TWI579455B - Turbocharger dynamic system - Google Patents

Turbocharger dynamic system Download PDF

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Publication number
TWI579455B
TWI579455B TW104102965A TW104102965A TWI579455B TW I579455 B TWI579455 B TW I579455B TW 104102965 A TW104102965 A TW 104102965A TW 104102965 A TW104102965 A TW 104102965A TW I579455 B TWI579455 B TW I579455B
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Taiwan
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circumferential surface
rotor
inner circumferential
vortex
casing
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TW104102965A
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Chinese (zh)
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TW201627570A (en
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陳瑞峰
羅方廷
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陳瑞峰
羅方廷
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    • 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

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Description

渦流增壓動力系統 Eddy current booster power system

本發明提供一種渦流增壓動力系統，其是與車輛動力裝置的結構有關。 The present invention provides a vortex booster power system that is related to the structure of a vehicle powerplant.

按，一般車輛於出廠時即具有一定的動力輸出能量，而車輛的動力來源來自於引擎，引擎動力的產生主要是透過進氣端導入氣體進入引擎燃燒室與油氣混合進行燃燒，藉由燃燒***的爆發力推動活塞而產生驅動動力；因此，燃燒效率將直接影響後端的出力表現，越能驅近於完全燃燒也就能達到最佳的出力表現，而必須達到完全燃燒的空氣需求往往大於一般車輛輸入引擎燃燒室的氣體量；因此，市面上便有一種渦輪增壓系統，如圖1所示，該渦輪增壓系統10主要包含一汽缸11、一廢氣渦輪12以及一從動壓縮渦輪13，該汽缸11燃燒的廢氣由一排氣端111連通輸入該廢氣渦輪12驅動該廢氣渦輪12轉動，而該廢氣渦輪12再透過一從動軸121帶動該從動壓縮渦輪13轉動，而該從動壓縮渦輪13同時吸入新鮮空氣，該從動壓縮渦輪13吸入新鮮空氣並壓縮空氣後再將氣體送入該汽缸11的進氣端112，據此使汽缸11接收壓縮後的空氣進而提升燃燒效率；然而，由於該渦輪增壓系統10必須接收廢氣產生動力，又必須吸收新鮮空氣進行壓縮，因此無法由單一個渦輪達成，而必須配置一個廢氣渦輪12及一個從動壓縮渦輪13，如此導致整體渦輪增壓系統10具有一定的重量及體積，而會增加車輛的負載； 且就結構方面來說，由於該渦輪增壓系統10必須銜接於引擎的排氣端111及進氣端112之間，管線的配置及構件位置的配置都必須有專業知識的專業人員才能順利組裝於車輛內，一般使用者自行安裝的難度高，因此一般使用者欲安裝該渦輪增壓系統10就必須負擔整體結構成本以及專業人員的安裝服務成本，如此往往降低使用者的使用慾望，影響經濟效益；有鑑於此，本發明人潛心研究並更深入構思，歷經多次研發試作後，終於發明出一種渦流增壓動力系統。 According to the general vehicle, there is a certain power output energy when it leaves the factory. The power source of the vehicle comes from the engine. The engine power is mainly generated by introducing gas into the engine combustion chamber through the intake end to mix with the oil and gas for combustion. The explosive force pushes the piston to generate driving power; therefore, the combustion efficiency will directly affect the output performance of the back end, and the closer it is to the complete combustion, the best output performance can be achieved, and the demand for the complete combustion air must be greater than that of the general vehicle. The amount of gas input into the combustion chamber of the engine; therefore, there is a turbocharger system on the market, as shown in FIG. 1, the turbocharger system 10 mainly includes a cylinder 11, an exhaust turbine 12, and a driven compression turbine 13, The exhaust gas combusted by the cylinder 11 is connected to the exhaust end 111 to be driven to the exhaust turbine 12 to drive the exhaust turbine 12 to rotate, and the exhaust turbine 12 is further driven to rotate by the driven compression turbine 13 through a driven shaft 121, and the driven The compression turbine 13 simultaneously draws in fresh air, and the driven compression turbine 13 draws in fresh air and compresses the air before feeding the gas into the The intake end 112 of the cylinder 11 thereby causes the cylinder 11 to receive the compressed air to increase the combustion efficiency; however, since the turbocharger system 10 must receive the exhaust gas to generate power, it must absorb the fresh air for compression, and thus cannot be single A turbine is achieved, and an exhaust turbine 12 and a driven compression turbine 13 must be configured, thus resulting in a certain weight and volume of the overall turbocharger system 10, which increases the load of the vehicle; And in terms of structure, since the turbocharger system 10 must be connected between the exhaust end 111 and the intake end 112 of the engine, the configuration of the pipeline and the configuration of the component positions must be assembled by professionals with professional knowledge. In a vehicle, it is difficult for a general user to install it by himself. Therefore, a general user who wants to install the turbocharger system 10 must bear the overall structural cost and the installation service cost of the professional, which tends to reduce the user's desire to use and affect the economy. Benefits; In view of this, the inventors have devoted themselves to research and deeper conceiving, and after a number of research and development trials, finally invented a vortex supercharged power system.

