TWI810042B - rotary engine - Google Patents
rotary engine Download PDFInfo
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- TWI810042B TWI810042B TW111132541A TW111132541A TWI810042B TW I810042 B TWI810042 B TW I810042B TW 111132541 A TW111132541 A TW 111132541A TW 111132541 A TW111132541 A TW 111132541A TW I810042 B TWI810042 B TW I810042B
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- rocker arm
- groove
- frame body
- stator
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- 230000017525 heat dissipation Effects 0.000 claims description 16
- 230000002093 peripheral effect Effects 0.000 claims description 9
- 238000007789 sealing Methods 0.000 claims description 6
- 230000000149 penetrating effect Effects 0.000 claims description 3
- 239000007788 liquid Substances 0.000 claims description 2
- 238000009434 installation Methods 0.000 claims 1
- 239000003921 oil Substances 0.000 description 70
- 238000001816 cooling Methods 0.000 description 10
- 230000000694 effects Effects 0.000 description 9
- 239000010687 lubricating oil Substances 0.000 description 9
- 230000006835 compression Effects 0.000 description 4
- 238000007906 compression Methods 0.000 description 4
- 238000004880 explosion Methods 0.000 description 4
- 239000000446 fuel Substances 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000003247 decreasing effect Effects 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008450 motivation Effects 0.000 description 1
Classifications
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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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- Valve-Gear Or Valve Arrangements (AREA)
- Valve Device For Special Equipments (AREA)
Abstract
一種旋轉式引擎,包含一包括一第一定子及一第二定子的定子單元、一包括一轉子件及一心軸的轉子單元、複數導引槽單元及複數汽動單元,該第一定子具有一第一軌跡槽,該第二定子具有一第二軌跡槽,每一導引槽單元包括一活塞孔、一形成於該第一定子且連通該活塞孔的第一溝槽,及一形成於該第二定子且連通該活塞孔的第二溝槽,每一汽動單元包括一能沿各自的該活塞孔移動的活塞件、一連接該活塞件並分別穿入該第一軌跡槽及該第二軌跡槽的軌跡桿,及一設置於該活塞孔的汽缸組,使該轉子件能夠受到多個汽動單元同時提供動力,而能讓該心軸能提供更大的動力。A rotary engine comprising a stator unit including a first stator and a second stator, a rotor unit including a rotor piece and a shaft, a plurality of guide slot units and a plurality of aerodynamic units, the first stator There is a first track groove, the second stator has a second track groove, each guide groove unit includes a piston hole, a first groove formed in the first stator and communicating with the piston hole, and a The second groove formed on the second stator and communicating with the piston hole, each aerodynamic unit includes a piston piece that can move along the respective piston hole, a piston piece connected to the piston piece and respectively penetrated into the first track groove and The track rod of the second track groove and a cylinder group arranged in the piston hole enable the rotor to be powered by multiple pneumatic units at the same time, so that the spindle can provide greater power.
Description
本發明是有關於一種引擎,特別是指一種旋轉式引擎。 The present invention relates to an engine, in particular to a rotary engine.
一種現有的引擎,是透過吸入混合燃料、壓縮混合燃料、點燃混合燃料及排放廢氣的四個步驟來完成輸出動力的過程,此過程通常會使用一汽缸、一活塞及一曲柄軸間的相互配合進行運作,藉由***混合燃料所產生的能量驅使該活塞移動,並帶動該曲柄軸轉動,進而使該活塞往復動作,而該曲柄軸的轉動時的能量就能帶動一輸出元件(例如車輪)運作,由於多種機械裝置都需要引擎作為動力源,因此各種形式的引擎仍在持續開發中。 An existing engine that completes the process of outputting power through four steps: intake of mixed fuel, compression of mixed fuel, ignition of mixed fuel and exhaust gas. This process usually uses the mutual cooperation between a cylinder, a piston and a crankshaft To operate, the piston is moved by the energy generated by the explosive mixed fuel, and the crankshaft is driven to rotate, thereby causing the piston to reciprocate, and the energy of the crankshaft rotation can drive an output element (such as a wheel) Since various mechanical devices require an engine as a power source, various forms of engines are still being developed.
因此,本發明的目的,即在提供一種旋轉式引擎。 Therefore, the object of the present invention is to provide a rotary engine.
於是,本發明旋轉式引擎,包含一定子單元、一轉子單元、複數導引槽單元,及複數汽動單元。 Therefore, the rotary engine of the present invention includes a stator unit, a rotor unit, a plurality of guide slot units, and a plurality of aerodynamic units.
該定子單元包括相對設置的一第一定子及一第二定子, 該第一定子具有一第一架體、一沿一軸線貫穿該第一架體的第一軸孔,及一形成於該第一架體對應該第二定子的一側並環繞該第一軸孔的第一軌跡槽,該第二定子具有一第二架體、一沿該軸線貫穿該第二架體的第二軸孔,及一形成於該第二架體對應該第一定子的一側並對應該第一軌跡槽的第二軌跡槽。 The stator unit includes a first stator and a second stator oppositely arranged, The first stator has a first frame body, a first shaft hole passing through the first frame body along an axis, and a first frame body formed on one side of the first frame body corresponding to the second stator and surrounding the first frame body. The first track groove of the shaft hole, the second stator has a second frame body, a second shaft hole passing through the second frame body along the axis, and a second frame body formed on the second frame body corresponding to the first stator One side of and corresponds to the second track groove of the first track groove.
該轉子單元包括一位於該第一架體及該第二架體間並能繞該軸線轉動的轉子件,及一沿該軸線穿設於該轉子件且兩端分別穿過該第一軸孔及該第二軸孔並能相對該第一架體及該第二架體轉動的心軸,該轉子件具有一朝向該第一架體的第一表面、一朝向該第二架體的第二表面,及一連接該第一表面及該第二表面並環繞該軸線的環繞面。 The rotor unit includes a rotor part located between the first frame body and the second frame body and capable of rotating around the axis, and a rotor part passing through the rotor part along the axis and passing through the first shaft hole at both ends respectively and the second shaft hole and can rotate relative to the first frame body and the second frame body. The rotor member has a first surface facing the first frame body and a first surface facing the second frame body. Two surfaces, and a surrounding surface connecting the first surface and the second surface and surrounding the axis.
該等導引槽單元繞該軸線形成於該轉子單元,每一導引槽單元包括一形成於該環繞面的活塞孔、一形成於該第一表面且連通該活塞孔的第一溝槽,及一形成於該第二表面且連通該活塞孔的第二溝槽。 The guide groove units are formed on the rotor unit around the axis, each guide groove unit includes a piston hole formed on the surrounding surface, a first groove formed on the first surface and communicating with the piston hole, and a second groove formed on the second surface and communicating with the piston hole.
每一汽動單元包括一能沿各自的該活塞孔移動的活塞件、一連接該活塞件並穿出各自的該第一溝槽及各自的該第二溝槽以使兩端分別穿入該第一軌跡槽及該第二軌跡槽的軌跡桿,及一設置於該活塞孔的汽缸組,該活塞件沿該活塞孔的延伸方向往復移動時,該軌跡桿沿該第一溝槽、該第二溝槽、該第一軌跡槽及該第二 軌跡槽移動而帶動該轉子件及該心軸轉動。 Each pneumatic unit includes a piston member that can move along the respective piston holes, a piston member that is connected to the piston member and passes through the respective first grooves and the respective second grooves so that both ends can respectively pass through the first grooves. A track groove and a track rod of the second track groove, and a cylinder group arranged in the piston hole, when the piston part reciprocates along the extending direction of the piston hole, the track bar moves two grooves, the first track groove and the second The track groove moves to drive the rotor and the spindle to rotate.
本發明的功效在於:藉由設置該第一定子、該第二定子、該轉子件、該等活塞孔及該等汽動單元,使該轉子件能夠受到多個汽動單元同時提供動力,而能讓該心軸能提供更大的動力。 The effect of the present invention is: by arranging the first stator, the second stator, the rotor, the piston holes and the pneumatic units, the rotor can be simultaneously powered by multiple pneumatic units, And the mandrel can be allowed to provide greater power.
