TWI673942B - Variable magnetoresistance flywheel - Google Patents
Variable magnetoresistance flywheel Download PDFInfo
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- TWI673942B TWI673942B TW107137364A TW107137364A TWI673942B TW I673942 B TWI673942 B TW I673942B TW 107137364 A TW107137364 A TW 107137364A TW 107137364 A TW107137364 A TW 107137364A TW I673942 B TWI673942 B TW I673942B
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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
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- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/16—Mechanical energy storage, e.g. flywheels or pressurised fluids
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Abstract
本發明係關於一種可變磁阻飛輪機構,設置於一具有一曲軸及安裝有 複數線圈定子之引擎總成上,包括:一飛輪外殼體、一飛輪內殼體及複數可動磁鐵總成。飛輪外殼體設置於曲軸上,飛輪內殼體設置於飛輪外殼體上並位於飛輪外殼體之內側,複數可動磁鐵總成設置於飛輪內殼體及飛輪外殼體之間並圍繞複數線圈定子,每一可動磁鐵總成包括有一磁鐵磁芯及一彈性構件,磁鐵磁芯藉由彈性構件之彈性力而朝向飛輪內殼體抵靠,並可自由移動於飛輪內殼體及飛輪外殼體之間。藉此,可動磁鐵總成可對應引擎轉速自動調整磁鐵磁芯與線圈定子之距離並調整發電量。 The present invention relates to a variable reluctance flywheel mechanism. The engine assembly of the plurality of coil stators includes a flywheel outer casing, a flywheel inner casing and a plurality of movable magnet assemblies. The flywheel outer casing is disposed on the crankshaft, the flywheel inner casing is disposed on the flywheel outer casing and is located inside the flywheel outer casing, and a plurality of movable magnet assemblies are disposed between the flywheel inner casing and the flywheel outer casing and surround a plurality of coil stators. Each movable magnet assembly includes a magnet core and an elastic member. The magnet core abuts against the inner shell of the flywheel by the elastic force of the elastic member, and can move freely between the inner shell of the flywheel and the outer shell of the flywheel. . Thereby, the movable magnet assembly can automatically adjust the distance between the magnet core and the coil stator and adjust the power generation amount according to the engine speed.
Description
本發明係關於一種可變磁阻飛輪機構,尤指一種利用可動磁鐵總成調整發電量之可變磁阻飛輪機構。 The present invention relates to a variable reluctance flywheel mechanism, and more particularly to a variable reluctance flywheel mechanism that uses a movable magnet assembly to adjust power generation.
現今常用之個人交通工具一般有汽車及機車,機車形式之交通工具為一種由引擎驅動,主要利用手把操縱方向的二輪、三輪或四輪等之車輛,由於有著操縱簡單、行動方便及價格低廉的特點,成為目前最常利用的交通工具。 Personal vehicles commonly used today include automobiles and locomotives. Locomotives are vehicles driven by engines that mainly use two, three, or four wheels to control the direction of the handlebar. They are simple to operate, easy to move, and inexpensive. Has become the most commonly used means of transportation.
一般來說,機車是利用設置於飛輪上之磁鐵及固鎖於引擎殼體上之線圈定子,在引擎運轉時同步帶動飛輪轉動,使飛輪上之磁鐵與線圈定子有固定的旋轉運動,飛輪旋轉切割了磁力線使磁力線對時間發生變化,就發生了交變的感應電勢在線圈導體中,因而產生電能。 Generally, a locomotive uses a magnet provided on the flywheel and a coil stator fixed on the engine case. When the engine is running, the flywheel is synchronously driven to rotate the magnet on the flywheel and the coil stator. The flywheel rotates and cuts the magnetic field lines so that the magnetic field lines change with time, and an alternating induced potential occurs in the coil conductor, thereby generating electrical energy.
參閱圖1至圖3B,其分別為習知具飛輪機構之引擎總成之構成示意圖、線圈定子構成示意圖、飛輪剖面示意圖及飛輪示意圖。習知飛輪機構設置於一具有一曲軸101及安裝有複數線圈定子102之引擎總成10上,包括有:一飛輪外殼體11、一飛輪內殼體12及複數磁鐵13。 1 to 3B, which are a schematic diagram of a conventional engine assembly with a flywheel mechanism, a coil stator structure, a flywheel cross-sectional view, and a flywheel. The conventional flywheel mechanism is disposed on an engine assembly 10 having a crankshaft 101 and a plurality of coil stators 102, and includes: a flywheel outer casing 11, a flywheel inner casing 12, and a plurality of magnets 13.
