to the internal boring machine via an exhaust path. The four-stroke internal combustion engine requires a number of components for operating the valve system within the cylinder head. These components increase the cost of the internal combustion engine. The internal combustion engine also emits a large amount of harmful gases in the form of exhaust gas. © 10 In the past, higher-speed and reliable internal combustion engines have been manufactured because of the availability of suitable materials. However, there is still a desire to manufacture other types of internal combustion engines, and another popular commercial product is a two-stroke internal combustion engine. The two-stroke internal combustion engine differs from the more popular four-stroke internal combustion engine i5 in that it performs the same four steps (intake, compression, supply, exhaust) in only two strokes of the piston. This result is achieved by using the compression and the start of the stroke and the post-supply stroke to perform the functions of exhaust and intake, respectively. This allows each turn of the crank to form a supply © power stroke ' instead of every two turns in a four-stroke internal combustion engine to form a power supply stroke. Therefore, the two-stroke internal combustion engine is equipped with high efficiency, so it is more suitable for portable and lightweight applications. However, it has been proposed to replace the valves and ports of the conventional internal combustion engine with a rotary valve to supply gas to a cylinder of the internal combustion engine and to exhaust the gas from the cylinder. U.S. Patent 4,852,532 discloses a rotary valve for an internal combustion engine having a hollow cylindrical rotor inclined-body-formed baffle, and the two have a grass plate along the hole therein. The right side of the baffle is placed on the right side of the baffle so that it can be placed in a solid state in the cylinder when a window is provided and the window is formed to rotate. The rotor is supported by a roller, and the -π of the rotor is supported by a roller on a surface formed on the surface of the thousand, on the inner surface. A plurality of sealing materials, the head of the gas red head - the hole of the hole is placed in the window, and the (four) pieces are arranged in the longitudinal groove #长条结构3δΑβ6,2Ι. The groove is formed in the cylinder

=的:且圓筒形環容納在氣-頭部的孔内的環狀凹 槽中。該等縱向長條以表面接觸方式晚接在該等圓周環之 一的表面的各端。數個通道備置在肢頭部中,俾以冷卻 水’且備置在轉子巾,俾以冷卻油。轉子的冷卻藉由輕射 熱至轉子孔的-她鄰表面而完成,該表面為水通道中的水 以及在油通道中的流動油所冷卻。 英國專利22343〇0揭露一冷卻空氣旋轉間,其包括在圓 15筒形旋轉閥内的一進氣管,當該管與氣缸對齊時,其與開 放至氣缸的一進氣口相通;以及一廢氣管,其與一廢氣埠 相通,而該廢氣埠與當與氣缸對齊時,開放至氣缸中的進 氣口在圓周上錯置。包含密封環的兩個圓周凹槽定位在進 氣口及排氣口的兩側,俾以隔離該等埠與外在環境。縱向 20密封桿的備置用以隔離進氣口及排氣口。旋轉閥藉由通過 旋轉閥的一孔之空氣而冷卻。 美國專利5,941,206揭露用於内燃機的—旋轉閥,其包 括一圓筒形閥轉子,在該轉子的一圓周表面上具有一進氣 口及排氣口。數個架設在閥轉子上的密封元件隔開轉子本 7 200928077 體的圓周表面,俾以界定分開的圓周表面區。該區之一配 置成使得當旋轉閥容納在一氣缸頭部中的一閥孔内時,該 密封元件ffltb接在閥孔表面上,而該進氣口及排氣口週期性 地被密封。 5 WO 02/27165專利揭露一轉動閥引擎,其備有容納一環 狀計時環的一内燃機殼體,備有一關閉端以及一開放端的 一可轉動氣缸;以及在該氣缸内的一活塞。該氣缸經由一 傳輸總成被活塞機械性地驅動,而該總成包括一連桿,該 連桿驅動一齒輪,並依次接合形成在該氣缸的開放端上的 10 一斜齒輪。該旋轉閥被強迫通過旋轉氣缸的油所冷卻。 美國專利2004/0144361揭露一旋轉閥内燃機,其包括 一曲柄軸,一節流閥,一節流閥起動器,一氣缸頭部,一 内燃機,以及至少一旋轉閥。該旋轉閥具有至少兩個埠, 該兩個埠在其週邊上形成開口端,該氣缸頭部具有一孔, 15 而旋轉閥在其中轉動。在該孔中的一窗與燃燒室相通,該 開口藉由轉動連續地與窗對齊。備有相位改變裝置的一驅 動機構驅動旋轉閥。該等埠包括一進氣口以及排氣口,且 該相位改變裝置回應至少一内燃機循環中的内燃機的操作 狀況的改變,施加一相位改變。 20 旋轉閥引擎的一大問題為須要尋找密封旋轉閥的閥 埠,俾以在壓力下防漏。 美國專利5,526,780揭露一種用於内燃機的一旋轉閥, 其中該閥具有軸向密封元件以及内週邊密封元件構成的一 組合,該等元件配置成一第一密封件加壓孔穴,該孔穴在 200928077 . 軸向密封元件以及兩個第二密封件加壓孔穴之間作週邊地 延伸,而該兩個第二密封件加壓孔穴各自位在内及毗鄰外 週邊密封元件之間,而該等密封元件軸向地位在一氣缸頭 部中的一窗開口的兩側上,而該閥在氣缸頭部中旋轉。此 5 配置允許高壓燃燒氣體自第一孔穴流至該兩個第二孔穴, 使得在燃燒時,該等外週邊密封元件由於朝向週邊延伸凹 槽的軸向最外側邊的力量,密封第二加壓孔穴,而該等外 週邊密封元件定位在該凹槽中,俾以阻止氣體作軸向向外 〇 的移動。該等内週邊密封元件軸向地向内負重,俾以朝向 10 週邊延伸凹槽的軸向最内側邊密封,而該等内週邊密封元 件定位在該等凹槽中,並軸向地使得該四個週邊密封元件 負重,俾以朝向一孔表面密封,而閥容納在該孔表面中, 且朝向它預先負重。 WO 03/100232揭露一種用於可旋轉閥總成的一閥密封 15 件機構,其在如同一旋轉氣缸閥内燃機中所使用的一旋轉 閥元件以及一固定閥元件之間備置一密封件。在一實施例 ® 中,該密封件機構包括一大體上堅固的密封框架,該框架 圍繞並密封圓筒形閥元件之一的閥埠的周圍,且亦密封另 一圓筒形閥元件的一表面。在另一實施例中,該密封件機 20 構包括具有可變直徑的一可彈性偏動的管狀元件,其架設 成繞著一第一閥元件,而該管狀元件的一直徑徑向地與第 一閥元件的一閥埠對齊,且該管狀元件在第一閥元件之外 徑向地偏動。閥及密封件機構的冷卻藉由抽出通過在閥的 一殼體中的冷卻劑通道,並旋轉閥元件的下方部份的冷卻 9 200928077 液而完成。 WO 2005八19018揭露一種 硬用於夂轉閥内燃機的一密封 組合,該内燃機具有一氣缸,卫 且邊氟缸包括與一燃燒室相 通的一閥埠。該氣紅可繞著复扃 可,、在一閥殼體的一圓筒形孔中 的縱轴轉動,該閥殼體具有— 硬氣口以及一排氣口,該等 埠適於在殼體中的氣缸轉動時,拉说 接續地與該閥琿對齊,俾 以使得流體㈣猶至崎Μ,且自^流出。—密封 件繞著在氣缸及一共中心表面之„μ 印之間的閥埠而備置,且包括 定位在氣缸中的一凹槽中的—率 10 15 在封件元件,在該閥埠中的 流體壓力在該密封件元件上作無 Τ動’俾以驅使該密封件元件 與共中心表面接觸,且自該埠的 垾的中心之外與該凹槽之周圍 接觸。 獨雇/02娜揭露料轴向旋轉閥内燃機的—密封 件系統,其包括-排浮動的氣體密封件以及―可選擇的 油封系統。該成排的浮動密封件圍繞著在氣㈣的孔中的 一窗’而通過該窗’等閥埠與-燃燒室相通。該成排的浮 動密封件包括軸向密封件,以及容納在氣紅頭的孔中的長 形孔中的週邊密封件,其㈣等週邊密封件軸向地配置在 轴向密封件的端部之間。該閥可藉由通過閥而抽出的油六 卻。 ^ wo 2_/024_揭露用於内燃機的—軸向流動_ 閥,其包括具有-孔的—氣缸頭’而—轴向流動旋轉間在 該孔中轉動。該閥具有一圓筒形中心部份,以及一進氣口 以及一排氣口,該等埠的末端為於在中心部份上的開口 20 200928077 . 該開口週期性地通過在孔中的一窗與一燃燒室相通。在中 心部份以及孔之間的一間隙為一排浮動密封件密封,該成 排的浮動密封件包括至少兩個軸向密封件,該等密封件分 隔於該窗的相對側邊上。該總成另包括至少一浮動的軸向 5 延伸遮蔽密封件,其配置在窗外,且在週邊上與軸向密封 件遠離。在一些實例中,閥藉由通過閥而抽出的油所冷卻。 因此,顯然地,在習知技藝中均使用複雜的機械組合 作為一旋轉閥的密密封件,俾以在壓力下防止軸向滲漏。 ❹ 【發明内容】 10 本發明的目的是至少減少上述習知技藝的缺點。 依據本發明,其備置一氣體密封件系統,該系統在一 旋轉閥的一埠,以及在一旋轉閥引擎的一燃燒室中的一埠 之間,該密封件包括形成圍繞著燃燒室埠的一渦輪閥構件 的一氣體通道構件,以及用以在氣體通道構件中形成一壓 • 15 力的一壓縮構件,而該壓力在内燃機的一壓縮行程以及一 動力行程中,較燃燒室中的壓力大。 ® 具有優點地,在渦輪閥構件以及旋轉閥的一外表面之 間的一間隙大約為0.0254 mm(l密耳)。 便利地,該壓縮構件包括一渦輪閥射出器構件,該構 20 件用以大體上切線地射出氣體至渦輪閥構件中。 便利地,該氣體密封件系統另包括一位置感應器構 件,其用以感測旋轉閥的一轉子的一旋轉位置,俾以傳送 信號至壓縮構件。 便利地,該氣體密封件系統另包括閥構件,其用以在 11 200928077 接收到感應器構件的信號時,控制壓縮氣體自壓縮構件進 入渦輪閥射出器構件。 具有優點地,該壓縮構件包括一壓縮室構件。 便利地,該壓縮構件包括被旋轉閥引擎的一曲柄軸轉 5 動的壓縮構件。 可選擇地,該壓縮構件包括被内燃機的進氣及動力行 程加壓的内燃機的一曲軸箱。 便利地,該曲軸箱包括一單向閥構件,其在内燃機壓 縮及排氣行程時,允許空氣進入曲軸箱中。 10 便利地,該氣體密封件系統另包括一止回閥構件,其 使得來自曲軸箱的壓縮空氣進入壓縮室構件中。 