本發明提供一種渦流增壓動力系統，其主要目的是改善一般渦輪增壓系統結構結構組態複雜、裝配難度高之缺失。 The invention provides a vortex supercharged power system, the main purpose of which is to improve the complexity of the structural structure of the general turbocharger system and the lack of assembly difficulty.

為達前述目的，本發明提供一種渦流增壓動力系統，包含：一進氣端；一殼體具有一外周面及一內周面，該外周面為兩端直徑相同之圓筒形，而該內周面相較於該外周面為斜面，該內周面圍繞界定出一圓錐形的容置空間，該內周面的兩端分別為一第一端及一第二端，該殼體以該第一端連通連接該進氣端；一轉子由一中軸的周緣呈輻射狀地發散間隔成形複數葉片，該轉子容置於該殼體的容置空間內，且連接該轉子的該中軸兩端的延伸方向定義為軸向X，而各該葉片具有相對的一葉片正面以及一葉片背面，各該葉片的葉片正面係面對相鄰的葉片的該葉片背面，且各該葉片分別以一連結側銜接於該中軸，相對該連結側為一外側，該連結側與該外側的兩端則再分別以一第一端側與一第二端側連結，且該第一端側於該連結側與該外側之間具有一第一端側長度，該第二端側於該連結側與該外側之間具有一第二端側長度，該第一端側長度大於該第二端側長度，該轉子容置於該殼體的容置空間內，並使該轉子的該 第一端側面對該內周面的第一端，而該第二端側則面對該殼體的內周面之第二端；一氣缸體，具有相連通的一燃燒室、一進氣口以及一排氣口，該氣缸體的進氣口連通連接該殼體的內周面之第二端。 To achieve the foregoing objective, the present invention provides a vortex booster power system including: an intake end; a housing having an outer peripheral surface and an inner peripheral surface, the outer peripheral surface being a cylindrical shape having the same diameter at both ends, and the outer peripheral surface The inner circumferential surface is a sloped surface, and the inner circumferential surface defines a conical housing space. The two ends of the inner circumferential surface are respectively a first end and a second end. a first end is connected to the inlet end; a rotor is radially dispersed by a peripheral edge of the central shaft to form a plurality of blades, the rotor is received in the accommodating space of the casing, and is connected to both ends of the central shaft of the rotor The extending direction is defined as an axial direction X, and each of the blades has an opposite blade front surface and a blade back surface, and the blade front surface of each of the blades faces the blade back surface of the adjacent blade, and each of the blades has a joint side Connecting to the central axis, the connecting side is an outer side, and the connecting side and the outer side are respectively connected by a first end side and a second end side, and the first end side is on the connecting side The outer side has a first end side length, The second end side has a second end side length between the connecting side and the outer side, the first end side length is greater than the second end side length, and the rotor is received in the accommodating space of the housing. And make the rotor The first end side faces the first end of the inner circumferential surface, and the second end side faces the second end of the inner circumferential surface of the casing; a cylinder block having a combustion chamber and an air inlet communicating And an air outlet, the air inlet of the cylinder block is connected to the second end of the inner circumferential surface of the casing.

本發明透過將主要用以壓縮氣體的轉子設置成為第一端側長度大於第二端側長度之態樣，據此使進氣壓力小於排氣壓力而達到壓縮氣體之目的，壓縮氣體再提供予氣缸體而能提高燃燒效率，優化末端出力狀況。 According to the present invention, the rotor mainly used for the compressed gas is disposed such that the length of the first end side is longer than the length of the second end side, whereby the intake pressure is smaller than the exhaust pressure to achieve the purpose of compressing the gas, and the compressed gas is supplied to the compressed gas. The cylinder block can improve combustion efficiency and optimize the end output.