飛輪外殼體11設置於曲軸101上,飛輪內殼體12設置於飛輪外殼體11上並位於飛輪外殼體11之內側,複數磁鐵13固設於飛輪內殼體12及飛輪外殼體11之間並圍繞複數線圈定子102,複數線圈定子102設置於引擎總成10之引擎殼體103上,每一線圈定子102包括有一金屬鋼片1021及一銅線札1022,銅線札1022纏繞金屬鋼片1021。藉此,引擎總成10運轉時同步帶動飛輪外殼體11轉動並產生電能。 The flywheel outer casing 11 is disposed on the crankshaft 101, the flywheel inner casing 12 is disposed on and inside the flywheel outer casing 11, and a plurality of magnets 13 are fixed between the flywheel inner casing 12 and the flywheel outer casing 11 and A plurality of coil stators 102 are arranged around the engine casing 103 of the engine assembly 10. Each coil stator 102 includes a metal steel sheet 1021 and a copper wire frame 1022. The copper wire frame 1022 is wound with metal steel. Tablet 1021. As a result, when the engine assembly 10 is running, the flywheel housing 11 is synchronously driven to rotate and generate electric energy.
然而,當引擎轉速越高則其產生的電能也越高,但以往為了滿足引擎低轉速電能的需求,於引擎高轉速時需把多餘的電能消耗,對於引擎來說則是額外能量的損失。 However, the higher the engine speed, the higher the electrical energy it generates. In the past, in order to meet the engine's low-speed electrical energy requirements, excess electrical energy was consumed at high engine speeds, which is an additional energy loss for the engine.
因此,為解決上述引擎在高轉速下發電量過剩的問題,本發明人基於積極發明創作之精神,構思出一種可變磁阻飛輪機構,將可動磁鐵總成設置於飛輪內殼體及飛輪外殼體之間,並可對應引擎轉速自動調整磁鐵磁芯與線圈定子之距離,避免發電量過剩的問題產生,幾經研究實驗終至完成本發明。 Therefore, in order to solve the above-mentioned problem of excessive power generation of the engine at high speeds, the inventor conceived a variable reluctance flywheel mechanism based on the spirit of active invention and creation. It can automatically adjust the distance between the magnet core and the coil stator according to the engine speed to avoid the problem of excessive power generation. After several research experiments, the present invention has been completed.
本發明之主要目的在於解決上述問題,利用可動磁鐵總成調整發電量之可變磁阻飛輪機構,改善發電量過剩的問題,本發明人思及以下方式。 The main purpose of the present invention is to solve the above-mentioned problems, and use the variable reluctance flywheel mechanism of the movable magnet assembly to adjust the power generation amount to improve the problem of excess power generation amount.
為達成上述目的,本發明之可變磁阻飛輪機構設置於一具有一曲軸及安裝有複數線圈定子之引擎總成上,包括有:一飛輪外殼體、一飛輪內殼體及複數可動磁鐵總成。飛輪外殼體設置於曲軸上,飛輪內殼體設置於飛輪外殼體上並位於飛輪外殼體之內側,複數可動磁鐵總成設置於飛輪內殼體及飛輪外殼體之間並圍繞複數線圈定子,每一可動磁鐵總成包括有一磁鐵磁芯及一彈 性構件,磁鐵磁芯藉由彈性構件之彈性力而朝向飛輪內殼體抵靠,並可自由移動於飛輪內殼體及飛輪外殼體之間。 To achieve the above object, the variable reluctance flywheel mechanism of the present invention is provided on an engine assembly having a crankshaft and a plurality of coiled stators, including: a flywheel outer casing, a flywheel inner casing, and a plurality of movable magnets. Assembly. The flywheel outer casing is disposed on the crankshaft, the flywheel inner casing is disposed on the flywheel outer casing and is located inside the flywheel outer casing, and a plurality of movable magnet assemblies are disposed between the flywheel inner casing and the flywheel outer casing and surround a plurality of coil stators. Each movable magnet assembly includes a magnet core and a spring The magnetic member and the magnetic core abut against the inner shell of the flywheel by the elastic force of the elastic member, and can move freely between the inner shell of the flywheel and the outer shell of the flywheel.
