TWI763610B - Flywheel power storage system - Google Patents
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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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Abstract
Description
本發明係關於一種電動機,特別是一種飛輪能量儲存系統。The present invention relates to an electric motor, in particular to a flywheel energy storage system.
飛輪能量儲存(Flywheel energy storage,FES)系統,是一種能量儲存的方式,其主要是利用加速具有轉軸的。A flywheel energy storage (FES) system is a method of energy storage, which mainly uses acceleration and has a rotating shaft.
典型的飛輪能量儲存系統包含一個腔體,其內配置有飛輪以及用於帶動其轉動的電動機組,電動機組可作為能量輸出與輸入的裝置,能以馬達的形態接收電力輸入以驅動飛輪旋轉,當飛輪轉動至極高速度,能量可以旋轉動能的形式儲存於系統中,電動機組也能改以發電機的形態將飛輪旋轉所儲存的能量轉換為電力輸出。A typical flywheel energy storage system includes a cavity, which is equipped with a flywheel and a motor unit for driving it to rotate. The motor unit can be used as a device for energy output and input, and can receive power input in the form of a motor to drive the flywheel to rotate. When the flywheel rotates to a very high speed, the energy can be stored in the system in the form of rotational kinetic energy, and the motor unit can also change the energy stored in the rotation of the flywheel into electrical output in the form of a generator.
由此可知,飛輪能量儲存系統可將機械能與電能作直接的轉換,且由於飛輪的轉速能被快速提升而得以快速地吸收或釋放能量,因此其功率相對於其他儲能裝置而言更大。例如相較於一般化學電池(例如鉛酸電池),飛輪能量儲存系統的功率密度明顯高出許多,使得在某些需要快速儲存能量的場合,飛輪能量儲存系統比起化學電池更為適用,例如在風量變化很大的風力發電廠,或水量變化很大的波浪發電廠等場合,需要快速吸收或釋放能量的裝置來穩定電壓或電量;或者,飛輪能量儲存系統也適用於機動車輛上,可以飛輪快速吸收煞車能量或減速能量,並於起動時快速釋出能量;又或者,由於飛輪能量系統的快速儲能特點,已有越來越多充電站引入飛輪能量系統的技術,以大幅縮短充電車輛所需的時間。前述的原因與優勢使得飛輪能量儲存系統逐漸受到業界的重視。It can be seen that the flywheel energy storage system can directly convert mechanical energy and electrical energy, and because the speed of the flywheel can be rapidly increased to quickly absorb or release energy, its power is larger than other energy storage devices. . For example, compared with general chemical batteries (such as lead-acid batteries), the power density of flywheel energy storage systems is significantly higher, making flywheel energy storage systems more suitable than chemical batteries in some occasions where fast energy storage is required, such as In occasions such as wind power plants with large changes in air volume, or wave power plants with large changes in water volume, devices that quickly absorb or release energy are required to stabilize voltage or electricity; alternatively, the flywheel energy storage system is also suitable for motor vehicles. The flywheel quickly absorbs braking energy or deceleration energy, and quickly releases energy when starting; or, due to the fast energy storage characteristics of the flywheel energy system, more and more charging stations have introduced the technology of the flywheel energy system to greatly shorten the charging time. time required for the vehicle. The aforementioned reasons and advantages make the flywheel energy storage system gradually attract the attention of the industry.
但,目前的飛輪能量儲存系統仍有不足之處。舉例來說,為了驅動飛輪,現有的飛輪能量儲存系統的電動機與飛輪均配置於真空腔室中,可是電動機運轉時,其定子線圈等元件會產生高熱,若不能排除,很容易因為累積過多熱量而燒毀,甚至也會嚴重影響周圍其他元件,例如使周邊電路損毀,或是使周圍的磁性材料產生熱應力,從而影響整體系統的可靠度與穩定性。為此,有業者採取在外殼上穿設氣冷管或液冷管,以對定子線圈進行散熱,但這樣的作法會嚴重影響氣密性,增加飛輪旋轉的阻力。However, current flywheel energy storage systems still have shortcomings. For example, in order to drive the flywheel, the motor and the flywheel of the existing flywheel energy storage system are arranged in a vacuum chamber, but when the motor is running, the stator coil and other components will generate high heat. If it cannot be eliminated, it is easy to accumulate too much heat. Burning can even seriously affect other surrounding components, such as damage to peripheral circuits, or thermal stress to surrounding magnetic materials, thereby affecting the reliability and stability of the overall system. For this reason, some manufacturers have adopted air-cooled tubes or liquid-cooled tubes through the casing to dissipate heat from the stator coil, but this approach will seriously affect the air tightness and increase the resistance of the flywheel to rotate.
據此,如何能在不影響飛輪儲能系統的真空密封性的前提,解決傳統上飛輪能量儲存系統的散熱問題,實為目前業界所致力研究的重點項目之一。Accordingly, how to solve the heat dissipation problem of the traditional flywheel energy storage system without affecting the vacuum tightness of the flywheel energy storage system is indeed one of the key research projects in the industry at present.