《習知技術》 "Knowledge Technology"

10‧‧‧渦輪增壓系統 10‧‧‧ turbocharged system

11‧‧‧汽缸 11‧‧‧ cylinder

111‧‧‧排氣端 111‧‧‧Exhaust end

112‧‧‧進氣端 112‧‧‧ intake end

12‧‧‧廢氣渦輪 12‧‧‧Exhaust turbine

121‧‧‧從動軸 121‧‧‧ driven shaft

13‧‧‧從動壓縮渦輪 13‧‧‧ driven compression turbine

《本發明》 "this invention"

20‧‧‧進氣端 20‧‧‧ intake end

30‧‧‧空氣濾清器 30‧‧‧Air filter

40‧‧‧殼體 40‧‧‧shell

41‧‧‧外周面 41‧‧‧ outer perimeter

42‧‧‧內周面 42‧‧‧ inner circumference

421‧‧‧第一端 421‧‧‧ first end

422‧‧‧第二端 422‧‧‧ second end

423‧‧‧內螺紋段 423‧‧‧Threaded section

43‧‧‧容置空間 43‧‧‧ accommodating space

45‧‧‧間隔肋 45‧‧‧ spaced ribs

46‧‧‧承座 46‧‧‧ seat

461‧‧‧凹槽 461‧‧‧ Groove

50‧‧‧轉子 50‧‧‧Rotor

51‧‧‧中軸 51‧‧‧Axis

52‧‧‧葉片 52‧‧‧ blades

521‧‧‧葉片正面 521‧‧‧Front front

522‧‧‧葉片背面 522‧‧‧The back of the blade

523‧‧‧連結側 523‧‧‧ Link side

524‧‧‧外側 524‧‧‧ outside

525‧‧‧第一端側 525‧‧‧ first end side

526‧‧‧第二端側 526‧‧‧ second end side

53‧‧‧軸承 53‧‧‧ bearing

60‧‧‧蓋體 60‧‧‧ cover

61‧‧‧抵段 61‧‧‧ arrived

62‧‧‧組設段 62‧‧‧ Section

621‧‧‧外螺紋部 621‧‧‧External thread

63‧‧‧肩部 63‧‧‧ shoulder

64‧‧‧承座 64‧‧ ‧ socket

641‧‧‧凹槽 641‧‧‧ Groove

65‧‧‧止擋肋 65‧‧‧stop ribs

70‧‧‧節氣門 70‧‧‧ Throttle

80‧‧‧氣缸體 80‧‧‧Cylinder block

81‧‧‧燃燒室 81‧‧‧ combustion chamber

82‧‧‧進氣口 82‧‧‧air inlet

83‧‧‧排氣口 83‧‧‧Exhaust port

X‧‧‧軸向 X‧‧‧ axial

L1‧‧‧第一端側長度 L1‧‧‧First end length

L2‧‧‧第二端側長度 L2‧‧‧second end length

D1‧‧‧第一葉片端距 D1‧‧‧first blade end distance

D2‧‧‧第二葉片端距 D2‧‧‧second blade end distance

P1‧‧‧第一外端部 P1‧‧‧ first outer end

P2‧‧‧第二外端部 P2‧‧‧ second outer end

θ‧‧‧扭轉角 Θ‧‧‧twist angle

圖1 為習知渦輪增壓系統的示意圖。 Figure 1 is a schematic illustration of a conventional turbocharger system.

圖2 為本發明渦流增壓動力系統的渦流增壓組件之立體結構分解圖。 2 is a perspective exploded view of the vortex booster assembly of the vortex booster power system of the present invention.

圖3 為本發明渦流增壓動力系統中轉子之端視圖。 Figure 3 is an end view of the rotor of the vortex supercharged power system of the present invention.

圖4 為本發明渦流增壓動力系統中轉子之另一端視圖。 Figure 4 is a cross-sectional view of the rotor of the vortex supercharged power system of the present invention.

圖5 為本發明渦流增壓動力系統的渦流增壓組件之組合剖視圖。 Figure 5 is a cross-sectional view showing the combination of the vortex pressurizing assembly of the vortex supercharging power system of the present invention.

圖6 為本發明渦流增壓動力系統的系統圖。 Figure 6 is a system diagram of the vortex booster power system of the present invention.