本發明更可包括複數形成於飛輪內殼體及飛輪外殼體之間之導引槽,複數導引槽分別對應容納複數可動磁鐵總成,且以曲軸作為圓心,每一導引槽使每一磁鐵磁芯於徑向方向位移。 The present invention may further include a plurality of guide grooves formed between the inner casing and the outer casing of the flywheel, the plurality of guide grooves correspondingly accommodate a plurality of movable magnet assemblies, and the crankshaft is used as a circle center. The magnetic core is displaced in the radial direction.
上述每一彈性構件可為一板狀彈簧、一線狀彈簧及一圓盤彈簧之其一。 Each of the aforementioned elastic members may be one of a plate spring, a wire spring, and a disc spring.
上述每一可動磁鐵總成更可包括有一設置磁鐵磁芯之保護套。 Each of the above-mentioned movable magnet assemblies may further include a protective sleeve provided with a magnetic core.
上述每一可動磁鐵總成更可包括有一固設於飛輪內殼體上並可使保護套轉動之樞轉部。 Each of the above-mentioned movable magnet assemblies may further include a pivoting portion fixed on the inner casing of the flywheel and capable of rotating the protective sleeve.
在本發明中,以曲軸作為圓心,樞轉部可位於鄰近磁鐵磁芯於圓周方向上之兩側之其中一側。 In the present invention, the crankshaft is used as the center of the circle, and the pivoting portion may be located on one of two sides adjacent to the magnetic core in the circumferential direction.
上述每一彈性構件可為一板狀彈簧、一線狀彈簧、一圓盤彈簧及一扭力彈簧之其一。 Each of the aforementioned elastic members may be one of a plate spring, a wire spring, a disc spring, and a torsion spring.
上述每一線圈定子可包括有一金屬鋼片及一銅線札,銅線札纏繞金屬鋼片。 Each of the above coil stators may include a metal steel sheet and a copper wire rod, and the copper wire rod is wound around the metal steel sheet.
以上概述與接下來的詳細說明,皆為示範性質,是為了進一步說明本發明的申請專利範圍,為使本發明之上述目的、特性與優點能更淺顯易懂,將在後續的說明與圖示加以闡述。 The above summary and the following detailed description are exemplary in nature, and are intended to further illustrate the scope of patent application of the present invention. In order to make the above-mentioned objects, features, and advantages of the present invention easier to understand, the following descriptions and diagrams will be provided. Explain.
10‧‧‧引擎總成 10‧‧‧ Engine Assembly
101‧‧‧曲軸 101‧‧‧ crankshaft
102‧‧‧線圈定子 102‧‧‧coil stator
1021‧‧‧金屬鋼片 1021‧‧‧Metal steel sheet
1022‧‧‧銅線札 1022‧‧‧Copper wire
103‧‧‧引擎殼體 103‧‧‧Engine housing
11‧‧‧飛輪外殼體 11‧‧‧ flywheel housing
12‧‧‧飛輪內殼體 12‧‧‧ Flywheel inner shell
13‧‧‧磁鐵 13‧‧‧magnet
21‧‧‧飛輪外殼體 21‧‧‧ flywheel housing
22‧‧‧飛輪內殼體 22‧‧‧ Flywheel inner shell
23A,23B,23C‧‧‧可動磁鐵總成 23A, 23B, 23C‧‧‧Movable magnet assembly
231‧‧‧磁鐵磁芯 231‧‧‧Magnet core
232a‧‧‧板狀彈簧 232a‧‧‧ leaf spring
232b‧‧‧線狀彈簧 232b‧‧‧Wire Spring
232c‧‧‧圓盤彈簧 232c‧‧‧Disc spring
233‧‧‧保護套 233‧‧‧Cover
24‧‧‧導引槽 24‧‧‧Guide groove
31‧‧‧飛輪外殼體 31‧‧‧flywheel housing
32‧‧‧飛輪內殼體 32‧‧‧ flywheel inner shell
33A,33B,33C,33D‧‧‧可動磁鐵總成 33A, 33B, 33C, 33D‧‧‧movable magnet assembly
331‧‧‧磁鐵磁芯 331‧‧‧Magnet core
332a‧‧‧板狀彈簧 332a‧‧‧ leaf spring
332b‧‧‧線狀彈簧 332b‧‧‧Wire Spring
332c‧‧‧圓盤彈簧 332c‧‧‧Disc spring
332d‧‧‧扭力彈簧 332d‧‧‧torsion spring
333‧‧‧保護套 333‧‧‧Protective case
334‧‧‧樞轉部 334‧‧‧Pivot
D1,D2,D3,D4‧‧‧距離 D1, D2, D3, D4 ‧‧‧ distance
圖1係習知具飛輪機構之引擎總成之構成示意圖。 FIG. 1 is a schematic diagram of a conventional engine assembly with a flywheel mechanism.
