CN113241890B - Flywheel falling protection structure and energy storage system - Google Patents
Flywheel falling protection structure and energy storage system Download PDFInfo
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- CN113241890B CN113241890B CN202110606125.9A CN202110606125A CN113241890B CN 113241890 B CN113241890 B CN 113241890B CN 202110606125 A CN202110606125 A CN 202110606125A CN 113241890 B CN113241890 B CN 113241890B
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- 238000004146 energy storage Methods 0.000 title claims abstract description 13
- 239000010687 lubricating oil Substances 0.000 claims description 10
- 229910000897 Babbitt (metal) Inorganic materials 0.000 claims description 6
- 239000011159 matrix material Substances 0.000 description 3
- 230000003139 buffering effect Effects 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000001050 lubricating effect Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000002457 bidirectional effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 238000000053 physical method Methods 0.000 description 1
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K5/00—Casings; Enclosures; Supports
- H02K5/24—Casings; Enclosures; Supports specially adapted for suppression or reduction of noise or vibrations
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
- H02K7/02—Additional mass for increasing inertia, e.g. flywheels
- H02K7/025—Additional mass for increasing inertia, e.g. flywheels for power storage
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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
- 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
Description
技术领域technical field
本发明涉及飞轮储能系统技术领域,具体涉及一种飞轮跌落保护结构及储能系统。The invention relates to the technical field of flywheel energy storage systems, in particular to a flywheel drop protection structure and an energy storage system.
背景技术Background technique
飞轮储能系统是一种机电能量转换的储能装置。该系统采用物理方法进行储能,并通过电动/发电互逆式双向电机实现电能与高速运转飞轮的机械动能之间的相互转换和储存。The flywheel energy storage system is an energy storage device for electromechanical energy conversion. The system uses physical methods to store energy, and realizes the mutual conversion and storage of electrical energy and the mechanical kinetic energy of the high-speed flywheel through the motor/generator reciprocal bidirectional motor.
现有技术中的飞轮储能系统主要包括,飞轮、轴承、电机/发电机、电力转换器和真空室等组件构成,运行时,电机通过轴承驱动飞轮在真空室内转动。但是,如果遇到突然断电或者轴系失稳等突发状况,可能会引起飞轮跌落,若此时飞轮与真空室的壳体发生直接摩擦,较高的相对速度很有可能导致飞轮和壳体的损坏。The flywheel energy storage system in the prior art mainly includes components such as flywheel, bearing, motor/generator, power converter and vacuum chamber. During operation, the motor drives the flywheel to rotate in the vacuum chamber through the bearing. However, in the event of a sudden power failure or shaft system instability, the flywheel may fall. If the flywheel and the shell of the vacuum chamber are directly rubbed at this time, the high relative speed is likely to cause the flywheel and the shell to fall. body damage.
发明内容SUMMARY OF THE INVENTION
因此,本发明要解决的技术问题在于克服现有技术中的飞轮储能系统中遇到突然断电或者轴系失稳等突发状况,可能会引起飞轮跌落,导致飞轮与真空室的壳体发生直接摩擦,最终使飞轮和壳体损坏的缺陷,从而提供一种飞轮跌落保护结构及储能系统。Therefore, the technical problem to be solved by the present invention is to overcome the sudden power failure or shaft system instability encountered in the flywheel energy storage system in the prior art, which may cause the flywheel to fall, resulting in the flywheel and the shell of the vacuum chamber. Direct friction occurs, and eventually the flywheel and the housing are damaged, thereby providing a flywheel drop protection structure and an energy storage system.
为解决上述技术问题,本发明的技术方案如下:For solving the above-mentioned technical problems, the technical scheme of the present invention is as follows:
一种飞轮跌落保护结构,包括,飞轮,其下端面凸设有摩擦限位端;防撞结构,位于所述飞轮的下方,其上设有与所述摩擦限位端正对设置的减摩件,所述减摩件朝向所述摩擦限位端的一面为曲面。A flywheel fall protection structure, comprising: a flywheel, the lower end face of which is protruded with a friction limit end; an anti-collision structure is located below the flywheel, on which is provided with a friction reducing part opposite to the friction limit end , the surface of the friction reducing member facing the friction limiting end is a curved surface.