有鑑於此,本發明提供一種飛輪能量儲存系統,可將生熱元件隔絕於真空腔室之外,從而可避免採用傳統上會影響真空密封性的散熱手段。In view of this, the present invention provides a flywheel energy storage system, which can isolate the heat generating element from the vacuum chamber, so as to avoid the traditional heat dissipation means that would affect the vacuum tightness.
根據本發明之一實施例所揭露的一種飛輪能量儲存系統,包含一外殼、一飛輪、一轉軸、一內轉子、一外轉子以及一定子。外殼具有一真空腔室。飛輪設於真空腔室。轉軸設於真空腔室且穿設飛輪。內轉子設於真空腔室且固定於轉軸上。外轉子設於真空腔室之外。外轉子圍繞內轉子而可磁力作用於內轉子。定子設於真空腔室之外。定子圍繞外轉子而可用於驅動外轉子。A flywheel energy storage system disclosed according to an embodiment of the present invention includes a casing, a flywheel, a rotating shaft, an inner rotor, an outer rotor and a stator. The housing has a vacuum chamber. The flywheel is arranged in the vacuum chamber. The rotating shaft is arranged in the vacuum chamber and passes through the flywheel. The inner rotor is arranged in the vacuum chamber and fixed on the rotating shaft. The outer rotor is arranged outside the vacuum chamber. The outer rotor surrounds the inner rotor and can magnetically act on the inner rotor. The stator is located outside the vacuum chamber. The stator surrounds the outer rotor and can be used to drive the outer rotor.
根據本發明前述實施例所揭露的飛輪能量儲存系統,由於可用於驅動外轉子的定子位於真空腔室之外,與外轉子作用的內轉子位於真空腔室之內,因此外轉子與內轉子能構成以磁力驅動轉軸與飛輪的磁性軸聯器,以實現無機械接觸的方式驅動轉軸與飛輪,以讓轉軸與飛輪能在無阻力的情況下旋轉。According to the flywheel energy storage system disclosed in the foregoing embodiments of the present invention, since the stator that can be used to drive the outer rotor is located outside the vacuum chamber, and the inner rotor that interacts with the outer rotor is located inside the vacuum chamber, the outer rotor and the inner rotor can A magnetic shaft coupling is formed that drives the shaft and the flywheel by magnetic force, and drives the shaft and the flywheel without mechanical contact, so that the shaft and the flywheel can rotate without resistance.
並且,電動機上通電流生熱的定子被排除於真空腔室之外,此配置能使飛輪能量儲存系統將運轉時主要產生熱能的元件隔絕於真空腔室之外,使飛輪能量儲存系統避免採用傳統上會影響真空密封性的散熱手段,從而有助於確保飛輪運轉所需的氣密性。In addition, the stator of the electric motor that generates heat through current is excluded from the vacuum chamber. This configuration enables the flywheel energy storage system to isolate the components that mainly generate heat energy during operation from the vacuum chamber, so that the flywheel energy storage system can avoid the use of Heat dissipation, which traditionally affects vacuum tightness, helps ensure the air tightness required for flywheel operation.
以上之關於本發明揭露內容之說明及以下之實施方式之說明,係用以示範與解釋本發明之精神與原理,並且提供本發明之專利申請範圍更進一步之解釋。The above description of the disclosure of the present invention and the description of the following embodiments are used to demonstrate and explain the spirit and principle of the present invention, and provide further explanation of the scope of the patent application of the present invention.
以下將以實施方式詳細敘述本發明之詳細特徵以及優點,其內容足以使任何熟習相關技藝者瞭解本發明之技術內容並據以實施,但非以任何觀點限制本發明之範疇。The detailed features and advantages of the present invention will be described in detail in the following embodiments, the content of which is sufficient to enable any person skilled in the relevant art to understand the technical content of the present invention and implement accordingly, but does not limit the scope of the present invention in any point of view.
以下實施例將搭配圖式進行說明,為達圖面整潔之目的,一些習知慣用的結構與元件在圖式可能會以簡單示意的方式繪示之。並且,圖式中部份的特徵可能會略為放大或改變其比例或尺寸,以達到便於理解與觀看本發明之技術特徵的目的,但這並非用於限定本發明。此外,為便於觀看,部分圖式中的某些結構線可能以虛線表示。The following embodiments will be described in conjunction with the drawings. For the purpose of neatness of the drawings, some conventional structures and elements may be shown in a simple and schematic manner in the drawings. In addition, some features in the drawings may be slightly enlarged or their proportions or dimensions may be changed to achieve the purpose of facilitating understanding and viewing of the technical features of the present invention, but this is not intended to limit the present invention. In addition, some of the structural lines in some of the drawings may be represented by dashed lines for ease of viewing.