圖2係習知具飛輪機構之引擎總成之線圈定子構成示意圖。 FIG. 2 is a schematic diagram of a coil stator of a conventional engine assembly with a flywheel mechanism.
圖3A係習知具飛輪機構之引擎總成之飛輪剖面示意圖。 3A is a schematic cross-sectional view of a flywheel of an engine assembly with a conventional flywheel mechanism.
圖3B係習知具飛輪機構之引擎總成之飛輪示意圖。 3B is a schematic diagram of a flywheel of an engine assembly with a conventional flywheel mechanism.
圖4A係本發明之可變磁阻飛輪機構之第一實施例處於低轉速之結構作動示意圖。 FIG. 4A is a schematic diagram illustrating the operation of the structure of the first embodiment of the variable reluctance flywheel mechanism of the present invention at a low rotation speed.
圖4B係本發明之可變磁阻飛輪機構之第一實施例處於高轉速之結構作動示意圖。 FIG. 4B is a schematic view showing the operation of the structure of the first embodiment of the variable reluctance flywheel mechanism of the present invention at a high rotation speed.
圖5係本發明之可變磁阻飛輪機構之第一實施例之具線狀彈簧之可動磁鐵總成之結構示意圖。 FIG. 5 is a schematic structural diagram of a movable magnet assembly with a linear spring according to the first embodiment of the variable reluctance flywheel mechanism of the present invention.
圖6A係本發明之可變磁阻飛輪機構之第一實施例之具圓盤彈簧之可動磁鐵總成之結構示意圖。 FIG. 6A is a schematic structural diagram of a movable magnet assembly with a disc spring in the first embodiment of the variable reluctance flywheel mechanism of the present invention.
圖6B係本發明之可變磁阻飛輪機構之可動磁鐵總成之圓盤彈簧結構示意圖。 FIG. 6B is a schematic structural diagram of a disc spring of a movable magnet assembly of a variable reluctance flywheel mechanism of the present invention.
圖7A係本發明之可變磁阻飛輪機構之第二實施例處於低轉速之結構作動示意圖。 FIG. 7A is a schematic diagram of the structure of the second embodiment of the variable reluctance flywheel mechanism of the present invention at a low rotation speed.
圖7B係本發明之可變磁阻飛輪機構之第二實施例處於高轉速之結構作動示意圖。 FIG. 7B is a schematic diagram of the structure of the second embodiment of the variable reluctance flywheel mechanism of the present invention at a high rotation speed.
圖8係本發明之可變磁阻飛輪機構之第二實施例之具線狀彈簧之可動磁鐵總成之結構示意圖。 8 is a schematic structural diagram of a movable magnet assembly with a linear spring according to a second embodiment of the variable reluctance flywheel mechanism of the present invention.
圖9係本發明之可變磁阻飛輪機構之第二實施例之具圓盤彈簧之可動磁鐵總成之結構示意圖。 FIG. 9 is a schematic structural diagram of a movable magnet assembly with a disc spring according to a second embodiment of the variable reluctance flywheel mechanism of the present invention.