2:定子單元 2: Stator unit
21:第一定子 21: The first stator
211:第一架體 211: The first frame body
212:第一軸孔 212: The first shaft hole
213:第一軌跡槽 213: The first track slot
214:第一環槽 214: The first ring groove
215:第一氣孔 215: The first air hole
216:第一油封孔 216: The first oil seal hole
217:第一內油封槽 217: The first inner oil seal groove
218:第一觸發架 218: First Trigger Rack
22:第二定子 22: Second stator
221:第二架體 221: The second frame
222:第二軸孔 222: Second shaft hole
223:第二軌跡槽 223: Second track slot
224:第二環槽 224: Second ring groove
225:第二氣孔 225:Second stomata
226:第二油封孔 226: Second oil seal hole
227:第二內油封槽 227: Second inner oil seal groove
228:第二觸發架 228: The second trigger frame
23:固定架 23: fixed frame
24:觸發電極 24: Trigger electrode
25:第一進油孔 25: The first oil inlet hole
26:第一洩油孔 26: The first drain hole
27:第二進油孔 27: Second oil inlet hole
28:第二洩油孔 28: Second drain hole
3:轉子單元 3: Rotor unit
31:轉子件 31: rotor parts
311:第一表面 311: first surface
312:第二表面 312: second surface
313:環繞面 313: surround surface
32:心軸 32: mandrel
321:氣槽 321: air tank
33:第一內環壁 33: The first inner ring wall
34:第一外環壁 34: The first outer ring wall
341:第一外油封槽 341: The first outer oil seal groove
35:第二內環壁 35: Second inner ring wall
36:第二外環壁 36: Second outer ring wall
361:第二外油封槽 361: Second outer oil seal groove
4:密封單元 4: sealed unit
41:第一加油罐 41: The first refueling tank
42:第二加油罐 42: The second refueling tank
43:第一外油封件 43: The first outer oil seal
44:第二外油封件 44: Second outer oil seal
45:第一內油封件 45: The first inner oil seal
46:第二內油封件 46: Second inner oil seal
5:導引槽單元 5: Guide groove unit
51:活塞孔 51: Piston hole
52:第一溝槽 52: The first groove
53:第二溝槽 53: Second groove
54:第一導孔 54: The first guide hole
55:第二導孔 55: Second guide hole
6:汽動單元 6:Pneumatic unit
61:活塞件 61:Piston parts
611:基壁 611: base wall
612:第一圍壁 612: The first wall
613:油孔 613: oil hole
614:安裝桿 614: Mounting rod
615:第二圍壁 615: Second wall
616:連接桿 616: connecting rod
62:軌跡桿 62:Track stick
63:汽缸組 63: cylinder bank
631:汽缸頭件 631: cylinder head
632:進氣閥門 632: intake valve
633:進氣汽門桿 633: intake valve lever
634:排氣閥門 634: exhaust valve
635:排氣汽門桿 635:Exhaust valve stem
636:火星塞 636: spark plug
637:進氣管道 637:Intake pipe
638:排氣管道 638: exhaust pipe
64:進氣彈簧 64: intake spring
65:排氣彈簧 65:Exhaust spring
66:進氣搖臂 66:Intake rocker arm
661:進氣搖臂觸發段 661: Intake rocker arm trigger section
662:進氣搖臂樞接段 662: Pivot section of intake rocker arm
663:進氣搖臂連動段 663: Intake rocker arm linkage section
67:排氣搖臂 67:Exhaust rocker arm
671:排氣搖臂觸發段 671: Exhaust rocker arm trigger section
672:排氣搖臂樞接段 672: Pivot section of exhaust rocker arm
673:排氣搖臂連動段 673: Exhaust rocker arm linkage section
7:滑接單元 7: Slide unit
71:第一滾珠孔 71: The first ball hole
72:第一滾珠 72: The first ball
73:第一滑接片 73: The first sliding piece
74:第二滾珠孔 74: Second ball hole
75:第二滾珠 75: The second ball
76:第二滑接片 76: The second sliding piece
8:散熱單元 8: cooling unit
81:第一散熱鰭片 81: The first cooling fin
82:散熱管 82: heat pipe
83:第二散熱鰭片 83: Second cooling fin
84:導風葉片 84:Guide vane
L:軸線 L: axis
R:運轉方向 R: running direction
S:滑動路線 S: sliding route
本發明的其他的特徵及功效,將於參照圖式的實施方式中清楚地呈現,其中:圖1是本發明旋轉式引擎的一第一實施例的一前視圖;圖2是該第一實施例的一前視分解圖;圖3是該第一實施例的一第一定子的一右視圖;圖4是該第一實施例的該第一定子的一左視圖;圖5是該第一實施例的一第二定子的一右視圖;圖6是該第一實施例的該第二定子的一左視圖;圖7是該第一實施例的一轉子單元及四汽動單元的一右視圖;圖8是該第一實施例的該轉子單元及該等汽動單元的一左視圖;圖9是該第一實施例的一剖視圖;圖10是該第一實施例的一使用示意圖,說明運轉的第一階段;圖11是沿圖10中直線XI-XI所取得的示意圖; 圖12是一類似於圖10的視圖,說明運轉的第二階段;圖13是沿圖12中直線XIII-XIII所取得的示意圖;圖14是一類似於圖12的視圖,說明運轉的第三階段;圖15是沿圖14中直線XV-XV所取得的示意圖;圖16是一類似於圖14的視圖,說明運轉的第四階段;圖17是沿圖16中直線XVII-XVII所取得的示意圖;圖18是本發明旋轉式引擎的一第二實施例的一剖視圖;圖19是本發明旋轉式引擎的一第三實施例的一前視分解圖;圖20是該第三實施例的一第二定子的一左視圖;圖21是本發明旋轉式引擎的一第四實施例的一轉子單元及四汽動單元的右視圖;及圖22是圖21的一局部放大圖。 Other features and effects of the present invention will be clearly presented in the embodiments with reference to the drawings, wherein: Fig. 1 is a front view of a first embodiment of the rotary engine of the present invention; Fig. 2 is the first embodiment A front exploded view of an example; Fig. 3 is a right view of a first stator of the first embodiment; Fig. 4 is a left view of the first stator of the first embodiment; Fig. 5 is a view of the first stator of the first embodiment A right view of a second stator of the first embodiment; Figure 6 is a left view of the second stator of the first embodiment; Figure 7 is a rotor unit and four pneumatic units of the first embodiment A right side view; Fig. 8 is a left side view of the rotor unit and the pneumatic units of the first embodiment; Fig. 9 is a sectional view of the first embodiment; Fig. 10 is a use of the first embodiment A schematic diagram illustrating the first stage of operation; Figure 11 is a schematic diagram taken along the line XI-XI in Figure 10; Fig. 12 is a view similar to Fig. 10, illustrating the second stage of operation; Fig. 13 is a schematic view taken along line XIII-XIII in Fig. 12; Fig. 14 is a view similar to Fig. 12, illustrating the third stage of operation stage; Fig. 15 is a schematic view taken along line XV-XV in Fig. 14; Fig. 16 is a view similar to Fig. 14, illustrating the fourth stage of operation; Fig. 17 is taken along line XVII-XVII in Fig. 16 Schematic diagram; Figure 18 is a cross-sectional view of a second embodiment of the rotary engine of the present invention; Figure 19 is a front exploded view of a third embodiment of the rotary engine of the present invention; Figure 20 is the third embodiment of the present invention A left side view of a second stator; FIG. 21 is a right side view of a rotor unit and four pneumatic units of a fourth embodiment of the rotary engine of the present invention; and FIG. 22 is a partially enlarged view of FIG. 21 .
在本發明被詳細描述之前,應當注意在以下的說明內容中,類似的元件是以相同的編號來表示。 Before the present invention is described in detail, it should be noted that in the following description, similar elements are denoted by the same numerals.