依據本發明的第二特徵,其備置一旋轉閥引擎,其包 括如上所述的一氣體密封件。 便利地,旋轉閥的一轉子配置成為通過轉子的一孔的 15 水所冷卻。 依據本發明的第三特徵,其備置一種方法,該方法在 旋轉閥的一埠以及在内燃機的一燃燒室中的一埠之間的一 旋轉閥引擎中設置一密封件,其包括以下步驟:備置一氣 體通道構件,其形成圍繞燃燒室埠的一渦輪閥構件;以一 20 氣體壓縮構件在氣體通道構件中形成一壓力,該壓力在内 燃機的一壓縮行程以及一動力行程中較燃燒室中的壓力 大。 便利地,該方法另包括大體上以一渦輪閥射出器構件 切線地射出氣體至渦輪閥構件中。 200928077 . 便利地,該方法另包括以一感應器構件感測出旋轉閥 的一轉子的一旋轉位置。 便利地,該方法另包括在接收到感測器構件之信號之 後,控制自壓縮構件進入渦輪閥射出器構件的壓縮氣體。 5 具有優點地,在氣體通道裝置中的一壓力包括在一壓 縮室構件中形成一壓力。 便利地,在氣體通道構件中的一壓力包括以旋轉閥引 擎的一曲柄軸驅動的一壓縮器構件形成一壓力。 ® 可選擇地,在氣體通路構件中的一壓力包括藉由内燃 10 機的進氣及動力行程加壓,在内燃機的一曲軸箱中的氣體。 便利地,在曲軸箱中加壓氣體包括在内燃機的壓縮及 排氣行程後,允許空氣通過一單向閥構件進入曲軸箱中。 便利地,在氣體通路構件中形成一壓力包括壓縮空氣 通過曲轴箱,經由氣壓管構件以及一止回閥構件,進入壓 15 縮室構件中。 本發明將藉由實例以及圖式詳加說明,其中: ® 第1圖為依據本發明的一旋轉閥内燃機的一剖開圖式; 第2圖為第1圖的内燃機的一垂直,縱向橫截面圖; 第3圖為第1圖的内燃機的一側視圖; 20 第4圖為第1圖的内燃機的一前視圖; 第5圖為第1圖的内燃機的一後視圖; 第6圖為第1圖的内燃機的一前視圖,該内燃機包括一 氣體壓縮系統; 第7圖為第6圖的内燃機的垂直,橫向戴面圖; 13 200928077 第8圖為第6圖的内燃機的一氣體密封件的一垂直,橫 向截面圖;以及 第9圖為第8圖的氣體密封件的平面圖。 t 】 5 在圖式中’類似的標號代表類似的部份。 現在參看第1至3及7圖,一旋轉閥引擎包括一單片氣缸 塊1以及氣缸頭部2,其省去了用以連接一分開的氣缸塊及 氣缸頭部的在一標準的内燃機中是必要元件的氣缸頭栓, 以及一氣缸頭墊圈,而該等元件在一以水冷卻的内燃機中 10可能是一漏水的源頭。該單片結構體亦備置較一標準的内 燃機堅固的結構。氣缸塊1備有一習知的曲柄軸3,連桿4, 以及活塞5。現在參看圖式中的内燃機之方向,在氣缸頭部 2内,以及活塞5之上的燃燒室6之上備有一旋轉閥7,該閥 控制進入及排出的氣體,該氣體分別經由燃燒室6之上端的 15 埠8進出。 使用内燃機之前方的一齒狀帶9,備有埠8的旋轉閥了 為曲柄轴3精確地所驅動,俾以對齊在旋轉閥7的週邊内的 進氣口 1G及排氣口 12’而準確的程度與在—標準内燃機中 的打開及關閉閥中的凸輪及機械機構所提供的相同。當活 2〇塞5向下移動至一氣缸11的一孔中的氣虹塊i時,旋_7内 的-埠10轉動至在氣缸頭埠8上的—位置,以允許進入的氣 體被拉至燃燒室6中。 ^ 當活塞5在-壓縮行程中上升氣紅孔中的氣缸^時,旋 轉閥7繼續轉動並封鎖氣㈣部2中的蜂8。然後,壓縮的電 200928077 火星塞所賴,形錢_7_轉動時的 荷為’譬如, 一動力行程< 時,在旋轉閥1中^订程中再次升起氣缸’俾以排出廢氣 轉閥7中的排氣口以到 允許廢氣通過旋轉間,自内間料2中的蟬8,以 中完成;各缸氣各白目 … 出。此步驟在内燃機 口。 %各自具有在旋轉町_成_進氣及排氣=: and the cylindrical ring is received in an annular recess in the bore of the gas-head. The longitudinal strips are joined to each end of the surface of one of the circumferential rings in a surface contact manner. Several channels are placed in the head of the limb, and the water is cooled and placed in the rotor to cool the oil. The cooling of the rotor is accomplished by lightly radiating heat to the adjacent surface of the rotor bore which is cooled by the water in the water passage and the flowing oil in the oil passage. British Patent No. 22,343,0 discloses a cooling air rotating chamber comprising an intake pipe in a circular cylindrical rotary valve which communicates with an air inlet opening to the cylinder when the pipe is aligned with the cylinder; An exhaust pipe that communicates with an exhaust gas enthalpy that is circumferentially offset from the intake port that is open to the cylinder when aligned with the cylinder. Two circumferential grooves including a seal ring are positioned on both sides of the intake and exhaust ports to isolate the helium and the external environment. The longitudinal 20 seal rods are provided to isolate the intake and exhaust ports. The rotary valve is cooled by passing air through a hole in the valve. U.S. Patent No. 5,941,206 discloses a rotary valve for an internal combustion engine which includes a cylindrical valve rotor having an intake and exhaust port on a circumferential surface of the rotor. A plurality of sealing elements mounted on the valve rotor separate the circumferential surface of the rotor to define a separate circumferential surface area. One of the zones is configured such that when the rotary valve is received in a valve bore in a cylinder head, the sealing member ffltb is attached to the valve bore surface, and the intake and exhaust ports are periodically sealed. 5 WO 02/27165 discloses a rotary valve engine having an internal combustion engine housing housing a ring-shaped timing ring, a rotatable cylinder having a closed end and an open end, and a piston within the cylinder. The cylinder is mechanically driven by a piston via a transmission assembly, and the assembly includes a link that drives a gear and sequentially engages a helical gear formed on the open end of the cylinder. The rotary valve is forced to cool by rotating the oil of the cylinder. U.S. Patent No. 2004/0144361 discloses a rotary valve internal combustion engine including a crankshaft, a throttle valve, a throttle valve starter, a cylinder head, an internal combustion engine, and at least one rotary valve. The rotary valve has at least two turns that form an open end on a periphery thereof, the cylinder head having an aperture 15 and a rotary valve rotating therein. A window in the aperture communicates with the combustion chamber, the opening being continuously aligned with the window by rotation. A drive mechanism provided with a phase change device drives the rotary valve. The ports include an air inlet and an air outlet, and the phase changing means applies a phase change in response to a change in the operating condition of the internal combustion engine in at least one internal combustion engine cycle. A major problem with the rotary valve engine is the need to find a valve that seals the rotary valve to prevent leakage under pressure. No. 5,526,780 discloses a rotary valve for an internal combustion engine, wherein the valve has a combination of an axial seal member and an inner peripheral seal member, the members being configured as a first seal pressurizing bore, the bore being at 200928077. Extending circumferentially between the sealing member and the two second sealing member pressing holes, wherein the two second sealing member pressing holes are located between and adjacent to the outer peripheral sealing member, and the sealing member shaft The valve is positioned on either side of a window opening in a cylinder head and the