為使貴審查委員對本發明之目的、特徵及功效能夠有更進一步之瞭解與認識，以下茲請配合【圖式簡單說明】詳述如後：本發明渦流增壓動力系統的較佳實施例如2至6所示，包含：一進氣端20；一空氣濾清器30，連通連接該進氣端20；一渦流增壓組件，一端連通連接該空氣濾清器30，該渦流增壓組件包含一殼體40、一轉子50以及一蓋體60，其中： 該殼體40為一端完全開放，一端局部開放之空心筒形結構並具有一外周面41及一內周面42，該外周面41為兩端直徑相同之圓筒形，而該內周面42相較於該外周面41為斜面，據此使該殼體40的該內周面42圍繞界定出一圓錐形的容置空間43，該內周面42的兩端分別為一第一端421及一第二端422，該殼體40的內周面42的第一端421完全連通該容置空間43，該殼體40的內周面42接鄰該第一端421設置一內螺紋段423，而該殼體40的內周面42的第二端422則再成形複數間隔肋45，各該間隔肋45匯集至該內周面42的中心位置的一承座46，該承座46面對該容置空間43的一面設置一凹槽461，該殼體40的內周面42的第二端422受各該間隔肋45的配置成為局部開放之形態；該殼體40以該第一端421連通連接該空氣濾清器30，並據此使該殼體40的該第一端421連通連接該進氣端20；該轉子50由一中軸51的周緣呈輻射狀地發散間隔成形複數葉片52，該中軸51的兩端分別穿套一軸承53，該轉子50容置於該殼體40的容置空間43內並使一端的軸承53容置於該凹槽641內，且連接該轉子50的該中軸51兩端的延伸方向定義為軸向X，而各該葉片52具有相對的一葉片正面521以及一葉片背面522，各該葉片52的葉片正面521係面對相鄰的葉片52的葉片背面522，且各該葉片52分別以一連結側523銜接於該中軸51，相對該連結側523為一外側524，該連結側523與該外側524的兩端則再分別以一第一端側525與一第二端側526連結，且該第一端側525於該連結側523與該外側524之間具有一第一端側長度L1，該第二端側526於該連結側523與該外側524之間具有一第二端側長度L2，該第一端側長度L1大於該第二端側長度L2，此外，該第一端側525與該外側524的銜接處為一第一外端部P1，而該第二端側526與該外側524的銜接處為一第二外端部P2，各該葉片52的第一外端部P1之間具有一第一葉片端距D1，而各該葉片52的第二外端部P2之間具有一第二葉片端距D2，該第一葉片端距D1大於該第二葉片端距D2； 另外，由該轉子50的兩端來看，各該葉片52的第一端側525與該第二端側526之間具有一扭轉角θ，該扭轉角θ為10°~180°之間，本實施例之扭轉角θ為75°，且該扭轉角θ亦可為45°、60°、90°、110°、130°、145°、160°；且該外側524相對於該軸向X為弧線；該轉子50容置於該殼體40的容置空間43內，並使該轉子50的該第一端側525面對該內周面42的第一端421，而該第二端側526則面對該殼體40的內周面42之第二端422；該蓋體60為空心環狀結構，且該蓋體60包含一抵段61銜接一組設段62，該組設段62具有外螺紋部621，而該抵段61的外徑大於該組設段62的外徑並於該抵段61與該組設段62的銜接處產生一肩部63，且該蓋體60由內周緣向中心匯集於一承座64銜接成形複數止擋肋65，該承座64上設置一凹槽641，且本實施例是等角間隔成形三個止擋肋65；該蓋體60以該組設段62穿組於該殼體40的該第一端41，並透過該蓋體60的組設段62之外螺紋部621螺接於該殼體40的內螺紋段423，使該蓋體60的抵段61之肩部63靠抵於該殼體40，且該蓋體60的凹槽641對應套覆該轉子50上的另一軸承53；該渦流增壓組件以該轉子50的第一端側525連通銜接該空氣濾清器30；一節氣門70，連通連接該渦流增壓組件的另一端，該節氣門70是連通銜接於轉子50的第二端側526；以及一氣缸體80，具有相連通的一燃燒室81、一進氣口82以及一排氣口83，該氣缸體80的進氣口82連通連接該節氣門70。 In order to enable the reviewing committee to have a better understanding and understanding of the purpose, features and functions of the present invention, the following is a detailed description of the following: a preferred embodiment of the vortex supercharged power system of the present invention is as follows: The air intake end 20 is connected to the air intake end 20; a housing 40, a rotor 50 and a cover 60, wherein: The housing 40 is a hollow cylindrical structure that is completely open at one end and partially open at one end and has an outer circumferential surface 41 and an inner circumferential surface 42. The outer circumferential surface 41 has a cylindrical shape with the same diameter at both ends, and the inner circumferential surface 42 The outer peripheral surface 41 is a beveled surface, and the inner peripheral surface 42 of the housing 40 defines a conical housing space 43. The two ends of the inner peripheral surface 42 are respectively a first end 421. And a second end 422, the first end 421 of the inner peripheral surface 42 of the housing 40 completely communicates with the accommodating space 43. The inner peripheral surface 42 of the housing 40 is adjacent to the first end 421 and is provided with an internal thread segment. 423, and the second end 422 of the inner circumferential surface 42 of the casing 40 is reshaped into a plurality of spacer ribs 45, and each of the spacer ribs 45 is collected to a socket 46 at a center position of the inner circumferential surface 42. The socket 46 A groove 461 is disposed on a surface of the accommodating space 43. The second end 422 of the inner circumferential surface 42 of the casing 40 is partially open by the arrangement of the ribs 45. The casing 40 is One end 421 is connected to the air cleaner 30, and the first end 421 of the housing 40 is connected to the intake end 20; the rotor 50 is sprung from the periphery of a central shaft 51. The plurality of blades 52 are formed in a spaced apart manner, and the two ends of the