圖10係本發明之可變磁阻飛輪機構之第二實施例之具扭力彈簧之可動磁鐵總成之結構示意圖。 FIG. 10 is a schematic structural diagram of a movable magnet assembly with a torsion spring according to a second embodiment of the variable reluctance flywheel mechanism of the present invention.
參閱圖4A至圖4B,其分別為本發明之可變磁阻飛輪機構之第一實施例處於低轉速之結構作動示意圖及處於高轉速之結構作動示意圖。本發明之可變磁阻飛輪機構設置於一具有一曲軸及安裝有複數線圈定子之引擎總成上,包括有:一飛輪外殼體21、一飛輪內殼體22、四可動磁鐵總成23A及四導引槽24。 Referring to FIG. 4A to FIG. 4B, it is a schematic diagram of a structure operation at a low rotation speed and a structural action diagram at a high rotation speed of the first embodiment of the variable reluctance flywheel mechanism of the present invention. The variable reluctance flywheel mechanism of the present invention is disposed on an engine assembly having a crankshaft and a plurality of coil stators, and includes: a flywheel outer casing 21, a flywheel inner casing 22, and four movable magnet assemblies 23A. And four guide grooves 24.
飛輪外殼體21設置於曲軸上,飛輪內殼體22設置於飛輪外殼體21上並位於飛輪外殼體21之內側,四可動磁鐵總成23A設置於飛輪內殼體22及飛輪外殼體21之間並圍繞複數線圈定子,複數線圈定子設置於引擎總成之引擎殼體上,每一線圈定子包括有一金屬鋼片及一銅線札,銅線札纏繞金屬鋼片,每一可動磁鐵總成23A包括有一磁鐵磁芯231、一板狀彈簧232a及一保護套233,磁鐵磁芯231藉由板狀彈簧232a之彈性力而朝向飛輪內殼體22抵靠,並可自由移動於飛輪內殼體22及飛輪外殼體21之間,保護套233用以設置磁鐵磁芯231,四導引槽24形成於飛輪內殼體22及飛輪外殼體21之間,四導引槽24分別對應容納四可動磁鐵總成23A,且以曲軸安裝處作為圓心,每一導引槽24使每一磁鐵磁芯231於徑向方向位移。 The flywheel outer casing 21 is disposed on the crankshaft, the flywheel inner casing 22 is disposed on and inside the flywheel outer casing 21, and the four movable magnet assemblies 23A are disposed between the flywheel inner casing 22 and the flywheel outer casing 21. A plurality of coil stators are arranged around the engine casing of the engine assembly. Each coil stator includes a metal steel sheet and a copper wire rod, and the copper wire rod is wound around the metal steel sheet. Component 23A includes a magnet core 231, a plate spring 232a, and a protective sleeve 233. The magnet core 231 abuts toward the flywheel inner casing 22 by the elastic force of the plate spring 232a, and can move freely in the flywheel Between the housing 22 and the flywheel outer body 21, a protective sleeve 233 is provided for the magnet core 231. Four guide grooves 24 are formed between the flywheel inner housing 22 and the flywheel outer body 21, and the four guide grooves 24 are respectively accommodated correspondingly. The four movable magnet assemblies are 23A, with the crankshaft installation as the center, and each guide groove 24 displaces each magnetic core 231 in the radial direction.
藉由上述結構,可動磁鐵總成23A會對應引擎總成之曲軸轉速,使磁鐵磁芯231自動調整與線圈定子之間的距離,詳細而言,如圖4A所示,在引擎總成處於低轉速時,飛輪外殼體21也處於低轉速,低轉速時磁鐵磁芯231 受到的離心力較小,板狀彈簧232a之彈性力使磁鐵磁芯231朝向飛輪內殼體22抵靠,使磁鐵磁芯231與飛輪外殼體21中心處之間具有距離D1,此時磁鐵磁芯231與線圈定子之徑向距離較近,磁力線較強而可產生較大的發電量。 With the above structure, the movable magnet assembly 23A will correspond to the crankshaft rotation speed of the engine assembly, so that the distance between the magnet core 231 and the coil stator is automatically adjusted. As shown in FIG. 4A, the engine assembly is located at When the speed is low, the flywheel housing 21 is also at a low speed. The magnet core 231 is at a low speed. The centrifugal force received is small, and the elastic force of the plate-shaped spring 232a makes the magnet core 231 abut against the flywheel inner casing 22, so that there is a distance D1 between the magnet core 231 and the center of the flywheel outer body 21, and the magnet core The radial distance between 231 and the coil stator is relatively short, and the magnetic field lines are strong and can generate a large amount of power generation.