此外,下文中可能會使用「端」、「部」、「部分」、「區域」、「處」等術語來描述特定元件與結構或是其上或其之間的特定技術特徵,但這些元件與結構並不受這些術語所限制。以下文中也可能使用諸如「實質上」、「約」及「大致上」等術語,用於描述所修飾之情況或事件可能存在的合理或可接受的偏差量,但仍可達到所預期的結果。In addition, hereinafter, terms such as "end", "portion", "portion", "region", "location" may be used to describe specific elements and structures or specific technical features on or between them, but these elements AND structures are not limited by these terms. Terms such as "substantially", "about" and "substantially" may also be used hereinafter to describe a reasonable or acceptable amount of deviation that may exist from the circumstances or events modified and still achieve the desired result .
另外,下文中可能使用「至少一」來描述所指元件的數量,但除非另有明確說明,其不應僅限於數量為「僅有一」的情況。下文中也可能使用「及/或」的術語,其應被理解為包括所列出項目中之任一者及一或多者之所有組合。In addition, hereinafter, "at least one" may be used to describe the quantity of a referenced element, but unless expressly stated otherwise, it should not be limited to the case where the quantity is "only one". The term "and/or" may also be used below, which should be understood to include any and all combinations of one or more of the listed items.
請參閱圖1,本發明之一實施例給出了一種飛輪能量儲存系統1,於下文中也可簡稱為「系統」。大致上,飛輪能量儲存系統1可包含一飛輪模組10以及一驅動模組20,飛輪模組10主要是飛輪能量儲存系統1中用於接收動能以儲存能量的部分,而驅動模組20可組裝於飛輪模組10上,是指飛輪能量儲存系統1中用於提供動能的部分。Referring to FIG. 1 , an embodiment of the present invention provides a flywheel
具體來看,飛輪模組10可包含一外殼110、一轉軸(shaft)150以及一飛輪(flywheel)130。外殼110可圍繞出一個封閉的空間並被抽真空,從而形成一真空腔室S,但本發明並非以外殼110的形狀與抽真空的手段為限。外殼110例如可由鋁合金等剛性高但不導磁的材質所構成,但本實施例並非以外殼110的材料為限。此外,外殼110不限於是一體成型的結構、或可由多段結構組裝成一體。在外殼110是以多段結構組裝成一體的情況中,各段結構可由螺栓相接,且各段結構之銜接處可採用墊襯或塗上密封膠等方式達到氣密的效果。Specifically, the
進一步來看,於本實施例中,外殼110可包含兩個部分,分別為一飛輪容置部111以及一延伸隔離部113。延伸隔離部113自飛輪容置部111的一側軸向延伸,飛輪容置部111與延伸隔離部113略呈筒狀,惟飛輪容置部111的直徑較延伸隔離部113的直徑大。飛輪容置部111與延伸隔離部113能以任何合適的方式相組裝,其內部空間相連而共同構成前述的真空腔室S。此外,於此定義外殼110可具有一內壁面114與一外壁面115,如圖所示,所述內壁面114是指飛輪容置部111與延伸隔離部113上用於圍繞形成真空腔室S的內表面,而所述外壁面115則是指與內壁面114相對而朝外的外表面。Looking further, in this embodiment, the
轉軸130容置於外殼110的真空腔室S中。如圖所示,部分的轉軸130容置於飛輪容置部111中,另一部分的轉軸130容置於延伸隔離部113中。飛輪150也容置於外殼110的真空腔室S中。如圖所示,飛輪150被容置於飛輪容置部111中,轉軸130穿設飛輪150並與飛輪150相固定,從而與飛輪150共同構成一旋轉體。在此配置下,轉軸130可接收驅動模組20的動能而旋轉,從而帶動飛輪150一併於真空腔室S中轉動。The rotating
此外,飛輪150作為能量儲存的載體,其每單位重量或單位體積下能儲存的能量越高越好(即能量密度),為了達到這個目的,於本實施例或其他實施例中,飛輪150的外型大致呈圓筒狀,但本發明並非以此為限,於本發明其他實施例之飛輪也可因應各種實際需求而具有所需的形狀。另一方面,飛輪150的材料可使用結構強度高且密度高的材料所構成,以助於提高其單位體積之旋轉質量、以及避免於旋轉而產生巨大離心力時不慎破裂的問題,但本發明並非以此為限。In addition, the
除此之外,於本實施例中,飛輪能量儲存系統1還可包含二被動式磁浮軸承(passive magnetic bearing,PMB)190,被動式磁浮軸承190可分別配置於轉軸130的相對兩端處。具體來說,其中一被動式磁浮軸承190可被配置於轉軸130上位於飛輪容置部111內之一端處,而另一被動式磁浮軸承190可被配置於轉軸130上位於延伸隔離部113內之一端處。被動式磁浮軸承190主要用於對轉軸130提供軸向方向的支撐。In addition, in this embodiment, the flywheel