central shaft 51 are respectively sleeved with a bearing 53. The rotor 50 is received in the accommodating space 43 of the casing 40 and the bearing 53 at one end is received in the concave portion. The extending direction of the two ends of the central shaft 51 connecting the rotor 50 is defined as an axial direction X, and each of the blades 52 has an opposite blade front surface 521 and a blade back surface 522, and the blade front surface 521 of each of the blades 52 is The blade back surface 522 of the adjacent blade 52 is disposed, and each of the blades 52 is coupled to the center shaft 51 by a connecting side 523, and an outer side 524 is opposite to the connecting side 523. The connecting side 523 and the two ends of the outer side 524 Then, the first end side 525 is coupled to the second end side 526, and the first end side 525 has a first end side length L1 between the connecting side 523 and the outer side 524. The second end The side 526 has a second end side length L2 between the connecting side 523 and the outer side 524. The first end side length L1 is greater than the second end side length L2. Further, the first end side 525 and the outer side 524 The junction is a first outer end P1, and the junction of the second end side 526 and the outer side 524 is a The outer end portion P2 has a first blade end distance D1 between the first outer end portions P1 of the blades 52, and a second blade end distance D2 between the second outer end portions P2 of the blades 52, The first blade end distance D1 is greater than the second blade end distance D2; In addition, as seen from both ends of the rotor 50, the first end side 525 of the vane 52 and the second end side 526 have a twist angle θ between 10° and 180°. The torsion angle θ of the embodiment is 75°, and the torsion angle θ may also be 45°, 60°, 90°, 110°, 130°, 145°, 160°; and the outer side 524 is opposite to the axial direction X. An arc is disposed in the accommodating space 43 of the housing 40, and the first end side 525 of the rotor 50 faces the first end 421 of the inner peripheral surface 42 and the second end The side 526 faces the second end 422 of the inner peripheral surface 42 of the casing 40; the cover 60 has a hollow annular structure, and the cover 60 includes an abutment 61 that engages with a set of segments 62. The segment 62 has an externally threaded portion 621, and the outer diameter of the abutting portion 61 is larger than the outer diameter of the assembled portion 62 and a shoulder portion 63 is formed at the junction of the abutting portion 61 and the assembled portion 62, and the cover portion A plurality of retaining ribs 65 are formed by the inner peripheral edge toward the center of a socket 64. The retaining seat 64 is provided with a recess 641. In this embodiment, three retaining ribs 65 are formed at equal intervals; the cover body 60 is disposed in the housing 40 by the set of segments 62 The first end 41 is threaded to the internal thread section 423 of the housing 40 through the externally threaded portion 621 of the assembly section 62 of the cover 60, so that the shoulder 63 of the abutment 61 of the cover 60 abuts The housing 40 and the recess 641 of the cover 60 correspondingly cover another bearing 53 on the rotor 50; the vortex pressurizing assembly communicates with the air filter 30 via the first end side 525 of the rotor 50. a valve 70 connected to the other end of the vortex plenum assembly, the throttle 70 is connected to the second end side 526 of the rotor 50; and a cylinder block 80 having a combustion chamber 81 connected thereto The gas port 82 and an exhaust port 83, the intake port 82 of the cylinder block 80 are connected to the throttle valve 70.