參閱圖1、2、3,本發明旋轉式引擎的一第一實施例,包含一定子單元2、一轉子單元3、一密封單元4、四導引槽單元5(見圖7)、四汽動單元6、一滑接單元7,及一散熱單元8。 Referring to Fig. 1, 2, 3, a first embodiment of the rotary engine of the present invention comprises a stator unit 2, a rotor unit 3, a sealing unit 4, four guide groove units 5 (see Fig. 7), four steam A moving unit 6, a sliding joint unit 7, and a cooling unit 8.
參閱圖2、4、5,該定子單元2包括相對設置的一第一定 子21及一第二定子22、一固定架23、一設置於該固定架23的觸發電極24、設置於該第一定子21的一第一進油孔25及一第一洩油孔26,及設置於該第二定子22的一第二進油孔27及一第二洩油孔28。 Referring to Fig. 2, 4, 5, the stator unit 2 includes a first fixed Sub 21 and a second stator 22, a fixed frame 23, a trigger electrode 24 arranged on the fixed frame 23, a first oil inlet hole 25 and a first oil drain hole 26 arranged on the first stator 21 , and a second oil inlet hole 27 and a second oil drain hole 28 disposed on the second stator 22 .
參閱圖2、3、4,該第一定子21具有一固定於該固定架23的第一架體211、一沿一軸線L貫穿該第一架體211的第一軸孔212、一形成於該第一架體211對應該第二定子22的一側並環繞該第一軸孔212的第一軌跡槽213、一形成於該第一架體211並環繞該第一軌跡槽213的第一環槽214、八橫向地貫穿該第一架體211並連通該第一環槽214的第一氣孔215、一形成於該第一架體211的外周面並連通該第一環槽214的第一油封孔216、一形成於該第一架體211且連通於該第一環槽214內側的第一內油封槽217,及一設置於該第一架體211的第一觸發架218。 2, 3, 4, the first stator 21 has a first frame body 211 fixed on the fixed frame 23, a first shaft hole 212 passing through the first frame body 211 along an axis L, and a formed On the side of the first frame body 211 corresponding to the second stator 22 and surrounding the first axis hole 212, a first track groove 213, a first track groove 213 formed on the first frame body 211 and surrounding the first track groove 213 An annular groove 214, eight first air holes 215 transversely passing through the first frame body 211 and communicating with the first annular groove 214, one formed on the outer peripheral surface of the first frame body 211 and communicating with the first annular groove 214 The first oil seal hole 216 , a first inner oil seal groove 217 formed on the first frame body 211 and connected to the inner side of the first annular groove 214 , and a first trigger frame 218 disposed on the first frame body 211 .
參閱圖4、5、6,該第二定子22具有一固定於該固定架23的第二架體221、一沿該軸線L貫穿該第二架體221的第二軸孔222、一形成於該第二架體221對應該第一定子21的一側並對應該第一軌跡槽213的第二軌跡槽223、一形成於該第二架體221並環繞該第二軌跡槽223的第二環槽224、八橫向地貫穿該第二架體221並連通該第二環槽224的第二氣孔225、一形成於該第二架體221的外周面並連通該第二環槽224的第二油封孔226、一形成於該第二架體221且連通於該第二環槽224內側的第二內油封槽227,及一 設置於該第二架體221並與該第一觸發架218繞該軸線L間隔設置的第二觸發架228。 4, 5, 6, the second stator 22 has a second frame body 221 fixed on the fixed frame 23, a second shaft hole 222 passing through the second frame body 221 along the axis L, and a second shaft hole 222 formed in the The second frame body 221 corresponds to one side of the first stator 21 and corresponds to the second track groove 223 of the first track groove 213 , a first track groove 223 formed on the second frame body 221 and surrounding the second track groove 223 Two ring grooves 224, eight second air holes 225 transversely penetrating through the second frame body 221 and communicating with the second ring groove 224, one formed on the outer peripheral surface of the second frame body 221 and communicating with the second ring groove 224 The second oil seal hole 226, a second inner oil seal groove 227 formed on the second frame body 221 and connected to the inner side of the second annular groove 224, and a The second trigger frame 228 is disposed on the second frame body 221 and spaced apart from the first trigger frame 218 around the axis L. As shown in FIG.
參閱圖2、4、5,該第一進油孔25貫穿該第一架體211、該第一洩油孔26貫穿該第一架體211且相對該第一進油孔25遠離該軸線L、該第二進油孔27貫穿該第二架體221,該第二洩油孔28貫穿該第二架體221且相對該第二進油孔27遠離該軸線L。 2, 4, 5, the first oil inlet hole 25 runs through the first frame body 211, the first oil drain hole 26 runs through the first frame body 211 and is away from the axis L relative to the first oil inlet hole 25. . The second oil inlet hole 27 runs through the second frame body 221 , and the second oil drain hole 28 runs through the second frame body 221 and is away from the axis L relative to the second oil inlet hole 27 .
參閱圖7、8、9,該轉子單元3包括一位於該第一架體211及該第二架體221間並能繞該軸線L轉動的轉子件31、一沿該軸線L穿設於該轉子件31且兩端分別穿過該第一軸孔212及該第二軸孔222並能相對該第一架體211及該第二架體221轉動的心軸32、一連接該轉子件31並環繞該軸線L的第一內環壁33、一連接該轉子件31並環繞該第一內環壁33的第一外環壁34、一連接該轉子件31並環繞該軸線L的第二內環壁35,及一連接該轉子件31並環繞該第二內環壁35的第二外環壁36。 Referring to Figures 7, 8 and 9, the rotor unit 3 includes a rotor member 31 located between the first frame body 211 and the second frame body 221 and capable of rotating around the axis L, a The rotor part 31 and the two ends respectively pass through the first shaft hole 212 and the second shaft hole 222 and can rotate relative to the first frame body 211 and the second frame body 221. A mandrel 32 connected to the rotor part 31 A first inner ring wall 33 that surrounds the axis L, a first outer ring wall 34 that connects the rotor member 31 and surrounds the first inner ring wall 33, a second outer ring wall 34 that connects the rotor member 31 and surrounds the axis L An inner ring wall 35 , and a second outer ring wall 36 connected to the rotor element 31 and surrounding the second inner ring wall 35 .
該轉子件31具有一朝向該第一架體211的第一表面311、一朝向該第二架體221的第二表面312,及一連接該第一表面311及該第二表面312並環繞該軸線L的環繞面313。該第一內環壁33及該第一外環壁34連接於該轉子件31的該第一表面311,該第二內環壁35及該第二外環壁36連接於該轉子件31的該第二表面312。 The rotor member 31 has a first surface 311 facing the first frame body 211, a second surface 312 facing the second frame body 221, and a connection connecting the first surface 311 and the second surface 312 and surrounding the Surrounding surface 313 of axis L. The first inner ring wall 33 and the first outer ring wall 34 are connected to the first surface 311 of the rotor member 31, and the second inner ring wall 35 and the second outer ring wall 36 are connected to the rotor member 31. The second surface 312 .
該心軸32具有四繞該軸線L呈角度間隔設置於外表面且 沿該軸線L的延伸方向延伸的氣槽321。 The mandrel 32 has four outer surfaces arranged at angular intervals around the axis L and The air groove 321 extends along the direction in which the axis L extends.
該第一外環壁34具有二間隔設置於外周面的第一外油封槽341,該第二外環壁36具有二間隔設置於外周面的第二外油封槽361。 The first outer ring wall 34 has two first outer oil seal grooves 341 disposed at intervals on the outer peripheral surface, and the second outer ring wall 36 has two second outer oil seal grooves 361 disposed at intervals on the outer peripheral surface.
該密封單元4包括一設置於該第一油封孔216的第一加油罐41、一設置於該第二油封孔226的第二加油罐42、二分別設置於該等第一外油封槽341的第一外油封件43、二分別設置於該等第二外油封槽361的第二外油封件44,一設置於該第一內油封槽217的第一內油封件45,及一設置於該第二內油封槽227的第二內油封件46,該第一油封孔216相反該第一加油罐41的開口對應於該等第一外油封件43間,該第二油封孔226相反該第二加油罐42的開口對應於該等第二外油封件44間。 The sealing unit 4 includes a first oil tank 41 set in the first oil seal hole 216, a second oil tank 42 set in the second oil seal hole 226, and two oil tanks 42 set in the first outer oil seal grooves respectively. The first outer oil seal 43 of 341, two second outer oil seals 44 respectively arranged in the second outer oil seal grooves 361, one first inner oil seal 45 arranged in the first inner oil seal groove 217, and one set In the second inner oil seal member 46 of the second inner oil seal groove 227, the opening of the first oil seal hole 216 opposite to the first refueling tank 41 corresponds to the space between the first outer oil seal members 43, and the second oil seal hole 226 On the contrary, the opening of the second oil tank 42 corresponds to the space between the second outer oil seals 44 .