valve rotates in the cylinder head. The 5 configuration allows high pressure combustion gases to flow from the first cavity to the two second holes such that upon combustion, the outer peripheral sealing elements seal the second due to the force of the axially outermost side of the groove extending toward the periphery The holes are pressurized and the outer peripheral sealing elements are positioned in the grooves to prevent the gas from moving axially outwardly. The inner peripheral sealing members are axially biased inwardly and are sealed toward the axially innermost side of the circumferentially extending groove 10, and the inner peripheral sealing members are positioned in the grooves and axially The four peripheral sealing elements are loaded with weight to seal against a surface of the bore, and the valve is received in the surface of the bore and preloaded towards it. WO 03/100232 discloses a valve seal 15 piece mechanism for a rotatable valve assembly that provides a seal between a rotary valve member and a fixed valve member as used in the same rotary cylinder valve internal combustion engine. In an embodiment®, the seal mechanism includes a substantially rigid sealing frame that surrounds and seals around the valve bore of one of the cylindrical valve members and also seals a surface of the other cylindrical valve member . In another embodiment, the sealer 20 includes an elastically biasable tubular member having a variable diameter that is erected about a first valve member and a diameter of the tubular member is radially A valve bore of the first valve member is aligned and the tubular member is radially biased outside of the first valve member. The cooling of the valve and seal mechanism is accomplished by drawing a coolant passage through a housing in the valve and rotating the lower portion of the valve member for cooling 9 200928077. WO 2005819018 discloses a seal assembly for use in a slewing valve internal combustion engine having a cylinder, the slewing cylinder including a valve port in communication with a combustion chamber. The gas red can be rotated around a longitudinal axis of a cylindrical bore of a valve housing having a hard air port and an exhaust port adapted to be in the housing When the cylinder is rotated, the pull is continuously aligned with the valve 俾 so that the fluid (4) is still rugged and flows out. - the seal is placed around the valve between the cylinder and a common central surface, and includes a rate 10 15 positioned in a recess in the cylinder, in the seal element, in the valve The fluid pressure is free of turbulence on the seal member to urge the seal member into contact with the common center surface and contact the periphery of the groove from the center of the ridge of the cymbal. A rotary seal internal combustion engine-seal system comprising a row of floating gas seals and an optional oil seal system. The rows of floating seals pass around a window in the bore of the gas (four) The window 'equal valve 相 communicates with the combustion chamber. The row of floating seals includes an axial seal, and a peripheral seal contained in the elongated hole in the hole of the gas red head, (4) a peripheral seal shaft Aligned between the ends of the axial seals. The valve can be extracted by the oil through the valve. ^ wo 2_/024_ exposes the axial flow _ valve for internal combustion engines, which includes - Hole-cylinder head's - axial flow rotation between the holes Rotating in. The valve has a cylindrical central portion, and an air inlet and an exhaust port, the ends of the turns being openings 20 in the central portion. 200928077. The opening periodically passes through the hole a window is in communication with a combustion chamber. A gap between the central portion and the aperture is a row of floating seal seals, the row of floating seals including at least two axial seals, the seals being separated from The opposite side of the window. The assembly further includes at least one floating axial 5 extended shield seal disposed outside the window and spaced away from the axial seal on the periphery. In some examples, the valve is passed The oil extracted by the valve is cooled. Therefore, it is apparent that in the prior art, a complicated mechanical combination is used as a tight seal of a rotary valve to prevent axial leakage under pressure. ❹ [Summary] SUMMARY OF THE INVENTION It is an object of the present invention to at least reduce the disadvantages of the above-described prior art. In accordance with the present invention, a gas seal system is provided which is a glimpse of a rotary valve and a ram in a combustion chamber of a rotary valve engine. The seal member includes a gas passage member forming a turbine valve member surrounding the combustion chamber bore, and a compression member for forming a pressure in the gas passage member, and the pressure is in the internal combustion engine The compression stroke and the one power stroke are greater than the pressure in the combustion chamber. ® Advantageously, a gap between the turbine valve member and an outer surface of the rotary valve is approximately 0.0254 mm (l mil). Conveniently, The compression member includes a turbine valve injector member for generally tangentially injecting gas into the turbine valve member. Conveniently, the gas seal system further includes a position sensor member for sensing rotation A rotational position of a rotor of the valve, to transmit