以上為本發明渦流增壓動力系統的結構組態及特徵，運作時，該進氣端20進氣，氣體經由空氣濾清器30過濾後送入該渦流增壓組件，空氣由該渦流增壓組件的轉子50的第一端側525進入，且空氣是率先進入該渦流增壓組件的殼體40接觸轉子50的各葉片52推動該轉子50轉動，氣體由該轉子50的第一端 側525進入，氣體順沿各該葉片52流向第二端側526，而由於本發明之第一端側長度L1大於該第二端側長度L2，且第一葉片端距D1大於第二葉片端距D2，因此氣體由第一端側525之間進入轉子50的空間大於由第二端側526之間輸出轉子50的空間，亦即，進入該轉子50的第一端側525之間的壓力小於氣體由轉子50第二端側526之間輸出的壓力，據此有效提高氣體壓力，形成壓縮氣體並將壓縮氣體經由節氣門70送入氣缸體80，藉此提高該氣缸體80的燃燒效率，並更能提高出力能量；此外，本發明之渦流增壓組件的結構體積小、組態極為簡單，且只需要銜接於進氣端20與氣缸體80之間就能完成組裝，不需複雜或專業的管線連接，一般使用者便能自行組裝，因此能提高使用者的使用慾望，也能據此創造更高的經濟效益；且本發明將該轉子50容置於該殼體40內，該殼體40的外周面41為兩端直徑相同之圓筒形，據此，便於使用者組裝該渦流增壓組件；且本發明之殼體40的內周面42又設置為配合轉子50形態的態樣，據此搭配轉子50形態而能確保轉子50形態產生的氣體壓縮的效能；還有，由於本案將該轉子50的各該葉片52之外側524設置為弧線，且該第一端側525與該第二端側526之間又設置扭轉角θ，據此使氣體接觸葉片52推動該轉子50轉動時能更為順暢地流動，確保該轉子50壓縮氣體的效能；本發明透過簡單的結構裝配於氣缸體80與進氣端20之間，便能提供壓縮氣體予氣缸體80產生動力，除了組裝的便利性高、使用成本低之外，更能有效提高出力，顯著提升動力性能。 The above is the structural configuration and characteristics of the vortex supercharged power system of the present invention. In operation, the intake end 20 is inducted, and the gas is filtered through the air filter 30 and sent to the vortex booster assembly, and the air is pressurized by the vortex. The first end side 525 of the rotor 50 of the assembly enters, and the air is the first to enter the vortex plenum assembly 40. The blades 52 that contact the rotor 50 push the rotor 50 to rotate, the gas being passed from the first end of the rotor 50. The side 525 enters, the gas flows along the respective blades 52 to the second end side 526, and since the first end side length L1 of the present invention is greater than the second end side length L2, and the first blade end distance D1 is greater than the second blade end The distance D2, therefore, the space between the gas entering the rotor 50 between the first end sides 525 is greater than the space between the second end sides 526 for outputting the rotor 50, that is, the pressure entering the first end side 525 of the rotor 50. Less than the pressure of the gas outputted between the second end sides 526 of the rotor 50, thereby effectively increasing the gas pressure, forming a compressed gas and feeding the compressed gas to the cylinder block 80 via the throttle valve 70, thereby increasing the combustion efficiency of the cylinder block 80. Moreover, the eddy current pressurization assembly of the present invention has a small structure and a simple configuration, and only needs to be connected between the intake end 20 and the cylinder block 80 to complete the assembly without complicated. Or a professional pipeline connection, which can be assembled by a general user, thereby improving the user's desire to use, and thereby creating a higher economic benefit; and the present invention accommodates the rotor 50 in the housing 40, The outer peripheral surface 41 of the housing 40 is The cylindrical shape having the same end diameter, thereby facilitating the user to assemble the vortex pressure pressurizing assembly; and the inner circumferential surface 42 of the casing 40 of the present invention is further configured to match the shape of the rotor 50, thereby being matched with the rotor 50 form. The effectiveness of the compression of the gas generated by the rotor 50 can be ensured; furthermore, since the outer side 524 of the blade 52 of the rotor 50 is arranged as an arc, and between the first end side 525 and the second end side 526 Further, a twist angle θ is provided, whereby the gas contact vane 52 pushes the rotor 50 to flow more smoothly, ensuring the efficiency of the rotor 50 to compress the gas; the present invention is assembled to the cylinder block 80 and the intake end through a simple structure. Between 20, compressed gas can be supplied to the cylinder block 80 to generate power. In addition to high assembly convenience and low use cost, the output can be effectively improved and the power performance can be significantly improved.