該等導引槽單元5繞該軸線L形成於該轉子單元3,每一導引槽單元5包括一形成於該轉子件31的該環繞面313的活塞孔51、一形成於該第一表面311且連通該活塞孔51的第一溝槽52、一形成於該第二表面312且連通該活塞孔51的第二溝槽53、一形成於該第一表面311且對應於該第一環槽214並連通各自的該活塞孔51的第一導孔54,及一形成於該第二表面312且對應於該第二環槽224並連通該活塞孔51的第二導孔55。 The guide groove units 5 are formed on the rotor unit 3 around the axis L, and each guide groove unit 5 includes a piston hole 51 formed on the surrounding surface 313 of the rotor member 31, a piston hole formed on the first surface 311 and connected to the first groove 52 of the piston hole 51, a second groove 53 formed on the second surface 312 and connected to the piston hole 51, a second groove 53 formed on the first surface 311 and corresponding to the first ring The groove 214 communicates with the respective first guide hole 54 of the piston hole 51 and a second guide hole 55 formed on the second surface 312 corresponding to the second ring groove 224 and communicated with the piston hole 51 .
每一活塞孔51自該轉子件31的該環繞面313沿一滑動路 線S向內延伸,該滑動路線S與該軸線L相交。於本實施例中,該等導引槽單元5繞該軸線L呈等角度間隔形成於該轉子單元3,該等活塞孔51相互連通,且連通該心軸32的該等氣槽321。 Each piston hole 51 is along a sliding path from the surrounding surface 313 of the rotor member 31 A line S extends inwards, the sliding path S intersecting the axis L. In this embodiment, the guide groove units 5 are formed on the rotor unit 3 at equal angular intervals around the axis L, and the piston holes 51 communicate with each other and communicate with the air grooves 321 of the spindle 32 .
參閱圖3、7,該第一進油孔25沿垂直該軸線L的方向相對位於每一第一溝槽52的範圍內,參閱圖6、8,該第二進油孔27沿垂直該軸線L的方向相對位於每一第二溝槽53的範圍內。 Referring to Figures 3 and 7, the first oil inlet hole 25 is relatively located within the scope of each first groove 52 along the direction perpendicular to the axis L, referring to Figures 6 and 8, the second oil inlet hole 27 is located along the direction perpendicular to the axis L The direction L is relatively within the range of each second groove 53 .
參閱圖7、8、9,該等第一導孔54位於該第一內環壁33及該第一外環壁34間,該等第二導孔55位於該第二內環壁35及該第二外環壁36間。 7, 8, 9, the first guide holes 54 are located between the first inner ring wall 33 and the first outer ring wall 34, and the second guide holes 55 are located between the second inner ring wall 35 and the first outer ring wall 34. There are 36 rooms on the second outer ring wall.
每一汽動單元6包括一能沿該活塞孔51移動的活塞件61、一連接該活塞件61並穿出該第一溝槽52及該第二溝槽53以使兩端分別穿入該第一軌跡槽213及該第二軌跡槽223的軌跡桿62、一設置於該活塞孔51的汽缸組63、設置於該汽缸組63的一進氣彈簧64及一排氣彈簧65、一進氣搖臂(intake drag lever)66,及一排氣搖臂(exhaust drag lever)67。 Each pneumatic unit 6 includes a piston part 61 that can move along the piston hole 51, a piston part 61 connected to the piston part 61 and passing through the first groove 52 and the second groove 53 so that the two ends are respectively inserted into the first groove 53. A track groove 213 and the track rod 62 of the second track groove 223, a cylinder group 63 arranged on the piston hole 51, an intake spring 64 and an exhaust spring 65 arranged on the cylinder group 63, an intake spring Rocker arm (intake drag lever) 66, and an exhaust rocker arm (exhaust drag lever) 67.
每一活塞件61具有一基壁611、一自該基壁611外周緣沿該滑動路線S的方向向內延伸並供各自的該軌跡桿62穿設的第一圍壁612,及複數呈角度間隔設置於該第一圍壁612的油孔613。該活塞件61沿該活塞孔51的延伸方向往復移動時,該軌跡桿62沿該第一溝槽52、該第二溝槽53、該第一軌跡槽213及該第二軌跡槽223 移動而帶動該轉子件31及該心軸32轉動。 Each piston member 61 has a base wall 611, a first surrounding wall 612 extending inwardly from the outer periphery of the base wall 611 along the direction of the sliding path S and for the respective track rods 62 to pass through, and a plurality of angled The oil holes 613 are disposed at intervals in the first surrounding wall 612 . When the piston member 61 reciprocates along the extending direction of the piston hole 51 , the track bar 62 moves along the first groove 52 , the second groove 53 , the first track groove 213 and the second track groove 223 . The movement drives the rotor member 31 and the spindle 32 to rotate.
每一汽缸組63具有一設置於各自的該活塞孔51且位於各自的該活塞件61外側的汽缸頭件631、一位於該汽缸頭件631及該活塞件61間的進氣閥門(intake valve)632、一連動該進氣閥門632並穿出該汽缸頭件631的進氣汽門桿633、一位於該汽缸頭件631及該活塞件61間且間隔該進氣閥門632設置的排氣閥門(exhaust valve)634、一連動該排氣閥門634並穿出該汽缸頭件631的排氣汽門桿635、一設置於該汽缸頭件631並延伸入該汽缸頭件631及該活塞件61間的火星塞636、一形成於該汽缸頭件631且兩相反端分別對應各自的該第一導孔54及各自的該進氣閥門632的進氣管道637,及一形成於該汽缸頭件631且兩相反端分別對應各自的該第二導孔55及各自的該排氣閥門634的排氣管道638,每一活塞件61的該基壁611與各自的該汽缸頭件631的相對表面對應設置,以使該活塞件61靠近該汽缸頭件631時,兩者之間的空隙能減至最小。於本實施例中,該等汽缸組63及該等活塞孔51繞該軸線L同心設置。 Each cylinder group 63 has a cylinder head 631 that is arranged on the respective piston holes 51 and is positioned outside the respective piston 61, and an intake valve (intake valve) between the cylinder head 631 and the piston 61. ) 632, an intake valve rod 633 that moves the intake valve 632 and passes through the cylinder head piece 631, an exhaust valve that is located between the cylinder head piece 631 and the piston piece 61 and is set at an interval of the intake valve 632 A valve (exhaust valve) 634, an exhaust valve stem 635 that moves the exhaust valve 634 and passes through the cylinder head piece 631, an exhaust valve rod 635 that is arranged on the cylinder head piece 631 and extends into the cylinder head piece 631 and the piston piece A spark plug 636 between 61, an intake pipe 637 formed on the cylinder head 631 and two opposite ends respectively corresponding to the respective first guide holes 54 and the respective intake valves 632, and an intake pipe 637 formed on the cylinder head 631 and the two opposite ends respectively correspond to the second guide hole 55 and the exhaust pipe 638 of the exhaust valve 634 respectively. The base wall 611 of each piston 61 is opposite to the cylinder head 631. The surfaces are arranged correspondingly so that when the piston member 61 is close to the cylinder head member 631, the gap between the two can be minimized. In this embodiment, the cylinder groups 63 and the piston holes 51 are arranged concentrically around the axis L. As shown in FIG.