而當引擎總成處於高轉速時,如圖4B所示,高轉速時磁鐵磁芯231受到的離心力較大,磁鐵磁芯231壓迫板狀彈簧232a而朝向遠離飛輪外殼體21中心處移動,使磁鐵磁芯231與飛輪外殼體21中心處之間形成大於距離D1之距離D2,此時磁鐵磁芯231與線圈定子之徑向距離較遠,磁力線較弱而可產生較小的發電量,如此即可滿足引擎總成低轉速時的發電量需求,又可解決引擎總成高轉速發電量過剩的問題。 When the engine assembly is at a high speed, as shown in FIG. 4B, the centrifugal force received by the magnetic core 231 is large at high speed, and the magnetic core 231 presses the plate spring 232a to move away from the center of the flywheel housing 21, so A distance D2 greater than the distance D1 is formed between the magnetic core 231 and the center of the flywheel housing 21. At this time, the radial distance between the magnetic core 231 and the coil stator is relatively long, and the magnetic field lines are weak and can generate a small amount of power. In this way, the power generation demand at low engine speed can be met, and the problem of excess power generation at high engine speed can be solved.
參閱圖5至圖6B,其分別為本發明之可變磁阻飛輪機構之第一實施例之具線狀彈簧之可動磁鐵總成之結構示意圖、第一實施例之具圓盤彈簧之可動磁鐵總成之結構示意圖及可動磁鐵總成之圓盤彈簧結構示意圖。圖5示出可動磁鐵總成23B之線狀彈簧232b,圖6A及圖6B示出可動磁鐵總成23C之圓盤彈簧232c,也就是說,可動磁鐵總成之彈性構件可為一板狀彈簧232a、一線狀彈簧232b及一圓盤彈簧232c之其一,或是其他具相同功效之彈性構件。 5 to 6B, which are structural diagrams of a movable magnet assembly with a linear spring in the first embodiment of the variable reluctance flywheel mechanism of the present invention, and a movable magnet with a disc spring in the first embodiment. Schematic diagram of the assembly and the structure of the disc spring of the movable magnet assembly. FIG. 5 shows the linear spring 232b of the movable magnet assembly 23B, and FIGS. 6A and 6B show the disk spring 232c of the movable magnet assembly 23C, that is, the elastic member of the movable magnet assembly may be a plate spring One of 232a, a linear spring 232b, and a disc spring 232c, or other elastic members with the same effect.
參閱圖7A至圖7B,其分別為本發明之可變磁阻飛輪機構之第二實施例處於低轉速之結構作動示意圖及處於高轉速之結構作動示意圖。本發明之可變磁阻飛輪機構設置於一具有一曲軸及安裝有複數線圈定子之引擎總成上,包括有:一飛輪外殼體31、一飛輪內殼體32及四可動磁鐵總成33A。 Referring to FIG. 7A to FIG. 7B, it is a schematic diagram of a structural operation at a low speed and a structural action at a high speed of a second embodiment of the variable reluctance flywheel mechanism of the present invention. The variable reluctance flywheel mechanism of the present invention is disposed on an engine assembly having a crankshaft and a plurality of coiled stators, and includes: a flywheel outer casing 31, a flywheel inner casing 32, and four movable magnet assemblies 33A. .