詳細來說,被動式磁浮軸承190各包含一永磁體組191與一永磁體組193,永磁體組191位於真空腔室S內且固定於轉軸130上,而永磁體組193位於真空腔室S外且固定於延伸隔離部113的外壁面115,並圍繞永磁體組191。更具體地,永磁體組193為周向地(circumferentially)配置於延伸隔離部113。永磁體組191與永磁體組193可為連續環狀結構或是由相間隔之多個子單元所構成,本發明並非以此為限。永磁體組191與193的位置相對應,且各自具有能與另一者相互作用的數個永久磁鐵排列,從而可對轉軸130提供軸向方向的磁浮力,進而可讓轉軸130以及飛輪150能懸浮於真空腔室S中,以避免轉軸130與飛輪150轉動時與周圍結構產生摩擦。由此可知,被動式磁浮軸承190可視為是被動式軸向磁浮軸承。於一些情況中,永磁體組191與193的永久磁鐵經過合適的排列與間隔配置下,可至少產生約900至1100牛頓的磁浮力,以幫助轉軸130以及飛輪150抵抗重力。但需聲明的是,只要能達到提供轉軸130以及飛輪150於所需方向的支撐,永磁體組191與193上相互作用的永久磁鐵可以任何已知的合適方式進行排列,其數量與規格也可依據實際需求進行調整,本發明並非以此為限。In detail, the passive
補充說明的是,被動式磁浮軸承190僅以永久磁鐵所構成,因此相互作用產生磁浮力時完全不會產生明顯的熱能。當然,基於其他實際考量,於其他實施例之飛輪模組內可選擇性增加或減少被動式磁浮軸承的數量,本發明並非以此為限。It should be added that the passive
另外,於本實施例中,飛輪能量儲存系統1還可包含一輔助軸承195,輔助軸承195可位於延伸隔離部113內,以支撐轉軸130之一外環部(flange)131,所述的外環部131為自轉軸130表面上徑向突出的環狀結構。輔助軸承195能支撐外環部131以對轉軸130提供徑向方向的定位及軸向方向的支撐,藉此,輔助軸承195還能用於防止系統中的磁浮軸承過載或故障等問題。但,外環部131與輔助軸承195均為選用,本發明並非以此為限。In addition, in this embodiment, the flywheel
另一方面,驅動模組20為一個利用磁耦合而非機械連接的方式來傳遞扭矩的裝置,因而可以在飛輪模組10的真空腔室S之外的情況下驅動轉軸130與飛輪150。如圖所示,驅動模組20可包含一安裝座205、一內轉子(inner rotor)211、一外轉子(outer rotor)213以及一定子(stator)230。On the other hand, the driving
詳細來說,安裝座205可固定於外殼110上,例如是套設於外殼110之延伸隔離部113外,並可以任何合適的方式固定於延伸隔離部113及飛輪容置部111,例如可以但不限於是螺鎖或焊接。In detail, the mounting
內轉子211位於外殼110之延伸隔離部113內,且內轉子211套設於轉軸130並與轉軸130相固定。或者說,內轉子211位於真空腔室S內且固定於轉軸130位於延伸隔離部113的部分。因此,內轉子211可與轉軸130及飛輪150構成一體而能一併在真空腔室S內轉動。並且,為了在真空腔室S轉動而不與延伸隔離部113之內壁面114產生干涉,內轉子211與延伸隔離部113之間可保持一個合適的間隙。內轉子211內可包含一內轉子磁鐵座2111,以供多顆合適的永久磁石2112設置固定,內轉子磁鐵座2111可以合適的材質或結構(如矽鋼片推疊)所製成,以支撐、保護並隔離這些永久磁石2112,但本發明並非以內轉子211內之永久磁石的數量、形狀、種類等為限。The
外轉子213設置於延伸隔離部113外且位置對應於內轉子211。或者說,外轉子213位於真空腔室S之外且圍繞內轉子211。進一步來看,外轉子213可經由滾珠軸承270而可活動地設置於安裝座205上,且外轉子213環繞延伸隔離部113且與延伸隔離部113保持一氣隙。外轉子213內可包含一外轉子磁鐵座2131,以供多顆合適的永久磁石2132設置固定,外轉子磁鐵座2131可以合適的材質或結構(如矽鋼片推疊)所製成,以支撐、保護並隔離這些永久磁石2132,但本發明並非以外轉子213內之永久磁石的數量、形狀、種類等為限。The
定子230固定於安裝座205且位於外轉子213的外側。或者說,定子230位於真空腔室S之外且圍繞外轉子213。定子230可包含定子鐵芯(stator core)與圈繞於定子鐵芯的繞組(windings),其中,為達圖式簡潔之目的,定子230僅以簡易方框示意而未具體繪示定子鐵芯與繞組。The
可對定子230的繞組通電流,從而在定子230的定子鐵芯與外轉子213的矽鋼片上產生磁場而驅使外轉子213轉動。由此可知,定子230與外轉子213可共同構成一電動機(electric motor)EM。在此情況下,定子230可視為或被稱為電動機EM的定子,而外轉子213可視為或被稱為電動機EM的內轉子。A current can be applied to the windings of the
並且,當定子230帶動外轉子213轉動時,外轉子213上之永久磁石2132的磁力線可穿過延伸隔離部113與間隙而帶動內轉子211,從而一併使內轉子211與轉軸130及飛輪150所共同構成的總成同步旋轉。由此可知,內轉子211與外轉子213可共同構成一磁性軸聯器(magnetic coupler)210,以透過磁力傳動的方式驅動位於真空腔室S內的轉軸130與飛輪150。於此需聲明的是,只要能達到使內轉子211與外轉子213之間能透過磁力同步旋轉之目的,內轉子211之永久磁石2112與外轉子213之永久磁石2132可以任何已知的合適方式進行排列,本發明並非以此為限。In addition, when the
此外,於本實施例中,飛輪能量儲存系統1還可包含至少一主動式磁浮軸承(active magnetic bearing,AMB)250,需先聲明的是,為達圖式簡潔之目的,主動式磁浮軸承250僅以永磁體組251與磁浮軸承定子部253表示,其他不影響理解本實施例之精神的元件,如致動器、控制器、功率放大器等,則將省略而未繪示。In addition, in the present embodiment, the flywheel