a signal to the compression member. Conveniently, the gas seal system further includes a valve member for controlling the compression of the compressed gas when the signal of the inductor member is received at 11 200928077 The member enters the turbine valve injector member. Advantageously, the compression member comprises a compression chamber member. Conveniently, the compression member includes a compression member that is pivoted by a crankshaft of the rotary valve engine. Alternatively, the compression member includes a crankcase of the internal combustion engine that is pressurized by the intake and power paths of the internal combustion engine. Conveniently, the crankcase includes a one-way valve member that allows air to enter the crankcase during compression and exhaust strokes of the internal combustion engine. 10 Conveniently, the gas seal system further includes a check valve member that causes compressed air from the crankcase to enter the compression chamber member. According to a second feature of the invention, a rotary valve engine is provided which includes a gas seal as described above. Conveniently, a rotor of the rotary valve is configured to be cooled by 15 holes of a hole in the rotor. According to a third feature of the invention, there is provided a method of providing a seal in a rotary valve engine between a rotary valve and a rotary valve in a combustion chamber of the internal combustion engine, comprising the steps of: A gas passage member is formed which forms a turbine valve member surrounding the combustion chamber bore; a pressure is formed in the gas passage member by a 20 gas compression member, the pressure being in the combustion chamber in a compression stroke and a power stroke of the internal combustion engine The pressure is great. Conveniently, the method further includes tangentially injecting gas into the turbine valve member generally with a turbine valve injector member. 200928077. Conveniently, the method further includes sensing a rotational position of a rotor of the rotary valve with an inductor member. Conveniently, the method further includes controlling the compressed gas entering the turbine valve injector member from the compression member after receiving the signal from the sensor member. 5 Advantageously, a pressure in the gas passage means includes forming a pressure in a compression chamber member. Conveniently, a pressure in the gas passage member includes a compressor member that is driven by a crankshaft of the rotary valve engine to create a pressure. ® Optionally, a pressure in the gas passage member includes a gas in a crankcase of the internal combustion engine by pressurizing the intake and power strokes of the internal combustion engine. Conveniently, pressurizing the gas in the crankcase includes allowing air to enter the crankcase through a one-way valve member after the compression and exhaust stroke of the internal combustion engine. Conveniently, forming a pressure in the gas passage member includes passing compressed air through the crankcase through the pneumatic tube member and a check valve member into the pressure chamber member. The invention will be explained in detail by way of examples and drawings, in which: Fig. 1 is a cutaway view of a rotary valve internal combustion engine according to the present invention; Fig. 2 is a vertical, vertical and horizontal cross section of the internal combustion engine of Fig. 1. Fig. 3 is a side view of the internal combustion engine of Fig. 1; Fig. 4 is a front view of the internal combustion engine of Fig. 1; Fig. 5 is a rear view of the internal combustion engine of Fig. 1; A front view of the internal combustion engine of Fig. 1 including a gas compression system; Fig. 7 is a vertical and lateral wear diagram of the internal combustion engine of Fig. 6; 13 200928077 Fig. 8 is a gas seal of the internal combustion engine of Fig. 6. A vertical, transverse cross-sectional view of the piece; and Figure 9 is a plan view of the gas seal of Figure 8. t 】 5 In the drawings, similar reference numerals denote similar parts. Referring now to Figures 1 through 3 and 7, a rotary valve engine includes a single cylinder block 1 and a cylinder head 2 which eliminates the need for a separate cylinder block and cylinder head for connection to a standard internal combustion engine. It is a cylinder head plug of the necessary components, and a cylinder head gasket, and these components may be a source of water leakage in a water-cooled internal combustion engine. The monolithic structure is also provided with a stronger structure than a standard internal combustion engine. The cylinder block 1 is provided with a conventional crankshaft 3, a connecting rod 4, and a piston 5. Referring now to the direction of the internal combustion engine in the drawings, a rotary valve 7 is provided in the cylinder head 2 and on the combustion chamber 6 above the piston 5, the valve controlling the incoming and outgoing gases, respectively, via the combustion chamber 6 15 埠 8 on the top end. Using a toothed belt 9 in front of the internal combustion engine, a rotary valve provided with a crucible 8 is precisely driven for the crankshaft 3 to align the intake port 1G and the exhaust port 12' in the periphery of the rotary valve 7 The degree of accuracy is the same as that provided by the cams and mechanical mechanisms in the opening and closing valves in standard internal combustion engines. When