40‧‧‧殼體 40‧‧‧shell

41‧‧‧外周面 41‧‧‧ outer perimeter

42‧‧‧內周面 42‧‧‧ inner circumference

421‧‧‧第一端 421‧‧‧ first end

422‧‧‧第二端 422‧‧‧ second end

423‧‧‧內螺紋段 423‧‧‧Threaded section

43‧‧‧容置空間 43‧‧‧ accommodating space

45‧‧‧間隔肋 45‧‧‧ spaced ribs

46‧‧‧承座 46‧‧‧ seat

461‧‧‧凹槽 461‧‧‧ Groove

50‧‧‧轉子 50‧‧‧Rotor

51‧‧‧中軸 51‧‧‧Axis

52‧‧‧葉片 52‧‧‧ blades

521‧‧‧葉片正面 521‧‧‧Front front

522‧‧‧葉片背面 522‧‧‧The back of the blade

523‧‧‧連結側 523‧‧‧ Link side

524‧‧‧外側 524‧‧‧ outside

525‧‧‧第一端側 525‧‧‧ first end side

526‧‧‧第二端側 526‧‧‧ second end side

60‧‧‧蓋體 60‧‧‧ cover

61‧‧‧抵段 61‧‧‧ arrived

62‧‧‧組設段 62‧‧‧ Section

621‧‧‧外螺紋部 621‧‧‧External thread

64‧‧‧承座 64‧‧ ‧ socket

641‧‧‧凹槽 641‧‧‧ Groove

65‧‧‧止擋肋 65‧‧‧stop ribs

X‧‧‧軸向 X‧‧‧ axial

Claims (9)