主動式磁浮軸承250例如可分別配置於電動機EM的相對兩側,或者說,電動機EM界於主動式磁浮軸承250之間。以其中一主動式磁浮軸承250來說,其磁浮軸承定子部253具有繞組(未繪示),永磁體組251可具有數個永久磁鐵的排列。永磁體組251位於真空腔室S內且固定於轉軸130上。磁浮軸承定子部253位於真空腔室S之外且圍繞永磁體組251。更具體地,磁浮軸承定子部253為周向地配置於延伸隔離部113。永磁體組251與磁浮軸承定子部253可為連續環狀結構或是由相間隔之多個子單元所構成,本發明並非以此為限。在此配置下,可對磁浮軸承定子部253的繞組通電流以產生磁力作用於永磁體組251上,從而對轉軸130產生徑向的磁浮力,以使轉軸130維持於其所預定的旋轉中心線上,並有助於穩定或抑制轉軸130於高速旋轉時所產生的晃動。由此可知,主動式磁浮軸承250可視為是一個主動式徑向磁浮軸承。此外,可選地,至少其中一個磁浮軸承定子部253可例如直接地貼附於延伸隔離部113處的外壁面115而位於真空腔室S之外,除了有助於直接將所產生的熱經由傳導給延伸隔離部113而排除於外,還有助於縮短磁浮軸承定子部253與永磁體組251之間的距離而達到所需的磁浮力。另外,補充說明的是,只要主動式磁浮軸承250能提供轉軸130以及飛輪150於所需方向的支撐,本發明並非以主動式磁浮軸承250及其內之永久磁鐵的數量、排列、規格等為限。For example, the active
綜上所述,飛輪能量儲存系統1利用磁性軸聯器210,能以無機械接觸的方式將電動機EM的動力傳遞給真空腔室S內的轉軸130與飛輪150,並且,轉軸130與飛輪150還可透過被動式磁浮軸承190懸浮於真空腔室S中。藉此,轉軸130與飛輪150能以無接觸無摩擦的方式在真空腔室S內旋轉,免於受到電動機EM的震動影響,且還有助於維持真空腔室S的氣密度。To sum up, the flywheel
並且,值得注意的是,電動機EM的定子230雖然會因通電流而於運轉時產生高溫,但定子230被隔絕於真空腔室S之外,因此其所產生的熱能不會影響到真空腔室S內的轉軸130與飛輪150,也不會影響到被動式磁浮軸承190內的永久磁鐵。並且,基於同樣的原因,定子230得以採用在真空腔室S外的冷卻手段,可避免採用將氣冷或液冷管穿入外殼的傳統散熱手段,從而大幅降低對電動機定子散熱的困難度。Moreover, it is worth noting that although the
除此之外,電動機EM的內轉子(即外轉子213)也位於真空腔室S之外,也就是說,電動機EM完全隔絕於真空腔室S之外,因此定子230與外轉子213之間的氣隙可維持於所需的範圍之內,以讓電動機EM的定子230可以合適大小的電流即能令內轉子(即外轉子213)達到所需的轉速。In addition, the inner rotor of the motor EM (ie the outer rotor 213 ) is also located outside the vacuum chamber S, that is, the motor EM is completely isolated from the vacuum chamber S, so there is a gap between the
另一方面,主動式磁浮軸承250的磁浮軸承定子部253雖然也會因通電流而產生高溫,但磁浮軸承定子部253被隔絕於真空腔室S之外,因此其所產生的熱能也不會影響到真空腔室S內的轉軸130、飛輪150以及被動式磁浮軸承190內的永久磁鐵。On the other hand, although the magnetic
由此可知,本實施例之飛輪能量儲存系統1可在採用電動機EM及主動式磁浮軸承250的情況下,將所有會產生熱能的元件(如電動機EM之定子211以及磁浮軸承定子部253)都隔絕於真空腔室S之外,使真空腔室S成為無熱源的環境而無散熱的需求,從而避免採用傳統上會影響真空密封性的散熱手段。From this, it can be seen that the flywheel
前述僅為本發明之其中一示例性實施例,並非用於限制本發明,相關領域中具有通常知識者,自可基於前述實施例所教示之內容進行適當且合理的調整。例如,請接著參閱圖2,為本發明之另一實施例之飛輪能量儲存系統1’的平面示意圖,由於本實施例之飛輪能量儲存系統1’與圖1之飛輪能量儲存系統1的差異僅在於電動機EM’的部分,因此以下僅段落針對實施例的差異處進行說明,而相似或相同的部分可經由參閱前述相關段落獲得理解而不再贅述。The foregoing is only one exemplary embodiment of the present invention, and is not intended to limit the present invention. Those with ordinary knowledge in the relevant field can make appropriate and reasonable adjustments based on the content taught by the foregoing embodiments. For example, please refer to FIG. 2 , which is a schematic plan view of a flywheel
如圖所示,於飛輪能量儲存系統1’之電動機EM’中,定子230’與外轉子213’(即電動機EM’的內轉子)之間設有至少一被動式磁浮軸承197。被動式磁浮軸承197各包含一永磁體組1971與一永磁體組1973。永磁體組1971固定於外轉子213’朝向定子230’的外壁面上,而永磁體組1973固定於定子230’朝向外轉子213’的外壁面上,並圍繞永磁體組1971與外轉子213’。類似或相同於前述實施例之被動式磁浮軸承190,被動式磁浮軸承197之永磁體組1971與1973的位置相對應,且各自具有能與另一者相互作用的數個永久磁鐵排列,從而可如提供軸向方向的磁浮力,此磁浮力可作用於外轉子213’,可大幅減少外轉子213’對滾珠軸承270產生的重力負載。藉此,從而可大幅降低接觸式軸承於轉動時所產生的摩擦力,不僅有助於降低滾珠軸承270的損耗而提升使用壽命,還有助於降低傳遞動能的摩擦損耗而有助於提升整體效能。As shown in the figure, in the motor EM' of the flywheel energy storage system 1', at least one passive