the live 2 plug 5 is moved downward to the air block i in a hole of a cylinder 11, the -10 in the coil 7 is rotated to the position on the cylinder head 8 to allow the incoming gas to be Pulled into the combustion chamber 6. ^ When the piston 5 ascends the cylinder in the red hole in the -compression stroke, the rotary valve 7 continues to rotate and blocks the bee 8 in the gas (four) portion 2. Then, the compressed electricity 200928077 Mars plugs, the money _7_ when the rotation is 'for example, a power stroke', when the rotary valve 1 in the booking process, the cylinder is lifted again to exhaust the exhaust gas The exhaust port in the valve 7 is made to allow the exhaust gas to pass through the rotating chamber, and is completed from the crucible 8 in the inner material 2; each cylinder gas is white. This step is at the internal combustion engine. % each has a rotation in the town _ into _ intake and exhaust

10 1510 15

的方二:較:知氣广的冷卻更具有效力 進入在氣1_—前 [域中的熱。水 如此確保轉+7得彳並在—後端14處離開。 社構俨u 的所欲冷卻效果。轉子7為一單片 可在4 適於㈣地配合任何數量軌缸,使得水 " 並通過另一端排出,不似-些習知旋轉閥, 、進氣及廢氣必須使用兩端中的一端傳遞,因而僅適於 無任何水冷卻的單—氣^^燃機。 本發明的旋轉閥的一項優點在於進氣及排氣閥塑形成 了作為&準内燃機的一習知埠,俾以允許氣體通過轉子 的—側進入及離開。此意謂著該氣缸或該等氣缸的進氣可 2〇進入轉子,通過它至其中心,然後向下移動至氣缸。 在燃燒發生之後’在轉子中的廢氣埠打開,俾以允許 廢氣進入該廢氣埠,並被迫通過轉子的一中心,進而向外 通過轉子的側邊,並通過氣缸頭埠,至一排氣管。 如此允許水進入轉子的前方,且具有繞著橫跨轉子之 15 200928077 兩側邊而架設的各蟑的一明禮的通道。 轉子的熱膨脹之控制易於達成,俾以與氣紅頭部維持 一滑動的間隙。 參看第4圖,排氣口12具有一彎曲的前緣口,如第6圖 5中清楚地顯示’該前緣轉氣缸頭部表面18上堆積的碳, 俾以確保燃燒麼力的最大密封,儘可能地減少以下將救述 的凹槽15中所須的-氣壓,俾以確保在内燃機的整個氣缸 頭部2使用壽命中的密封。 現在參看第1及7至9圖,為維持在氣缸頭部2内的進氣 ◎ 1〇之壓縮,備置一凹槽15,其包圍氣虹的一上端之一外表面 上的埠8,且連接至空氣通道,如第8圖所示,俾以形成一 渦輪閥26。空氣在壓力下被供應至渦輪閥26。空氣可為未 顯不的,以曲柄軸3驅動的小壓縮機所供應,或如第6圖中 所示,所須要的壓力在内燃機内部為活塞5所產生。 15 當活塞5上升時,未顯示的在曲轴箱19的側邊上的一閥 自動地開放至大氣中,以允許空氣抽至曲軸箱中。當活塞5 下降至内燃機的動力行程時,曲軸箱閥關閉,且活塞壓縮 〇 在曲軸箱19内的空氣,迫使空氣通過氣壓管以及一止回閥 20,至一空氣儲存室21中。在一多氣缸内燃機上,曲軸箱 20具有未顯不的分隔壁,其鑄造成曲軸箱的一部份,或分開 地配置,俾以備置個別的室,而該等室在曲柄軸的主要軸 承上設有一油封。如此允許各室與在各別室中的活塞之向 下行程及向上行程所起動的一各別空氣閥系統共同工作。 空氣儲存室的此充電在内燃機的每次動力行程中發生 16 200928077 兩次’使得空氣儲存室21備有定量的壓縮空氣。當内燃機 的活塞5為其動力行程在壓縮下上升時,一螺線管閥22被在 氣缸頭部2中的轉子7所操作的一感應器23觸發成操作狀 況’俾以允許空氣經由氣壓管系統24及電子螺線管閥22自 5 ❹ 10 15 ❹ 20 空氣儲存室21引導至一渦輪閥射出器25,該射出器迫使壓 縮空氣大體上切線地進入圓形凹槽15,如第9圖所示,俾以 繞著渴輪閥26的凹槽15高速地循環。雜閥26定位在燃燒 至6的一上端’且僅與轉子7的週邊16距離〇 〇254爪爪。英吋 的 1/1000)。 渴輪閥26的-壁的一上部備有與轉子7的一外週邊配 〇的一輪廓,且具有一斜面27。如此可集中氣壓在轉子7的 一表面以及渦輪閥的一上邊緣之間的〇 〇254 mm(i/i〇〇〇英 吋)之間隙28上。 在渴輪閥及轉子表面之間的間隙28中循環的壓力配置 成較燃燒室6⑽氣壓A ’使得所有賴料及引爆燃燒氣體 在壓縮及動力行程中維持在燃燒室6中。 在内燃機的燃燒及排氣行程進行中,此外部氣壓維持 在满輪閥26中。當轉子7内的排氣diq移動至在埠8上的一 位置’俾以允許廢氣排出時’感應器Μ自轉子了接收一脈 動,並送出造成螺線管閥22關閉的—信號。同時,繞著渦 輪閥26的壓縮空氣流出_,以料P即將進人大氣中的廢 氣。 一習知__會發散出大4的有毒氣體至大氣中。 此係由於排出閥由於操作而變得過熱,因而過度加熱通過 17 200928077 它們的氣體。由於本發明的内燃機在十分涼的狀況下操 作’且不會產生這些問題,内燃機發散出的廢氣產生較習 知内燃機少的空氣污染。 須瞭解的是螺線管閥22可以,譬如,一機械凸輪從動 5 閥所替代。 【圖式簡皁說明】 第1圖為依據本發明的一旋轉閥内燃機的一剖開圖式; 第2圖為第1圖的内燃機的一垂直,縱向橫截面圖; 第3圖為第1圖的内燃機的一側視圖; 第4囷為第1圖的内燃機的一前視圖; 第5圖為第1圖的内燃機的一後視圖; 第6圖為第1圖的内燃機的一前視圖,該内燃機包括一 氣體壓縮系統; 第7圖為第6圖的内燃機的垂直’橫向截面圖; 第8圖為第6圖的内燃機的一氣體密封件的一垂直,橫 向截面圖;以及 第9圖為第8圖的氣體密封件的平面圖 【主要元件符號說明】 l··.氣缸塊 7…旋轉閥; 2…氣缸頭部 8…埠 3…曲柄軸 9…齒狀帶 4…連桿 10…進氣口 5…活塞 ll·.·氣缸 6…燃燒室 12…排氣口 200928077 13…前端 21…空氣儲存室 Μ…後端 22···螺線管閥 15…凹槽 23…感應器 16…旋轉閥的表面 24…氣壓管系統 17…彎曲的前緣 25···渦輪閥射出器 18…氣缸頭部表面 26…渦輪閥 19…曲轴箱 27···斜面 20…止回閥 28…間隙Fang 2: Compared with: the wide-ranging cooling is more effective. Entering in the gas 1_- before [the heat in the domain. The water is thus guaranteed to turn +7 and exit at the rear end 14. The cooling effect of the community 俨u. The rotor 7 is a single piece that can fit any number of rail cylinders at 4 (4) so that the water is discharged through the other end. Unlike some conventional rotary valves, the intake and exhaust gases must use one of the ends. Transfer, and thus only suitable for single-gas burners without any water cooling. An advantage of the rotary valve of the present invention is that the intake and exhaust valves are shaped as a conventional reference for "quasi-internal combustion engines" to allow gas to pass through and exit the side of the rotor. This means that the intake of the cylinder or cylinders can enter the rotor, pass it to its center, and then move down to the cylinder. After the combustion occurs, the exhaust gas in the rotor is opened to allow the exhaust gas to enter the exhaust gas, and is forced to pass through a center of the rotor, and then outwardly through the side of the rotor, and through the cylinder head to the exhaust tube. This allows water to enter the front of the rotor and has a clear passageway around the sides of the rotor that erects the sides of the 15200928077. The control of the thermal expansion of the rotor is easily achieved by maintaining a sliding gap with the gas red head. Referring to Fig. 4, the venting opening 12 has a curved leading edge opening, as shown in Fig. 6 clearly showing 'the leading edge of the carbon deposited on the head surface 18 of the cylinder head, to ensure maximum compression of the combustion force. The air pressure required in the recess 15 to be circulated below is reduced as much as possible to ensure a seal over the life of the entire cylinder head 2 of the internal combustion engine. Referring now to Figures 1 and 7 to 9, in order to maintain the compression of the intake air in the cylinder head 2, a recess 15 is provided which surrounds the cymbal 8 on the outer surface of one of the upper ends of the gas rainbow, and Connected to the air passage, as shown in Figure 8, to form a turbine valve 26. Air is supplied to the turbine valve 26 under pressure. The air may be unobstructed, supplied by a small compressor driven by the crankshaft 3, or as shown in Fig. 6, the