每一進氣彈簧64設置於各自的該進氣閥門632及各自的該汽缸頭件631間以使該進氣閥門632未受力時恆抵於該汽缸頭件631而封閉各自的該進氣管道637,每一排氣彈簧65設置於各自的該排氣閥門634及該汽缸頭件631間以使該排氣閥門634未受力時 恆抵於該汽缸頭件631而封閉各自的該排氣管道638。 Each intake spring 64 is arranged between the respective intake valve 632 and the respective cylinder head 631 so that the intake valve 632 is constantly pressed against the cylinder head 631 when the intake valve 632 is not stressed to close the respective intake valves. Pipeline 637, each exhaust spring 65 is arranged between the exhaust valve 634 and the cylinder head 631 so that when the exhaust valve 634 is not stressed Constantly reach the cylinder head 631 to close the respective exhaust pipes 638 .
該進氣搖臂66具有一進氣搖臂觸發段661、一連接該進氣搖臂觸發段661且樞設於該轉子件31的進氣搖臂樞接段662,及一連接該進氣搖臂樞接段662相反該進氣搖臂觸發段661的一側且連動各自的該進氣汽門桿633的進氣搖臂連動段663,該排氣搖臂67具有一排氣搖臂觸發段671、一連接該排氣搖臂觸發段671且樞設於該轉子件31的排氣搖臂樞接段672,及一連接該排氣搖臂樞接段672相反該排氣搖臂觸發段671的一側且連動各自的該排氣汽門桿635的排氣搖臂連動段673。 The intake rocker arm 66 has an intake rocker arm trigger section 661, an intake rocker arm pivot section 662 connected to the intake rocker arm trigger section 661 and pivotally arranged on the rotor member 31, and an intake rocker arm pivot section 662 connected to the intake rocker arm trigger section 661. The pivoting section 662 of the rocker arm is on the opposite side of the triggering section 661 of the intake rocker arm and links the respective intake rocker arm linkage section 663 of the intake valve lever 633. The exhaust rocker arm 67 has an exhaust rocker arm A trigger section 671, an exhaust rocker arm pivot section 672 connected to the exhaust rocker arm trigger section 671 and pivotally arranged on the rotor member 31, and a exhaust rocker arm pivot section 672 connected to the exhaust rocker arm One side of the trigger section 671 is linked with the respective exhaust rocker arm linkage section 673 of the exhaust valve lever 635 .
參閱圖4、5、9,該觸發電極24自該轉子件31的該環繞面313外側朝該環繞面313延伸,該觸發電極24、該第一觸發架218及該第二觸發架228繞該軸線L間隔設置,該轉子件31轉動而使任一火星塞636通過並接觸該觸發電極24時,對應的該火星塞636會通電而點火。 4, 5, 9, the trigger electrode 24 extends from the outer side of the surrounding surface 313 of the rotor member 31 toward the surrounding surface 313, the trigger electrode 24, the first trigger frame 218 and the second trigger frame 228 surround the The axes L are arranged at intervals. When the rotor member 31 rotates so that any spark plug 636 passes and touches the trigger electrode 24 , the corresponding spark plug 636 will be energized and ignited.
該轉子件31轉動而使任一進氣搖臂觸發段661通過該第一觸發架218時,對應的該進氣搖臂觸發段661會受壓而連動使對應的該進氣汽門桿633帶動對應的該進氣閥門632克服該進氣彈簧64的彈力而脫離對應的該汽缸頭件631。 When the rotor member 31 rotates so that any intake rocker arm trigger section 661 passes through the first trigger frame 218, the corresponding intake rocker arm trigger section 661 will be pressed and linked to make the corresponding intake valve lever 633 Drive the corresponding intake valve 632 to overcome the elastic force of the intake spring 64 and separate from the corresponding cylinder head 631 .
該轉子件31轉動而使任一排氣搖臂觸發段671通過該第二觸發架228時,對應的該排氣搖臂觸發段671會受壓而連動使對 應的該排氣汽門桿635帶動對應的該排氣閥門634克服該排氣彈簧65的彈力而脫離對應的該汽缸頭件631。 When the rotor member 31 rotates so that any exhaust rocker arm trigger section 671 passes through the second trigger frame 228, the corresponding exhaust rocker arm trigger section 671 will be pressurized and linked to make the pair The corresponding exhaust valve rod 635 drives the corresponding exhaust valve 634 to overcome the elastic force of the exhaust spring 65 and separate from the corresponding cylinder head 631 .
參閱圖2、4、5,該滑接單元7包括複數形成於該第一架體211且呈角度間隔設置於該第一環槽214及該第一軌跡槽213間的第一滾珠孔71、複數分別設置於該等第一滾珠孔71的第一滾珠72、一位於該等第一滾珠72內側並環繞該心軸32的第一滑接片73、複數形成於該第二架體221且呈角度間隔設置於該第二環槽224及該第二軌跡槽223間的第二滾珠孔74、複數分別設置於該等第二滾珠孔74的第二滾珠75,及一位於該等第二滾珠75內側並環繞該心軸32的第二滑接片76。於本實施例中,該等第一滾珠72分別凸出該等第一滾珠孔71的長度為0.1mm,該等第二滾珠75分別凸出該等第二滾珠孔74的長度為0.1mm,該第一滑接片73及該第二滑接片76的厚度為0.1mm。 Referring to Figures 2, 4, and 5, the sliding joint unit 7 includes a plurality of first ball holes 71 formed on the first frame body 211 and arranged at angular intervals between the first ring groove 214 and the first track groove 213, A plurality of first balls 72 respectively disposed in the first ball holes 71, a first sliding piece 73 located inside the first balls 72 and surrounding the spindle 32, a plurality formed in the second frame body 221 and The second ball holes 74 arranged at angular intervals between the second ring groove 224 and the second track groove 223, a plurality of second balls 75 respectively arranged in the second ball holes 74, and a second The ball 75 is inside and surrounds the second sliding piece 76 of the spindle 32 . In this embodiment, the length of the first balls 72 protruding from the first ball holes 71 is 0.1 mm, and the length of the second balls 75 protruding from the second ball holes 74 is 0.1 mm. The first sliding piece 73 and the second sliding piece 76 have a thickness of 0.1 mm.
參閱圖2、3、6,該散熱單元8包括複數設置於該第一架體211的第一散熱鰭片81、一設置於該第二架體221並用於通入液體的散熱管82、複數設置於該轉子件31的該環繞面313的第二散熱鰭片83,及複數繞該軸線L設置於該等第二散熱鰭片83的導風葉片84,該轉子件31轉動時,能連動使該等導風葉片84轉動以將外部空氣導引至該等第二散熱鰭片83進行散熱。 2, 3, 6, the heat dissipation unit 8 includes a plurality of first heat dissipation fins 81 arranged on the first frame 211, a heat dissipation pipe 82 arranged on the second frame 221 and used for feeding liquid, a plurality of The second cooling fins 83 arranged on the surrounding surface 313 of the rotor member 31, and the plurality of wind guide vanes 84 arranged on the second cooling fins 83 around the axis L, when the rotor member 31 rotates, they can move in unison. The wind guide vanes 84 are rotated to guide the external air to the second heat dissipation fins 83 for heat dissipation.
參閱圖2、9、10,使用時,該轉子件31及該心軸32能相 對該第一定子21、該第二定子22及該固定架23以一運轉方向R轉動,該第一觸發架218、該觸發電極24及該第二觸發架228是沿著該運轉方向R依序設置,且為了保持平衡,該等汽動單元6及該等導引槽單元5是繞該軸線L成等角度間隔設置。為了方便說明,以下以其中一汽動單元6及所對應的其中一導引槽單元5進行說明運轉的四個階段。 Referring to Fig. 2, 9, 10, during use, the rotor member 31 and the mandrel 32 can The first stator 21, the second stator 22 and the fixed frame 23 are rotated in a running direction R, and the first trigger frame 218, the trigger electrode 24 and the second trigger frame 228 are along the running direction R Arranged in sequence, and in order to maintain balance, the aerodynamic units 6 and the guide groove units 5 are arranged at equal angular intervals around the axis L. For the convenience of description, one of the pneumatic units 6 and one of the corresponding guide groove units 5 are used to illustrate the four stages of operation.