補充說明的是,於一些情況中,永磁體組1971與1973的永久磁鐵經過合適的排列與間隔配置下,可至少產生約900至1100牛頓的磁浮力以幫助外轉子213’抵抗重力。但需聲明的是,只要能達到提供外轉子213’於所需方向的支撐,永磁體組1971與1973上相互作用的永久磁鐵可以任何已知的合適方式進行排列,其數量與規格也可依據實際需求進行調整,本發明並非以此為限。It is added that, in some cases, the permanent magnets of the permanent magnet sets 1971 and 1973 can generate at least about 900 to 1100 N of magnetic buoyancy force to help the outer rotor 213' resist gravity under proper arrangement and spacing configuration. It should be noted that, as long as the outer rotor 213' can be supported in the desired direction, the permanent magnets interacting with the
當然,基於一些實際需求,可選擇性地將主動式磁浮軸承之至少其中一者的磁浮軸承定子部改為置放於真空腔室內。舉例來說,請參閱圖3,本發明之一實施例的飛輪能量系統1’’與前述實施例之飛輪能量系統的差異可僅在於,主動式磁浮軸承250’之磁浮軸承定子部253可改為置於真空腔室S內,更具體地,磁浮軸承定子部253可例如貼附於延伸隔離部113處的內壁面114而位於真空腔室S之內。Of course, based on some practical requirements, the magnetic bearing stator part of at least one of the active magnetic bearing can be selectively placed in the vacuum chamber. For example, referring to FIG. 3 , the difference between the
在此配置下,主動式磁浮軸承250’之磁浮軸承定子部253與永磁體組251均位於真空腔室S之內,因此,磁浮軸承定子部253與永磁體組251之間不存在延伸隔離部113的實體材質且更縮短彼此之間的間隔距離,這有助於進一步增強磁浮軸承定子部253對永磁體組251所產生的磁力作用效果,從而有助於提升主動式磁浮軸承250’對轉軸130產生的徑向磁浮力。換句話說,在此主動式磁浮軸承250’的配置下,可更進一步抑制轉軸130高速旋轉時所產生的振動,從而確保轉軸130於所預定的旋轉中心線轉動。於此補充說明的是,由於磁浮軸承定子部253為直接貼附於延伸隔離部113的內壁面114,因此磁浮軸承定子部253於運轉時所產生的熱能可直接經由傳導給延伸隔離部113而排出於外。In this configuration, the magnetic
或者,也可基於一些需求選擇性地將其中一個主動式磁浮軸承改為置放於轉軸之一端、或是將一個額外的主動式磁浮軸承置放於轉軸之一端。舉例來說,請參閱圖4,本發明之一實施例的飛輪能量系統1’’’與前述實施例之飛輪能量系統的差異可僅在於,其中一組主動式磁浮軸承250改為置放於轉軸130延伸隔離部113之一端,從而改為配置於飛輪容置部111。Alternatively, based on some requirements, one of the active magnetic bearings can be selectively placed at one end of the rotating shaft, or an additional active magnetic bearing can be placed at one end of the rotating shaft. For example, referring to FIG. 4 , the difference between the
飛輪容置部111中可用於配置主動式磁浮軸承250的區域較為充裕,有助於主動式磁浮軸承250進一步依據如尺寸或規格相關等需求進行調整。並且,在此配置下,主動式磁浮軸承250的控制可直接針對轉軸130的相對兩端處進行到控制,並且,由於其中一主動式磁浮軸承250配置於轉軸130較靠近飛輪150的區域,使得飛輪150延軸向方向的相對兩側處都可經由轉軸130接受到主動式磁浮軸承250的徑向磁浮力,從而,有助於更進一步降低飛輪150對整體動件的轉動穩定性的影響。除此之外,可選地,主動式磁浮軸承250之磁浮軸承定子部253可直接貼附於飛輪容置部111處的內壁面114,或是直接嵌設於飛輪容置部111的實體部分,使得磁浮軸承定子部253於運轉時所產生的熱能可直接經由傳導給飛輪容置部111而排出於外。The area in the
綜上所述,本發明實施例所揭露的飛輪能量儲存系統中,由於電動機之轉子同時作為磁性軸聯器的外轉子以驅動真空腔室內與轉軸固定之內轉子,從而能實現無機械接觸的方式驅動轉軸與飛輪,以讓轉軸與飛輪能在無阻力的情況下旋轉。To sum up, in the flywheel energy storage system disclosed in the embodiments of the present invention, since the rotor of the electric motor simultaneously acts as the outer rotor of the magnetic coupling to drive the inner rotor fixed to the rotating shaft in the vacuum chamber, it is possible to realize the mechanical contactless system. The shaft and the flywheel are driven in such a way that the shaft and the flywheel can rotate without resistance.