飛輪外殼體31設置於曲軸上,飛輪內殼體32設置於飛輪外殼體31上並位於飛輪外殼體31之內側,四可動磁鐵總成33A設置於飛輪內殼體32及飛輪外殼體31之間並圍繞複數線圈定子,複數線圈定子設置於引擎總成之引 擎殼體上,每一線圈定子包括有一金屬鋼片及一銅線札,銅線札纏繞金屬鋼片,每一可動磁鐵總成33A包括有一磁鐵磁芯331、一板狀彈簧332a、一保護套333及一樞轉部334,磁鐵磁芯331藉由板狀彈簧332a之彈性力而朝向飛輪內殼體32抵靠,並可自由移動於飛輪內殼體32及飛輪外殼體31之間,保護套333用以設置磁鐵磁芯331,樞轉部334固設於飛輪內殼體32上並可使保護套333轉動,且以曲軸安裝處作為圓心,樞轉部334位於鄰近磁鐵磁芯331於圓周方向上之兩側之其中一側。 The flywheel outer casing 31 is disposed on the crankshaft, the flywheel inner casing 32 is disposed on and inside the flywheel outer casing 31, and the four movable magnet assemblies 33A are disposed between the flywheel inner casing 32 and the flywheel outer casing 31. And surrounds a plurality of coil stators, and the plurality of coil stators are arranged at the lead of the engine assembly On the engine case, each coil stator includes a metal steel sheet and a copper wire rod, and the copper wire rod is wound around the metal steel sheet. Each movable magnet assembly 33A includes a magnet core 331, a plate spring 332a, and a protection. The sleeve 333 and a pivot portion 334, the magnet core 331 abut against the flywheel inner casing 32 by the elastic force of the plate spring 332a, and can move freely between the flywheel inner casing 32 and the flywheel outer casing 31. The protective sleeve 333 is used to set the magnetic core 331. The pivoting portion 334 is fixed on the flywheel inner casing 32 and can rotate the protective sleeve 333. The crankshaft is installed as the center. The pivoting portion 334 is located adjacent to the magnetic core 331. One of the two sides in the circumferential direction.
藉由上述結構,可動磁鐵總成33A會對應引擎總成之曲軸轉速,使磁鐵磁芯331自動調整與線圈定子之間的距離,詳細而言,如圖7A所示,在引擎總成處於低轉速時,磁鐵磁芯331受到的離心力較小,板狀彈簧332a之彈性力使磁鐵磁芯331朝向飛輪內殼體32抵靠,使磁鐵磁芯331與飛輪外殼體31中心處之間具有距離D3,此時磁鐵磁芯331與線圈定子之徑向距離較近,磁力線較強而可產生較大的發電量。 With the above structure, the movable magnet assembly 33A will correspond to the crankshaft rotation speed of the engine assembly, so that the distance between the magnet core 331 and the coil stator is automatically adjusted. As shown in FIG. 7A, in detail, the engine assembly is located at At low speeds, the centrifugal force received by the magnet core 331 is small, and the elastic force of the plate spring 332a makes the magnet core 331 abut against the flywheel inner casing 32, so that the magnet core 331 and the center of the flywheel housing 31 have The distance D3, at this time, the radial distance between the magnet core 331 and the coil stator is relatively short, the magnetic field lines are strong and a large amount of power can be generated.
而當引擎總成處於高轉速時,如圖7B所示,高轉速時磁鐵磁芯331受到的離心力較大,磁鐵磁芯331以樞轉部334為軸心轉動同時遠離飛輪外殼體31中心處,使磁鐵磁芯331與飛輪外殼體31中心處之間形成大於距離D3之距離D4,此時磁鐵磁芯331與線圈定子之徑向距離較遠,磁力線較弱而可產生較小的發電量,如此即可滿足引擎總成低轉速時的發電量需求,又可解決引擎總成高轉速發電量過剩的問題。 When the engine assembly is at a high speed, as shown in FIG. 7B, the centrifugal force received by the magnetic core 331 is large at high speed. The magnetic core 331 rotates around the pivot 334 as an axis while being far away from the center of the flywheel housing 31. The distance D4 between the magnetic core 331 and the center of the flywheel housing 31 is greater than the distance D3. At this time, the radial distance between the magnetic core 331 and the coil stator is relatively long, and the magnetic field lines are weak and can generate smaller power generation. This can meet the power generation demand of the engine assembly at low speed, and can solve the problem of excessive power generation of the engine assembly at high speed.