required pressure is generated inside the internal combustion engine by the piston 5. When the piston 5 is raised, a valve, not shown, on the side of the crankcase 19 is automatically opened to the atmosphere to allow air to be drawn into the crankcase. When the piston 5 is lowered to the power stroke of the internal combustion engine, the crankcase valve is closed and the piston compresses the air trapped in the crankcase 19, forcing air through the air tube and a check valve 20 into an air storage chamber 21. In a multi-cylinder internal combustion engine, the crankcase 20 has an unobstructed dividing wall that is cast as part of the crankcase or separately configured to provide individual chambers, and the main bearings of the chambers in the crankshaft There is an oil seal on it. This allows the chambers to work in conjunction with a separate air valve system activated by the downward and upward strokes of the pistons in the respective chambers. This charging of the air storage chamber occurs in each power stroke of the internal combustion engine. 16 200928077 twice 'the air storage chamber 21 is provided with a quantity of compressed air. When the piston 5 of the internal combustion engine is raised under compression for its power stroke, a solenoid valve 22 is triggered by an inductor 23 operated by the rotor 7 in the cylinder head 2 into an operating condition '俾 to allow air to pass through the air tube. System 24 and electronic solenoid valve 22 are directed from 5 ❹ 10 15 ❹ 20 air storage chamber 21 to a turbine valve injector 25 that forces compressed air to enter the circular recess 15 generally tangentially, as shown in FIG. As shown, the crucible circulates around the groove 15 of the thirteen wheel valve 26 at a high speed. The miscellaneous valve 26 is positioned at an upper end 'burning to 6' and is only spaced from the periphery 16 of the rotor 7 by 〇 254 claws. 1/1000 of the UK). An upper portion of the wall of the thirteen wheel valve 26 is provided with a contour that is aligned with an outer periphery of the rotor 7, and has a slope 27. Thus, the concentrated air pressure is on the gap 28 of 〇 254 mm (i/i 〇〇〇 之间) between a surface of the rotor 7 and an upper edge of the turbine valve. The pressure circulating in the gap 28 between the thirst wheel valve and the rotor surface is arranged to be higher than the combustion chamber 6 (10) air pressure A' such that all of the material and the detonating combustion gas are maintained in the combustion chamber 6 during compression and power stroke. This external air pressure is maintained in the full wheel valve 26 during the combustion and exhaust stroke of the internal combustion engine. When the exhaust gas diq in the rotor 7 is moved to a position '俾 on the crucible 8 to allow the exhaust gas to be exhausted', the inductor receives a pulse from the rotor and sends a signal that causes the solenoid valve 22 to close. At the same time, the compressed air flowing around the scroll valve 26 flows out to feed the exhaust gas which is about to enter the atmosphere. A conventional __ will emit a large 4 toxic gas into the atmosphere. This is because the discharge valve becomes overheated due to operation, and thus the gas is excessively heated through 17 200928077. Since the internal combustion engine of the present invention operates in a very cool condition and does not cause such problems, the exhaust gas emitted from the internal combustion engine produces less air pollution than the conventional internal combustion engine. It should be understood that the solenoid valve 22 can be replaced, for example, by a mechanical cam driven 5 valve. BRIEF DESCRIPTION OF THE DRAWINGS Fig. 1 is a cross-sectional view of a rotary valve internal combustion engine according to the present invention; Fig. 2 is a vertical, longitudinal cross-sectional view of the internal combustion engine of Fig. 1; Figure 1 is a side view of the internal combustion engine; Figure 4 is a front view of the internal combustion engine of Figure 1; Figure 5 is a rear view of the internal combustion engine of Figure 1, and Figure 6 is a front view of the internal combustion engine of Figure 1 The internal combustion engine includes a gas compression system; FIG. 7 is a vertical 'transverse cross-sectional view of the internal combustion engine of FIG. 6; and FIG. 8 is a vertical, transverse cross-sectional view of a gas seal of the internal combustion engine of FIG. 6; and FIG. Fig. 8 is a plan view of the gas seal of Fig. 8 [main element symbol description] l··. cylinder block 7... rotary valve; 2... cylinder head 8...埠3...crankshaft 9...toothed belt 4...link 10... Intake port 5...Piston ll···Cylinder 6...Combustion chamber 12...Exhaust port 200928077 13...Front end 21...Air storage chamberΜ...Back end 22···Solenoid valve 15...groove 23...inductor 16 ...the surface 24 of the rotary valve...the pneumatic tube system 17...the curved leading edge 25···the turbo valve injector 1 8...Cylinder head surface 26...Steam valve 19...Crankcase 27···Bevel 20...Check valve 28...Gap

1919

Claims (1)