並且,電動機上通電流生熱的定子被排除於真空腔室之外,此配置能使飛輪能量儲存系統將運轉時主要產生熱能的元件隔絕於真空腔室之外,使飛輪能量儲存系統避免採用傳統上會影響真空密封性的散熱手段,從而有助於確保飛輪運轉所需的氣密性。In addition, the stator of the electric motor that generates heat through current is excluded from the vacuum chamber. This configuration enables the flywheel energy storage system to isolate the components that mainly generate heat energy during operation from the vacuum chamber, so that the flywheel energy storage system can avoid the use of Heat dissipation, which traditionally affects vacuum tightness, helps ensure the air tightness required for flywheel operation.
可選地,也可將主動式磁浮軸承之磁浮軸承定子部一併地排除於真空腔室之外,在此情況下,飛輪能量儲存系統之電動機的定子與主動式磁浮軸承之磁浮軸承定子部均位於真空腔室之外,使得飛輪能量儲存系統可在同時採用電動機及主動式磁浮軸承的情況下,確實地將會產生熱能的元件都隔絕於真空腔室之外,使真空腔室成為無熱源的環境而無散熱的需求。Optionally, the magnetic bearing stator part of the active magnetic bearing can also be excluded from the vacuum chamber together. In this case, the stator of the motor of the flywheel energy storage system and the magnetic bearing stator part of the active magnetic bearing All are located outside the vacuum chamber, so that the flywheel energy storage system can use the motor and the active magnetic bearing at the same time. The environment of the heat source without the need for heat dissipation.
當然,為了達到進一步提升主動式磁浮軸承對轉軸的徑向磁浮力等一些實際需求,主動式磁浮軸承之磁浮軸承定子部也可配置於真空腔室內以避免主動式磁浮軸承之磁浮軸承定子部與永磁體組之間存在實體材質。且在此配置下,可藉由將主動式磁浮軸承250’之磁浮軸承定子部253直接貼附於外殼的內壁面的方式,直接地將磁浮軸承定子部所產生的熱能傳導而排出於外,因而可在達到提升徑向磁浮效果的同時,避免熱能對運轉產生的影響。Of course, in order to further improve the radial magnetic levitation force of the active magnetic bearing on the rotating shaft and other practical requirements, the magnetic bearing stator part of the active magnetic bearing can also be arranged in the vacuum chamber to avoid the magnetic bearing stator part of the active magnetic bearing and the magnetic levitation bearing. Solid materials exist between groups of permanent magnets. And under this configuration, by directly adhering the magnetic
除此之外,本發明實施例之飛輪能量系統中可選擇性地於動件處設置被動式磁浮軸承,例如可在轉軸之一端、相對兩端或是任何所需的位置處、或是在電動機之定子與轉子之間,從而對所施用的動件提供特定方向的磁浮力,以助於穩定動件的轉動運動及降低摩擦阻力,還有助於減低動件對接觸式軸承所產生的負載,從而可在將動能傳遞損耗的同時,延長軸承的使用壽命。In addition, in the flywheel energy system of the embodiment of the present invention, a passive magnetic bearing can be selectively disposed at the moving element, for example, at one end of the rotating shaft, opposite ends or at any desired position, or at the motor between the stator and the rotor, so as to provide a magnetic levitation force in a specific direction to the applied moving parts, so as to help stabilize the rotational motion of the moving parts and reduce frictional resistance, and also help reduce the load generated by the moving parts on the contact bearing. , so that the kinetic energy can be transmitted and lost, and the service life of the bearing can be extended.