參閱圖9、10、11,於第一階段中,當該轉子件31轉動至使該汽缸組63的該進氣搖臂觸發段661接觸該第一觸發架218時,該進氣搖臂66克服該進氣彈簧64的彈力,而連動使該進氣閥門632脫離該汽缸頭件631,使該活塞件61跟該汽缸頭件631之間的空間透過該進氣管道637連通該第一導孔54、該第一環槽214及該等第一氣孔215,此時該活塞件61朝遠離該汽缸頭件631的方向移動,而將外部的一混合油氣自該等第一氣孔215外側吸入該汽缸頭件631及該活塞件61之間。 9, 10, 11, in the first stage, when the rotor member 31 rotates to make the intake rocker arm trigger section 661 of the cylinder group 63 contact the first trigger frame 218, the intake rocker arm 66 Overcoming the elastic force of the intake spring 64, the intake valve 632 is separated from the cylinder head piece 631 in interlocking motion, so that the space between the piston piece 61 and the cylinder head piece 631 communicates with the first guide through the intake pipe 637. Hole 54, the first annular groove 214 and the first air holes 215. At this time, the piston member 61 moves away from the cylinder head member 631, and an external mixed oil gas is sucked from the outside of the first air holes 215. Between the cylinder head 631 and the piston 61 .
參閱圖9、12、13,於第二階段中,接著該轉子件31繼續轉動而使該進氣搖臂觸發段661脫離該第一觸發架218,該進氣彈簧64的彈力會推抵使該進氣閥門632抵靠於該汽缸頭件631而使該進氣管道637封閉,此時該活塞件61朝鄰近該汽缸頭件631的方向移動,進而壓縮該混合油氣。 Referring to Figures 9, 12, and 13, in the second stage, the rotor member 31 continues to rotate to make the intake rocker arm trigger section 661 disengage from the first trigger frame 218, and the elastic force of the intake spring 64 will push against the The intake valve 632 abuts against the cylinder head 631 to close the intake pipe 637 , and at this time the piston 61 moves toward the direction adjacent to the cylinder head 631 , thereby compressing the mixed oil and gas.
參閱圖9、14、15,於第三階段中,而當該轉子件31繼 續轉動至使該火星塞636接觸該觸發電極24時,該火星塞636產生的火花能點燃壓縮後的該混合油氣,***時的能量就能推抵使該活塞件61朝遠離該汽缸頭件631的方向移動。 Referring to Fig. 9,14,15, in the third stage, when the rotor part 31 continues Continue to rotate until the spark plug 636 contacts the trigger electrode 24, the spark generated by the spark plug 636 can ignite the compressed gas mixture, and the energy of the explosion can push the piston 61 away from the cylinder head Move in the direction of 631.
參閱圖9、16、17,於第四階段中,接著該轉子件31繼續轉動至使該汽缸組63的該排氣搖臂觸發段671接觸該第二觸發架228,該排氣搖臂67克服該排氣彈簧65的彈力,而連動使該排氣閥門634脫離該汽缸頭件631,使該活塞件61跟該汽缸頭件631之間的空間透過該排氣管道638連通該第二導孔55、該第二環槽224及該等第二氣孔225,此時該活塞件61朝鄰近該汽缸頭件631的方向移動,而將***後的廢氣推入該排氣管道638而自該等第二氣孔225排出。接著即可再從第一階段開始循環重複。 9, 16, 17, in the fourth stage, then the rotor member 31 continues to rotate until the trigger section 671 of the exhaust rocker arm of the cylinder group 63 contacts the second trigger frame 228, and the exhaust rocker arm 67 Overcoming the elastic force of the exhaust spring 65, the exhaust valve 634 is separated from the cylinder head piece 631 in interlocking motion, so that the space between the piston piece 61 and the cylinder head piece 631 communicates with the second guide through the exhaust pipe 638. Holes 55, the second annular groove 224 and the second air holes 225. At this time, the piston member 61 moves toward the direction adjacent to the cylinder head member 631, and the exhaust gas after the explosion is pushed into the exhaust pipe 638 and released from the exhaust pipe 638. Wait until the second air hole 225 is discharged. Then you can repeat the cycle from the first stage.
由於***時所產生的能量能夠驅使該活塞件61藉由該軌跡桿62而順著該第一溝槽52及該第二溝槽53而朝遠離該汽缸頭件631的方向移動,此時該軌跡桿62也會順著該第一軌跡槽213及該第二軌跡槽223移動,就能推抵使該轉子件31連動該心軸32轉動,而該心軸32的轉動就能作為後續輸出的動力。 The energy generated during the explosion can drive the piston 61 to move away from the cylinder head 631 along the first groove 52 and the second groove 53 through the track rod 62. The track bar 62 will also move along the first track groove 213 and the second track groove 223, and can push against the rotor member 31 to drive the spindle 32 to rotate, and the rotation of the spindle 32 can be used as a subsequent output motivation.
參閱圖4、5、9,於本實施例中,該第一軌跡槽213及該第二軌跡槽223的軌跡,是於四個階段的整個過程中,讓該軌跡桿62連動該活塞件61能相對該汽缸頭件631往返兩次,並讓該轉子件31能夠轉動一圈。而四個汽動單元6及四個導引槽單元5的設計, 就能使該等汽動單元6輪流提供動力,使該心軸32的總動力達到單一汽動單元6的輸出動力的四倍。 Referring to Figures 4, 5 and 9, in this embodiment, the tracks of the first track groove 213 and the second track groove 223 are in the whole process of four stages, so that the track rod 62 is linked to the piston member 61 It can go back and forth twice relative to the cylinder head piece 631 and allow the rotor piece 31 to rotate once. And the design of four pneumatic units 6 and four guide groove units 5, Just can make these aerodynamic units 6 provide power in turn, make the total power of this mandrel 32 reach four times of the output power of single aerodynamic unit 6.
參閱圖2、4、5,此外,該定子單元2的該第一進油孔25及該第二進油孔27可用於注入潤滑油,參閱圖7、8、9,潤滑油能夠在該轉子件31轉動時通過該等第一溝槽52及該等第二溝槽53而流入該等活塞孔51內,並在受到轉動所產生的離心力時流入該等活塞件61內並通過該等油孔613流出,以使該等活塞件61能夠獲得潤滑,而流出的多餘的潤滑油可自該等活塞孔51再通過該等第一溝槽52及該等第二溝槽53流出,參閱圖4、5,最後通過該第一洩油孔26及該第二洩油孔28排出。 Referring to Fig. 2, 4, 5, in addition, the first oil inlet hole 25 and the second oil inlet hole 27 of the stator unit 2 can be used to inject lubricating oil, referring to Fig. 7, 8, 9, lubricating oil can be in the rotor When the member 31 rotates, it flows into the piston holes 51 through the first grooves 52 and the second grooves 53, and flows into the piston members 61 and passes through the oil when subjected to the centrifugal force generated by the rotation. The holes 613 flow out so that the pistons 61 can be lubricated, and the excess lubricating oil that flows out can flow out from the piston holes 51 through the first grooves 52 and the second grooves 53, see Fig. 4, 5, finally discharged through the first oil drain hole 26 and the second oil drain hole 28.
參閱圖4、5、9,該第一加油罐41及該第二加油灌42能夠分別將油通過該第一油封孔216及該第二油封孔226而注入該第一環槽214內的該等第一外油封件43之間及該第二環槽224內的該等第二外油封件44之間而能潤滑,配合該第一內油封件45及該第二內油封件46的設置,使內部的潤滑油不會經由該第一內環壁33及該第二內環壁35而洩漏,達到密封防漏的效果。 Referring to Figures 4, 5, and 9, the first oil tank 41 and the second oil tank 42 can inject oil into the first annular groove 214 through the first oil seal hole 216 and the second oil seal hole 226 respectively. Between the first outer oil seals 43 and between the second outer oil seals 44 in the second ring groove 224 can lubricate, cooperate with the first inner oil seal 45 and the second inner oil seal 46 It is arranged so that the internal lubricating oil will not leak through the first inner ring wall 33 and the second inner ring wall 35, so as to achieve the effect of sealing and anti-leakage.
因此,該旋轉式引擎就能達到以多個汽動單元6同時提供動力的功效,而能讓該心軸32能提供更大的動力。 Therefore, the rotary engine can achieve the effect of simultaneously providing power with multiple aerodynamic units 6 , so that the spindle 32 can provide greater power.