200928077 十、申請專利範圍: 1. 一種氣體密封件系統,其位在一旋轉閥引擎的一旋轉閥 的一埠以及一燃燒室中的一埠之間,該密封件包括氣體 通道構件,該構件形成圍繞該燃燒室埠的一渦輪閥構 5 件;以及一壓縮構件,該壓縮構件用以在該引擎的一壓 縮行程以及一動力行程期間,在該氣體通道構件中形成 一壓力,而該壓力大於該燃燒室中的一壓力。 2. 如申請專利範圍第1項的氣體密封件系統,其中在該渦輪 閥構件以及該旋轉閥的一外表面之間的一間隙大約為 10 0.0254 mm(l 密耳)。 3. 如申請專利範圍第1項的氣體密封件系統,其中該壓縮構 件包括一渦輪閥射出器構件,該射出器構件用以大體上 切線地射出氣體至該渦輪閥構件中。 4. 如申請專利範圍第3項的氣體密封件系統,其包括一位置 15 感應器構件,該構件用以感測出該旋轉閥的一轉子的一 旋轉位置,俾以發出信號至該壓縮構件。 5. 如申請專利範圍第4項的氣體密封件系統,其包括一閥構 件,該構件用以在接收到來自該感應器構件之信號時, 控制該壓縮構件中的壓縮氣體進入該渦輪閥射出器構 20 件。 6. 如申請專利範圍第1項的氣體密封件系統,其中該壓縮構 件包括一壓縮室構件。 7. 如申請專利範圍第1項的氣體密封件系統,其中該壓縮構 件包括壓縮器構件,而該壓縮器構件被該旋轉閥引擎的 200928077 一曲柄軸驅動。 8.如申請專利範圍第1項的氣體密封件系統,其中該壓縮構 件包括該引擎的一曲軸箱,且該曲軸箱為該引擎的進氣 及動力行程所加壓。 5 9.如申請專利範圍第8項的氣體密封件系統,其中該曲軸箱 包括一單向閥構件,其用以允許空氣在該引擎的壓縮及 排出行程進行時,進入該曲軸箱中。 10. 如申請專利範圍第8項的氣體密封件系統,其包括一止回 (non-return)閥構件,該止回閥構件用以使得該曲軸箱中 10 的壓縮空氣進入該壓縮室構件。 11. 一種旋轉閥引擎,其包括如申請專利範圍第1項的一氣體 密封件。 12. 如申請專利範圍第11項的旋轉閥引擎,其中該旋轉閥的 一轉子配置成藉由通過該轉子的一孔的水所冷卻。 15 13. —種備置一密封件於一旋轉閥引擎中該引擎之一旋轉閥 中的一埠以及一燃燒室中的一埠之間的方法,該方法包 括以下步驟: a.備置一氣體通道構件,其形成圍繞該燃燒室埠的 一渦輪閥構件; 20 b.以氣體壓縮構件在該氣體通道構件中形成一壓 力,該壓力在該引擎的一壓縮行程以及一動力行程期 間,大於在該燃燒室中的一壓力。 14.如申請專利範圍第13項的方法,其包括藉由一渦輪閥射 出器構件,大體上切線地射出氣體至該渦輪閥構件中。 21 200928077 15. 如申請專利範圍第13項的方法,其包括藉由一感應器構 件感測出該旋轉閥的一轉子的一旋轉位置,俾以發出信 號至該壓縮構件。 16. 如申請專利範圍第14項的方法,其包括當接收到來自該 5 感應器構件的信號時,控制該壓縮構件中的壓縮氣體進 入該渦輪閥射出器構件。 17. 如申請專利範圍第13項的方法,其中在該氣體通道構件 中形成一壓力的步驟包括在一壓縮室構件中形成一壓 力。 10 18.如申請專利範圍第13項的方法,其中在該氣體通道構件 中形成一壓力包括藉由被該旋轉閥引擎的一曲柄軸驅動 的一壓縮機構件形成一壓力。 19. 如申請專利範圍第13項的方法,其中在該氣體通道構件 中形成一壓力包括藉由該引擎的進氣及動力行程,加壓 15 在該引擎的一曲軸箱中的空氣。 20. 如申請專利範圍第19項的方法,其中在該曲轴箱中加壓 空氣包括在該引擎的壓縮及排出行程中,允許空氣通過 一單向閥構件,進入該曲軸箱中。 21. 如申請專利範圍第17項的方法,其中在該氣體通道構件 20 中形成一壓力的步驟包括使得該曲軸箱中的壓縮空氣通 過一氣壓管構件及一止回閥構件進入該壓縮室構件。200928077 X. Patent application scope: 1. A gas seal system, which is located between a turn of a rotary valve of a rotary valve engine and a turn of a combustion chamber, the seal comprising a gas passage member, the member Forming a turbine valve member 5 around the combustion chamber bore; and a compression member for forming a pressure in the gas passage member during a compression stroke and a power stroke of the engine, and the pressure Greater than a pressure in the combustion chamber. 2. The gas seal system of claim 1, wherein a gap between the turbine valve member and an outer surface of the rotary valve is about 10 0.0254 mm (1 mil). 3. The gas seal system of claim 1, wherein the compression member comprises a turbine valve injector member for injecting gas substantially tangentially into the turbine valve member. 4. The gas seal system of claim 3, comprising a position 15 inductor member for sensing a rotational position of a rotor of the rotary valve to send a signal to the compression member . 5. The gas seal system of claim 4, comprising a valve member for controlling the flow of compressed gas in the compression member into the turbine valve upon receipt of a signal from the inductor member 20 pieces of structure. 6. The gas seal system of claim 1, wherein the compression member comprises a compression chamber member. 7. The gas seal system of claim 1 wherein the compression member comprises a compressor member and the compressor member is driven by a 200928077 crankshaft of the rotary valve engine. 8. The gas seal system of claim 1 wherein the compression member comprises a crankcase of the engine and the crankcase is pressurized for intake and power travel of the engine. 5. The gas seal system of claim 8 wherein the crankcase includes a one-way valve member for allowing air to enter the crankcase as the compression and discharge strokes of the engine progress. 10. The gas seal system of claim 8 which includes a non-return valve member for causing compressed air in the crankcase 10 to enter the compression chamber member. A rotary valve engine comprising a gas seal as in claim 1 of the patent application. 12. The rotary valve engine of claim 11, wherein a rotor of the rotary valve is configured to be cooled by water passing through a hole in the rotor. 15 13. A method of placing a seal between a turn of a rotary valve and a turn of a combustion chamber in a rotary valve engine, the method comprising the steps of: a. preparing a gas passage a member forming a turbine valve member surrounding the combustion chamber bore; 20 b. forming a pressure in the gas passage member with the gas compression member, the pressure being greater during the compression stroke and the power stroke of the engine a pressure in the combustion chamber. 14. The method of claim 13, comprising substantially tangentially ejecting gas into the turbine valve member by a turbine valve injector member. The method of claim 13, comprising sensing a rotational position of a rotor of the rotary valve by an inductor member to signal a compression member. 16. The method of claim 14, comprising controlling compressed gas in the compression member to enter the turbine valve injector member when receiving a signal from the 5 inductor member. 17. The method of claim 13 wherein the step of forming a pressure in the gas passage member comprises forming a pressure in a compression chamber member. The method of claim 13, wherein forming a pressure in the gas passage member comprises forming a pressure by a compressor member driven by a crank shaft of the rotary valve engine. 19. The method of claim 13 wherein forming a pressure in the gas passage member comprises pressurizing 15 air in a crankcase of the engine by an intake and power stroke of the engine. 20. The method of claim 19, wherein the pressurized air in the crankcase is included in a compression and discharge stroke of the engine, allowing air to pass through a one-way valve member into the crankcase. 21. The method of claim 17, wherein the step of forming a pressure in the gas passage member 20 comprises causing compressed air in the crankcase to enter the compression chamber member through a pneumatic tube member and a check valve member. .