一種渦流增壓動力系統，包含：一進氣端；一殼體具有一外周面及一內周面，該外周面為兩端直徑相同之圓筒形，而該內周面相較於該外周面為斜面，該內周面圍繞界定出一圓錐形的容置空間，該內周面的兩端分別為一第一端及一第二端，該殼體以該第一端連通連接該進氣端；一轉子由一中軸的周緣呈輻射狀地發散間隔成形複數葉片，該轉子容置於該殼體的容置空間內，且連接該轉子的該中軸兩端的延伸方向定義為軸向，而各該葉片具有相對的一葉片正面以及一葉片背面，各該葉片的葉片正面係面對相鄰的葉片的該葉片背面，且各該葉片分別以一連結側銜接於該中軸，相對該連結側為一外側，該連結側與該外側的兩端則再分別以一第一端側與一第二端側連結，且該第一端側於該連結側與該外側之間具有一第一端側長度，該第二端側於該連結側與該外側之間具有一第二端側長度，該第一端側長度大於該第二端側長度，該轉子容置於該殼體的容置空間內，並使該轉子的該第一端側面對該內周面的第一端，而該第二端側則面對該殼體的內周面之第二端；一氣缸體，具有相連通的一燃燒室、一進氣口以及一排氣口，該氣缸體的進氣口連通連接該殼體的內周面之第二端；其中，該殼體的內周面的第一端完全連通該容置空間，該殼體的內周面接鄰該第一端設置一內螺紋段，而該殼體的內周面的第二端則再成形複數間隔肋，該殼體的內周面的第二端受各該間隔肋的配置成為局部開放之形態，而該殼體的第一端再組設一蓋體，該蓋體為空心環狀結構並具有外螺紋部，該蓋體以該外螺紋部螺接於該殼體的內螺紋段。 A vortex supercharged power system includes: an intake end; a casing having an outer circumferential surface and an inner circumferential surface, wherein the outer circumferential surface is a cylindrical shape having the same diameter at both ends, and the inner circumferential surface is opposite to the outer circumferential surface a slanting surface, the inner circumferential surface defines a conical housing space, the two ends of the inner circumferential surface are respectively a first end and a second end, and the housing is connected to the air inlet by the first end a rotor; a rotor is radially dispersed by a circumference of a central shaft to form a plurality of blades, the rotor is accommodated in the accommodating space of the casing, and an extending direction of the two ends of the central shaft connecting the rotor is defined as an axial direction, and Each of the blades has a first blade front surface and a blade back surface, and the blade front surface of each of the blades faces the blade back surface of the adjacent blade, and each of the blades is coupled to the central axis by a joint side, opposite to the joint side An outer side of the connecting side and the outer side are respectively connected by a first end side and a second end side, and the first end side has a first end between the connecting side and the outer side. Side length, the second end side is on the joint side and the Between the sides having a second end side length, the first end side length is greater than the second end side length, the rotor is received in the accommodating space of the housing, and the first end side of the rotor is opposite a first end of the inner circumferential surface, the second end side facing the second end of the inner circumferential surface of the casing; a cylinder block having a combustion chamber, an air inlet and an exhaust gas connected to each other The air inlet of the cylinder block is connected to the second end of the inner circumferential surface of the casing; wherein the first end of the inner circumferential surface of the casing completely communicates with the accommodating space, and the inner circumferential surface of the casing is connected Adjacent to the first end, an internal thread segment is disposed, and the second end of the inner circumferential surface of the casing is reshaped into a plurality of spaced ribs, and the second end of the inner circumferential surface of the casing is partially configured by each of the spaced ribs An open form, wherein the first end of the housing is further provided with a cover body, the cover body has a hollow annular structure and has an external thread portion, and the cover body is screwed to the internal thread of the housing by the external thread portion segment. 如申請專利範圍第1項所述的渦流增壓動力系統，其中，由該轉子的兩端來看，各該葉片的第一端側與該第二端側之間具有一扭轉角，該扭轉角為10°~180°之間。 The vortex supercharging power system of claim 1, wherein a twist angle is formed between the first end side and the second end side of each of the vanes as viewed from both ends of the rotor, the twist The angle is between 10° and 180°. 如申請專利範圍第2項所述的渦流增壓動力系統，其中，該扭轉角為75°。 The vortex supercharged power system of claim 2, wherein the torsion angle is 75°. 如申請專利範圍第1項所述的渦流增壓動力系統，其中，該轉子的各該葉片之外側相對於該軸向為弧線。 The vortex supercharged power system of claim 1, wherein the outer side of each of the blades of the rotor is curved with respect to the axial direction. 如申請專利範圍第1項所述的渦流增壓動力系統，其中，各該葉片的該第一端側與該外側的銜接處為一第一外端部，而該第二端側與該外側的銜接處為一第二外端部，各該葉片的第一外端部之間具有一第一葉片端距，而各該葉片的第二外端部之間具有一第二葉片端距，該第一葉片端距大於該第二葉片端距。 The vortex-charged power system of claim 1, wherein the first end side of the blade and the outer side are a first outer end, and the second end side and the outer side are The junction is a second outer end, each of the blades has a first blade end distance between the first outer ends, and a second blade end distance between the second outer ends of each of the blades. The first blade end distance is greater than the second blade end distance. 如申請專利範圍第1項所述的渦流增壓動力系統，其中，該蓋體包含一抵段銜接一組設段，該組設段具有該外螺紋部，而該抵段的外徑大於該組設段的外徑並於該抵段與該組設段的銜接處產生一肩部，該蓋體的該抵段之肩部靠抵於該殼體。 The vortex supercharged power system of claim 1, wherein the cover body comprises an abutting portion that engages a set of segments, the set segment has the externally threaded portion, and the outer diameter of the abutting portion is greater than the The outer diameter of the segment is set and a shoulder is formed at the junction of the abutting segment and the set segment, and the shoulder of the abutting portion of the cover abuts against the casing. 如申請專利範圍第1項所述的渦流增壓動力系統，其中，該轉子的該中軸的兩端分別穿套一軸承，該蓋體成形複數止擋肋，而該殼體的各該間隔肋以及蓋體的各該止擋肋分別匯集至一承座，且該承座面對該容置空間的一面上設置一凹槽，該轉子兩端的各該軸承容置於各該凹槽內。 The vortex supercharging power system of claim 1, wherein both ends of the central shaft of the rotor are respectively sleeved with a bearing, and the cover body forms a plurality of stop ribs, and the spacer ribs of the housing And the retaining ribs of the cover body are respectively assembled to a socket, and a recess is disposed on a side of the socket facing the accommodating space, and each of the bearings at both ends of the rotor is received in each of the recesses. 如申請專利範圍第1項所述的渦流增壓動力系統，其中，該進氣端與該殼體之間更連通設置一空氣濾清器。 The vortex supercharged power system of claim 1, wherein an air cleaner is disposed in communication between the intake end and the housing. 如申請專利範圍第1項所述的渦流增壓動力系統，其中，該殼體與該氣缸體之間更連通設置一節氣門。 The vortex supercharged power system of claim 1, wherein the casing and the cylinder block are further connected to each other to provide a throttle.
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Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102220883A (en) * 2010-04-19 2011-10-19 霍尼韦尔国际公司 Axial turbine wheel
CN102966402A (en) * 2012-11-12 2013-03-13 上海交通大学 System for synchronously adjusting lifts of intake valve and exhaust valve of supercharged engine
CN204060911U (en) * 2013-03-11 2014-12-31 伊顿公司 A kind of pressurization system for motor

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102220883A (en) * 2010-04-19 2011-10-19 霍尼韦尔国际公司 Axial turbine wheel
CN102966402A (en) * 2012-11-12 2013-03-13 上海交通大学 System for synchronously adjusting lifts of intake valve and exhaust valve of supercharged engine
CN204060911U (en) * 2013-03-11 2014-12-31 伊顿公司 A kind of pressurization system for motor

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