值得一提的是,該等汽動單元6及該等導引槽單元5的數量也可以視需要增加或減少,只要該第一軌跡槽213及該第二軌跡 槽223對應調整對應的軌跡,即便只有一個汽動單元6及一個導引槽單元5,也同樣能達到相同的功效。另外,本案實施例係以圓360度均分為四份,亦即各90度角作為引擎的四個行程來解釋及說明,但事實上卻是可以依照需要稍作調整,例如將第四階段的排氣行程調整為75度角,第二階段的壓縮行程縮減為80度角,則第一階段的吸氣行程即可增加為115度角,藉以增加吸氣飽足度,進而提高引擎高速運轉時的工作效率。 It is worth mentioning that the number of the pneumatic units 6 and the guide groove units 5 can also be increased or decreased as required, as long as the first track groove 213 and the second track The groove 223 adjusts the corresponding trajectory correspondingly, even if there is only one pneumatic unit 6 and one guide groove unit 5, the same effect can be achieved. In addition, the embodiment of this case is based on the fact that a circle of 360 degrees is divided into four parts, that is, each 90 degree angle is used as the four strokes of the engine to explain and illustrate, but in fact it can be slightly adjusted according to needs, for example, the fourth stage The exhaust stroke of the exhaust stroke is adjusted to 75 degrees, the compression stroke of the second stage is reduced to 80 degrees, and the suction stroke of the first stage can be increased to 115 degrees, so as to increase the fullness of the suction and improve the high speed of the engine. Efficiency during operation.
本案實施例的四個活塞孔51是由兩個貫通該轉子件31且垂直交叉的貫孔形成,且由該心軸32分隔出四個汽缸組63,每個汽缸組63所對應的該活塞件61的底部設有各自的該軌跡桿62,該軌跡桿62貫穿出該轉子件31兩側且***該第一定子21的該第一軌跡槽213及該第二定子22的該第二軌跡槽223,該軌跡桿62在穿出轉子件31兩側的部分安裝有滾針軸承,沿著既定的該第一軌跡槽213及該第二軌跡槽223移動,而該轉子件31兩側並設有該第一溝槽52及該第二溝槽53供該軌跡桿62作往復運動。 The four piston holes 51 of the embodiment of the present case are formed by two through holes passing through the rotor member 31 and vertically intersecting, and the spindle 32 separates four cylinder groups 63, and the corresponding pistons of each cylinder group 63 The bottom of the member 61 is provided with the track bar 62 respectively, and the track bar 62 passes through both sides of the rotor member 31 and is inserted into the first track slot 213 of the first stator 21 and the second track slot 213 of the second stator 22. The track groove 223, the track bar 62 is equipped with needle bearings on the part passing through the two sides of the rotor member 31, and moves along the predetermined first track groove 213 and the second track groove 223, while the two sides of the rotor member 31 The first groove 52 and the second groove 53 are provided for the reciprocating movement of the track rod 62 .
又本發明旋轉式引擎的每一活塞件61及對應的該軌跡桿62的上、下止點是由該第一軌跡槽213及該第二軌跡槽223控制,尤其是上止點依排氣與壓縮行程的不同而使該活塞件61及該軌跡桿62的位置不同;亦即本發明係利用該軌跡桿62在該第一軌跡槽213及該第二軌跡槽223內移動的位置來完成引擎吸氣、壓縮、爆 炸及排氣等四個行程。 The top and bottom dead centers of each piston member 61 of the rotary engine of the present invention and the corresponding track rod 62 are controlled by the first track groove 213 and the second track groove 223, especially the top dead center depends on the exhaust gas. The position of the piston member 61 and the track rod 62 is different due to the difference in the compression stroke; that is, the present invention utilizes the position where the track rod 62 moves in the first track groove 213 and the second track groove 223 to complete Engine suction, compression, explosion Four strokes including frying and exhausting.
參閱圖2,9,又本發明旋轉式引擎的散熱方式,除了設置該等第一散熱鰭片81、該等第二散熱鰭片83及該等導風葉片84,利用空氣冷卻外,並在該轉子件31與該第一定子21及該第二定子22間的間隙持續注入潤滑油,在離心力的作用下,潤滑油在該等活塞孔51內、外流動,達到機件潤滑及散熱的效果。 Referring to Fig. 2, 9, the heat dissipation mode of the rotary engine of the present invention, except that these first heat dissipation fins 81, these second heat dissipation fins 83 and these wind guide vanes 84 are arranged, utilize air cooling, and in The gap between the rotor part 31 and the first stator 21 and the second stator 22 is continuously injected with lubricating oil. Under the action of centrifugal force, the lubricating oil flows inside and outside the piston holes 51 to achieve lubrication and heat dissipation of the parts. Effect.
參閱圖7、8,9,又本發明旋轉式引擎的該轉子件31兩側表面上,在與該等汽缸組63的該等進氣管道637及該等排氣管道638相通的該等第一導孔54及該等第二導孔55的兩側,設置凸起的環狀壁,即該第一內環壁33、該第一外環壁34、該第二內環壁35及該第二外環壁36,當該等環壁***該第一定子21的該第一環槽214及該第二定子22的該第二環槽224,會形成供該旋轉式引擎進、排氣的氣室,以供該旋轉式引擎進、排氣用。 Referring to Fig. 7, 8, 9, on the surface of both sides of the rotor member 31 of the rotary engine of the present invention, on the first air ducts 637 and the exhaust air ducts 638 of the cylinder groups 63 communicate with each other. Both sides of a guide hole 54 and the second guide holes 55 are provided with raised annular walls, namely the first inner ring wall 33 , the first outer ring wall 34 , the second inner ring wall 35 and the second inner ring wall 35 . The second outer ring wall 36, when these ring walls are inserted into the first ring groove 214 of the first stator 21 and the second ring groove 224 of the second stator 22, will form an inlet and outlet for the rotary engine. Air chamber for the intake and exhaust of the rotary engine.
又本發明在該轉子件31內的該等活塞孔51的氣體相通,另在該心軸32上設有該等氣槽321,使該等活塞孔51的內部氣體可以與外界相通,以便隨時調節該等活塞孔51內因該等活塞件61移動產生的氣壓差異。 The gas of these piston holes 51 in the rotor member 31 of the present invention communicates, and these air grooves 321 are provided on the mandrel 32 in addition, so that the internal gas of these piston holes 51 can communicate with the outside world, so that at any time Adjust the air pressure difference in the piston holes 51 due to the movement of the piston parts 61 .
參閱圖3、6、9,又本發明旋轉式引擎在每一汽缸組63的該進氣閥門632及該排氣閥門634的開闔,係利用安裝在該轉子件31或該等汽缸頭件631上的對應的進氣、排氣搖臂66、67,依其 有無碰觸安置於該定子單元2外圓周凸起的該第一觸發架218及該第二觸發架228,進而有無壓迫對應的進氣彈簧64及排氣彈簧65的動作來控制進氣閥門632及排氣閥門634的開關。 Referring to Fig. 3, 6, 9, the opening and closing of the intake valve 632 and the exhaust valve 634 of the rotary engine of the present invention at each cylinder group 63 is to utilize the valve mounted on the rotor 31 or the cylinder heads. Corresponding intake air on 631, exhaust rocker arm 66,67, according to its Whether to touch the first trigger frame 218 and the second trigger frame 228 protruding from the outer circumference of the stator unit 2, and whether to press the corresponding intake spring 64 and exhaust spring 65 to control the intake valve 632 And the switch of exhaust valve 634.
又本發明旋轉式引擎因該導引槽單元5與該汽動單元6的各機件間具有潤滑油,致使相互摩擦損耗的能源極低,故能讓該旋轉式引擎發揮最大的動力。 The rotary engine of the present invention has lubricating oil between the parts of the guide groove unit 5 and the pneumatic unit 6, so that the energy lost by mutual friction is extremely low, so the rotary engine can exert maximum power.