參閱圖8至圖10,其分別為本發明之可變磁阻飛輪機構之第二實施例之具線狀彈簧之可動磁鐵總成之結構示意圖、第二實施例之具圓盤彈簧之可動磁鐵總成之結構示意圖及第二實施例之具扭力彈簧之可動磁鐵總成之結構 示意圖。圖8示出可動磁鐵總成33B之線狀彈簧332b,圖9示出可動磁鐵總成33C之圓盤彈簧332c,圖10示出可動磁鐵總成33D之扭力彈簧332d,也就是說,可動磁鐵總成之彈性構件可為一板狀彈簧332a、一線狀彈簧332b、一圓盤彈簧332c及一扭力彈簧332d之其一,或是其他具相同功效之彈性構件。 8 to 10, which are structural diagrams of a movable magnet assembly with a linear spring in the second embodiment of the variable reluctance flywheel mechanism of the present invention, and a movable magnet with a disc spring in the second embodiment. Schematic diagram of the assembly and the structure of the movable magnet assembly with a torsion spring of the second embodiment schematic diagram. FIG. 8 shows the linear spring 332b of the movable magnet assembly 33B, FIG. 9 shows the disc spring 332c of the movable magnet assembly 33C, and FIG. 10 shows the torsion spring 332d of the movable magnet assembly 33D, that is, the movable magnet The elastic member of the assembly may be one of a plate spring 332a, a linear spring 332b, a disc spring 332c, and a torsion spring 332d, or other elastic members having the same effect.
由上述內容可知,本發明之可變磁阻飛輪機構利用可動磁鐵總成對應引擎轉速自動調整磁鐵磁芯與線圈定子之距離並調整發電量,在引擎總成低轉速時提供較高發電量,引擎總成高轉速時提供較低發電量,避免發電量過剩之問題產生。 From the above, it can be known that the variable reluctance flywheel mechanism of the present invention uses a movable magnet assembly to automatically adjust the distance between the magnet core and the coil stator and adjust the power generation amount according to the engine speed, and provides a higher power generation amount when the engine assembly has a low speed , The engine assembly provides lower power generation at high speeds to avoid the problem of excessive power generation.
上述實施例僅係為了方便說明而舉例而已,本發明所主張之權利範圍自應以申請專利範圍所述為準,而非僅限於上述實施例。 The above embodiments are merely examples for the convenience of description. The scope of the claimed rights of the present invention should be based on the scope of the patent application, rather than being limited to the above embodiments.
Claims (8)
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Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1998002325A1 (en) * | 1996-07-12 | 1998-01-22 | Un Kil Paek | High-powered powertrains by wheel and axle potential energy |
| US5829319A (en) * | 1996-10-04 | 1998-11-03 | Vibratech, Inc. | Magneto-rheological torsional vibration damper |
| EP1191673A2 (en) * | 2000-09-14 | 2002-03-27 | Denso Corporation | Compact and reliable structure of multi-rotor synchronous machine |
| US20020047418A1 (en) * | 2000-09-14 | 2002-04-25 | Masahiro Seguchi | Compact and reliable structure of multi-rotor synchronous machine |
| WO2003047068A1 (en) * | 2001-09-08 | 2003-06-05 | Lei He | Ring mode starter/generator |
| WO2011154182A1 (en) * | 2010-06-09 | 2011-12-15 | Robert Bosch Gmbh | Device for damping and energy recovery for internal combustion engines |
-
2018
- 2018-10-23 TW TW107137364A patent/TWI673942B/en not_active IP Right Cessation
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1998002325A1 (en) * | 1996-07-12 | 1998-01-22 | Un Kil Paek | High-powered powertrains by wheel and axle potential energy |
| US5829319A (en) * | 1996-10-04 | 1998-11-03 | Vibratech, Inc. | Magneto-rheological torsional vibration damper |
| EP1191673A2 (en) * | 2000-09-14 | 2002-03-27 | Denso Corporation | Compact and reliable structure of multi-rotor synchronous machine |
| US20020047418A1 (en) * | 2000-09-14 | 2002-04-25 | Masahiro Seguchi | Compact and reliable structure of multi-rotor synchronous machine |
| WO2003047068A1 (en) * | 2001-09-08 | 2003-06-05 | Lei He | Ring mode starter/generator |
| WO2011154182A1 (en) * | 2010-06-09 | 2011-12-15 | Robert Bosch Gmbh | Device for damping and energy recovery for internal combustion engines |
Non-Patent Citations (1)
| Title |
|---|
| )A1;)A1 * |
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