雖然本發明以前述之實施例揭露如上,然其並非用以限定本發明。在不脫離本發明之精神和範圍內,所為之更動與潤飾,均屬本發明之專利保護範圍。關於本發明所界定之保護範圍請參考所附之申請專利範圍。Although the present invention is disclosed in the foregoing embodiments, it is not intended to limit the present invention. Changes and modifications made without departing from the spirit and scope of the present invention belong to the scope of patent protection of the present invention. For the protection scope defined by the present invention, please refer to the attached patent application scope.
1, 1’, 1’’, 1’’’:飛輪能量儲存系統
10:飛輪模組
20:驅動模組
110:外殼
111:飛輪容置部
113:延伸隔離部
114:內壁面
115:外壁面
130:轉軸
131:外環部
150:飛輪
190:被動式磁浮軸承
191, 193, 251, 1971, 1973:永磁體組
195:輔助軸承
197:被動式磁浮軸承
205:安裝座
210, 210’:磁性軸聯器
211, 211’:內轉子
213, 213’:外轉子
230, 230’:定子
250, 250’:主動式磁浮軸承
253:磁浮軸承定子部
270:滾珠軸承
2111:內轉子磁鐵座
2112, 2132:永久磁石
2131:外轉子磁鐵座
EM, EM’:電動機
S:真空腔室
1, 1’, 1’’, 1’’’: Flywheel energy storage system
10: Flywheel module
20: Driver module
110: Shell
111: Flywheel accommodating part
113: Extension Separator
114: inner wall surface
115: Outer wall
130: Spindle
131: Outer Ring Department
150: Flywheel
190: Passive
圖1係為依據本發明之一實施例之飛輪能量儲存系統的平面示意圖。 圖2係為依據本發明之另一實施例之飛輪能量儲存系統的平面示意圖。 圖3係為依據本發明之又一實施例之飛輪能量儲存系統的平面示意圖。 圖4係為依據本發明之再一實施例之飛輪能量儲存系統的平面示意圖。 FIG. 1 is a schematic plan view of a flywheel energy storage system according to an embodiment of the present invention. 2 is a schematic plan view of a flywheel energy storage system according to another embodiment of the present invention. 3 is a schematic plan view of a flywheel energy storage system according to yet another embodiment of the present invention. 4 is a schematic plan view of a flywheel energy storage system according to still another embodiment of the present invention.
1:飛輪能量儲存系統 1: Flywheel energy storage system
10:飛輪模組 10: Flywheel module
20:驅動模組 20: Driver module
110:外殼 110: Shell
111:飛輪容置部 111: Flywheel accommodating part
113:延伸隔離部 113: Extension Separator
130:轉軸 130: Spindle
131:外環部 131: Outer Ring Department
150:飛輪 150: Flywheel
190:被動式磁浮軸承 190: Passive Magnetic Bearings
191,193,251:永磁體組 191, 193, 251: Permanent Magnet Sets
195:輔助軸承 195: Auxiliary bearing
205:安裝座 205: Mounting Seat
210:磁性軸聯器 210: Magnetic coupling
211:內轉子 211: inner rotor
213:外轉子 213: Outer rotor
230:定子 230: Stator
250:主動式磁浮軸承 250: Active Magnetic Bearing
253:磁浮軸承定子部 253: Magnetic bearing stator part
270:滾珠軸承 270: Ball bearing
2111:內轉子磁鐵座 2111: Inner rotor magnet holder
2112,2132:永久磁石 2112, 2132: Permanent Magnets
2131:外轉子磁鐵座 2131: Outer rotor magnet holder
EM:電動機 EM: electric motor
S:真空腔室 S: Vacuum chamber
Claims (13)
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CN115360849A (en) * | 2022-10-21 | 2022-11-18 | 华驰动能(北京)科技有限公司 | Flywheel energy storage system |
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TWM433021U (en) * | 2012-01-03 | 2012-07-01 | Cai Chang-Cheng | The energy storage flywheel device |
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TW202018182A (en) * | 2018-11-07 | 2020-05-16 | 財團法人工業技術研究院 | Flywheel power storage system |
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US20140026552A1 (en) * | 2011-04-07 | 2014-01-30 | Kobelco Construction Machinery Co., Ltd. | Hybrid construction machine |
US20140366684A1 (en) * | 2011-05-23 | 2014-12-18 | Active Power, Inc | Insulation system for prevention of corona discharge |
TWM433021U (en) * | 2012-01-03 | 2012-07-01 | Cai Chang-Cheng | The energy storage flywheel device |
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TW202018182A (en) * | 2018-11-07 | 2020-05-16 | 財團法人工業技術研究院 | Flywheel power storage system |
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