參閱圖18,本發明的一第二實施例是類似於該第一實施例,其差異之處在於:每一活塞孔51自該轉子件31的該環繞面313沿該滑動路線S向內延伸,每一活塞件61具有一基壁611、一自該基壁611外周緣沿該滑動路線S的方向向內延伸的第一圍壁612、複數呈角度間隔設置於該第一圍壁612的油孔613、一連接該第一圍壁612的安裝桿614、一沿該滑動路線S的延伸方向間隔該第一圍壁612間隔設置並供各自的該軌跡桿62穿設的第二圍壁615,及一連接該安裝桿614及該軌跡桿62的連接桿616。 Referring to FIG. 18 , a second embodiment of the present invention is similar to the first embodiment, the difference is that each piston hole 51 extends inwardly from the surrounding surface 313 of the rotor member 31 along the sliding path S Each piston member 61 has a base wall 611, a first surrounding wall 612 extending inwardly from the outer periphery of the base wall 611 along the direction of the sliding path S, and a plurality of angular intervals arranged on the first surrounding wall 612 An oil hole 613, a mounting rod 614 connected to the first surrounding wall 612, a second surrounding wall spaced apart from the first surrounding wall 612 along the extending direction of the sliding route S and provided for the respective track rods 62 to pass through 615, and a connecting rod 616 connecting the mounting rod 614 and the track rod 62.
每一進氣搖臂樞接段662樞設於各自的該汽缸頭件631,每一排氣搖臂樞接段672樞設於各自的該汽缸頭件631。 Each intake rocker arm pivot section 662 is pivotally mounted on the respective cylinder head piece 631 , and each exhaust rocker arm pivot section 672 is pivotally mounted on the respective cylinder head piece 631 .
如此,該第二實施例也可達到與上述第一實施例相同的目的與功效,且多餘的潤滑油除了能自該等油孔613流出之外,也能夠透過每一活塞件61的該第一圍壁612及該第二圍壁615之間的 開放空間流出。 In this way, the second embodiment can also achieve the same purpose and effect as the above-mentioned first embodiment, and the excess lubricating oil can not only flow out from the oil holes 613, but also pass through the first lubricating oil of each piston member 61. Between a surrounding wall 612 and the second surrounding wall 615 Open space flows out.
參閱圖19、20,本發明的一第三實施例是類似於該第一實施例,其差異之處在於:該第一觸發架218可卸離地設置於該第一架體211,該第二觸發架228可卸離地設置於該第二架體221。 19 and 20, a third embodiment of the present invention is similar to the first embodiment, the difference is that: the first trigger frame 218 is detachably arranged on the first frame body 211, the first Two trigger frames 228 are detachably disposed on the second frame body 221 .
如此,該第三實施例也可達到與上述第一實施例相同的目的與功效。 In this way, the third embodiment can also achieve the same purpose and effect as the above-mentioned first embodiment.
參閱圖21、22,本發明的一第四實施例是類似於該第一實施例,其差異之處在於:每一活塞孔51自該轉子件31的該環繞面313沿各自的該滑動路線S向內延伸,每一滑動路線S與該軸線L不相交,每一活塞件61的基壁611與各自的該汽缸頭件631的相對表面對應設置。於本實施例中,每一活塞孔51的延伸範圍與該軸線L不相交,而偏離中心,使每一活塞件61移動時相對該軸線L所產生的力矩增加,進而提高角動量,而能在工業上有更廣的用途。 Referring to Fig. 21, 22, a fourth embodiment of the present invention is similar to this first embodiment, and its difference is: each piston hole 51 is along the respective sliding route from the surrounding surface 313 of the rotor member 31 S extends inward, each sliding path S does not intersect the axis L, and the base wall 611 of each piston member 61 is disposed correspondingly to the opposite surface of the respective cylinder head member 631 . In this embodiment, the extension range of each piston hole 51 does not intersect with the axis L, but deviates from the center, so that the torque generated relative to the axis L when each piston member 61 moves increases, thereby increasing the angular momentum, and can There are wider uses in industry.
如此,該第四實施例也可達到與上述第一實施例相同的目的與功效。 In this way, the fourth embodiment can also achieve the same purpose and effect as the above-mentioned first embodiment.
綜上所述,藉由設置該第一定子21、該第二定子22、該轉子件31、該等活塞孔51及該等汽動單元6,使該轉子件31能夠受到多個汽動單元6同時提供動力,而能讓該心軸32能提供更大的動 力,故確實能達成本發明的目的。 In summary, by setting the first stator 21, the second stator 22, the rotor member 31, the piston holes 51 and the pneumatic units 6, the rotor member 31 can be subjected to multiple pneumatic drives. Unit 6 provides power simultaneously, and can allow this mandrel 32 to provide greater dynamic Power, so can really reach the purpose of the present invention.
惟以上所述者,僅為本發明的實施例而已,當不能以此限定本發明實施的範圍,凡是依本發明申請專利範圍及專利說明書內容所作的簡單的等效變化與修飾,皆仍屬本發明專利涵蓋的範圍內。 But the above-mentioned ones are only embodiments of the present invention, and should not limit the scope of the present invention. All simple equivalent changes and modifications made according to the patent scope of the present invention and the content of the patent specification are still within the scope of the present invention. Within the scope covered by the patent of the present invention.
2:定子單元 2: Stator unit
21:第一定子 21: The first stator
22:第二定子 22: Second stator
23:固定架 23: fixed frame
24:觸發電極 24: Trigger electrode
3:轉子單元 3: Rotor unit
31:轉子件 31: rotor parts
313:環繞面 313: surround surface
32:心軸 32: mandrel
34:第一外環壁 34: The first outer ring wall
36:第二外環壁 36: Second outer ring wall
4:密封單元 4: sealed unit
41:第一加油罐 41: The first refueling tank
42:第二加油罐 42: The second refueling tank
43:第一外油封件 43: The first outer oil seal
44:第二外油封件 44: Second outer oil seal
6:汽動單元 6:Pneumatic unit
7:滑接單元 7: Slide unit
72:第一滾珠 72: The first ball
73:第一滑接片 73: The first sliding piece
75:第二滾珠 75: The second ball
76:第二滑接片 76: The second sliding piece
8:散熱單元 8: cooling unit
81:第一散熱鰭片 81: The first cooling fin
82:散熱管 82: heat pipe
83:第二散熱鰭片 83: Second cooling fin
84:導風葉片 84:Guide vane
Claims (17)
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TW111132541A TWI810042B (en) | 2022-08-29 | 2022-08-29 | rotary engine |
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TW111132541A TWI810042B (en) | 2022-08-29 | 2022-08-29 | rotary engine |
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TWI810042B true TWI810042B (en) | 2023-07-21 |
TW202409410A TW202409410A (en) | 2024-03-01 |
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Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4003338C2 (en) * | 1990-02-05 | 1992-04-30 | Straetling, Geb. Toelle, Hedwig, 4630 Bochum, De | |
WO2007075047A1 (en) * | 2005-12-27 | 2007-07-05 | Sung-Duck Kim | Rotary engine having piston |
CN101371006A (en) * | 2005-12-21 | 2009-02-18 | 德兹莫特克股份公司 | Engine with rotary piston |
KR20090055707A (en) * | 2007-11-29 | 2009-06-03 | 이용걸 | Century engine |
CN112031930A (en) * | 2020-09-07 | 2020-12-04 | 陕西新年动力科技有限公司 | Rotary engine based on track control |
-
2022
- 2022-08-29 TW TW111132541A patent/TWI810042B/en active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4003338C2 (en) * | 1990-02-05 | 1992-04-30 | Straetling, Geb. Toelle, Hedwig, 4630 Bochum, De | |
CN101371006A (en) * | 2005-12-21 | 2009-02-18 | 德兹莫特克股份公司 | Engine with rotary piston |
WO2007075047A1 (en) * | 2005-12-27 | 2007-07-05 | Sung-Duck Kim | Rotary engine having piston |
KR20090055707A (en) * | 2007-11-29 | 2009-06-03 | 이용걸 | Century engine |
CN112031930A (en) * | 2020-09-07 | 2020-12-04 | 陕西新年动力科技有限公司 | Rotary engine based on track control |
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