TW097138693A 2007-10-12 2008-10-08 Seal for a rotary valve for an internal combustion engine TW200928077A (en)

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GB0720009A GB2453593A (en) 2007-10-12 2007-10-12 Turbo valve gas seal system for i.c. engine rotary valve

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
TWI826412B (en) * 2018-09-06 2023-12-21 英商Rcv引擎有限公司 A spark ignition rotary valve internal combustion engine

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ITMI20112396A1 (en) * 2011-12-27 2013-06-28 Nuovo Pignone Spa ROTARY VALVES WITH CLOSING PROFILES BETWEEN STATOR AND ROTOR AND RELATED METHODS
US20140158080A1 (en) * 2012-07-11 2014-06-12 C. Budd Bayliff Rotary Exhaust Valve
ITBZ20130006A1 (en) * 2013-02-07 2014-08-08 Dissertori Kg Sas A FLUID MOTOR AND A MODIFICATION KIT TO REALIZE THIS ENGINE.
US9222405B2 (en) * 2013-07-08 2015-12-29 Massachusetts Institute Of Technology Turbocharged single cylinder internal combustion engine using an air capacitor
ITUB20155684A1 (en) * 2015-10-30 2017-04-30 Leonardo Mangiaracina SUCTION AND DISCHARGE GAS DISTRIBUTION SYSTEM FOR ALTERNATIVE COMBUSTION INTERNAL MOTORS VIA A ROTATING SHAFT.
US10947847B2 (en) * 2018-06-16 2021-03-16 Anton Giger Engine crank and connecting rod mechanism

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR632631A (en) * 1928-01-12
DE678953C (en) * 1935-06-20 1939-07-26 Argus Motoren Ges M B H Seal for internal combustion engines with a rotating slide or a slide swinging around its central axis in the form of a ball
US2354305A (en) * 1941-09-18 1944-07-25 Cross Roland Claude Rotary valve controlled internal-combustion engine
US2387973A (en) * 1942-06-25 1945-10-30 Aspin Frank Metealf Internal-combustion engine
US2730089A (en) * 1952-06-04 1956-01-10 Louis O French Rotary valve internal combustion engine
DE3132831A1 (en) * 1980-08-21 1982-04-29 Richard Davidson 60093 Winnetka Ill. Harza Rotary valve and sealing for this
US4606309A (en) * 1982-07-27 1986-08-19 Elf France Device for controlling the combustion chambers exhaust and/or intake for internal combustion engines
DE3540441A1 (en) * 1985-11-14 1987-05-21 Ficht Gmbh INTERNAL COMBUSTION ENGINE WITH A ROTATING SHUT-OFF ORGAN FOR CONTROLLING THE GAS EXCHANGE
FR2621648B1 (en) * 1987-10-07 1993-03-05 Inst Francais Du Petrole TWO-STROKE ENGINE WITH PNEUMATIC INJECTION AND EXHAUST FLOW RESTRICTION
FR2674906A1 (en) * 1991-04-03 1992-10-09 Inst Francais Du Petrole TWO-STROKE ENGINE WITH SELECTIVE CONTROL OF THE LOAD INTRODUCED INTO THE COMBUSTION CHAMBER.
DE69316661T2 (en) * 1992-11-06 1998-06-18 A E Bishop Research Pty DEVICE FOR GAS SEALING FOR ROTARY VALVES
US5546908A (en) * 1994-01-07 1996-08-20 Stokes; Richard A. Plural fuel system for internal combustion engine
US5503130A (en) * 1994-11-10 1996-04-02 Pomeisl; James R. Internal combustion engine with improved exhaust valve, timing system, and injector
AUPN559395A0 (en) * 1995-09-22 1995-10-19 Smith, Brian Rotary valve for an internal combustion engine
US5967108A (en) * 1996-09-11 1999-10-19 Kutlucinar; Iskender Rotary valve system
AUPO770797A0 (en) * 1997-07-04 1997-07-31 Smith, Brian Rotary valve for internal combustion engines
US6513475B2 (en) * 2001-04-18 2003-02-04 Barry Muth Rotary valve internal combustion engine
GB0130903D0 (en) * 2001-12-22 2002-02-13 Kingsley Windham Bevan Charles Improvements in and relating to cylinder heads
DE10257046A1 (en) * 2002-12-06 2004-06-24 Christoph Conradty Rotary valve seal
AU2003243828A1 (en) * 2003-07-11 2005-01-28 The Ramsey Valve Company Pty Ltd Rotary valve for i.c. engines
JP2008511777A (en) * 2004-09-01 2008-04-17 ビショップ イノヴェーション リミテッド Rotary valve gas and oil seals
WO2007013406A1 (en) * 2005-07-25 2007-02-01 Kabushiki Kaisha Toyota Jidoshokki Piston type compressor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
TWI826412B (en) * 2018-09-06 2023-12-21 英商Rcv引擎有限公司 A spark ignition rotary valve internal combustion engine

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MX2010003996A (en) 2010-09-14
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