进一步地,所述减摩件为巴氏合金。Further, the friction reducing member is a babbitt alloy.
进一步地,所述防撞结构还包括安装座,所述安装座上设有开口朝向所述摩擦限位端方向设置的容纳槽,所述减摩件置于所述容纳槽内。Further, the anti-collision structure further includes a mounting seat, the mounting seat is provided with an accommodating groove with an opening facing the direction of the friction limit end, and the anti-friction member is placed in the accommodating groove.
进一步地,所述摩擦限位端伸进所述容纳槽的开口内,且与所述容纳槽的侧壁之间具有间隙。Further, the friction limit end extends into the opening of the accommodating groove and has a gap with the side wall of the accommodating groove.
进一步地,所述曲面为具有凹陷区的凹凸起伏面。Further, the curved surface is a concave-convex surface with a concave area.
进一步地,所述凹凸起伏面的凹陷区上存放有润滑油。Further, lubricating oil is stored on the concave area of the convex and concave surface.
进一步地,所述摩擦限位端呈圆环形且与所述飞轮同轴设置。Further, the friction limit end is in the shape of a circular ring and is coaxially arranged with the flywheel.
进一步地,所述容纳槽呈圆环形且与所述飞轮同轴设置。Further, the accommodating groove is annular and arranged coaxially with the flywheel.
进一步地,所述减摩件呈圆环形且与所述飞轮同轴设置。Further, the anti-friction member is in the shape of an annular shape and is arranged coaxially with the flywheel.
一种飞轮储能系统,包括上述所述的飞轮跌落保护结构。A flywheel energy storage system includes the flywheel drop protection structure described above.
本发明技术方案,具有如下优点:The technical scheme of the present invention has the following advantages:
1.本发明提供的飞轮跌落保护结构,当飞轮跌落后,飞轮下端面设置的摩擦限位端与飞轮下方的减摩件接触,避免飞轮直接与壳体发生摩擦,从而保护飞轮和壳体不受损坏;而且减摩件与摩擦限位端的接触面为曲面,曲面凸起的部分可先与摩擦限位端接触并发生摩擦,对于飞轮的撞击可以起到缓冲作用,从而更好的保护飞轮。1. In the flywheel fall protection structure provided by the present invention, when the flywheel falls, the friction limiting end provided on the lower end face of the flywheel contacts with the anti-friction part below the flywheel, preventing the flywheel from directly rubbing with the housing, thereby protecting the flywheel and the housing from being damaged. Damaged; and the contact surface between the anti-friction part and the friction limit end is a curved surface, and the convex part of the curved surface can contact the friction limit end first and generate friction, which can buffer the impact of the flywheel, so as to better protect the flywheel. .
附图说明Description of drawings
为了更清楚地说明本发明具体实施方式或现有技术中的技术方案,下面将对具体实施方式或现有技术描述中所需要使用的附图作简单地介绍,显而易见地,下面描述中的附图是本发明的一些实施方式,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其他的附图。In order to illustrate the specific embodiments of the present invention or the technical solutions in the prior art more clearly, the following briefly introduces the accompanying drawings that need to be used in the description of the specific embodiments or the prior art. Obviously, the accompanying drawings in the following description The drawings are some embodiments of the present invention. For those of ordinary skill in the art, other drawings can also be obtained based on these drawings without creative efforts.
图1为本发明一个实施例中的飞轮跌落保护结构的示意图;1 is a schematic diagram of a flywheel drop protection structure in an embodiment of the present invention;
图2为图1中的安装座的俯视图;Fig. 2 is the top view of the mounting seat in Fig. 1;
图3为图1中的安装座的放大示意图。FIG. 3 is an enlarged schematic view of the mounting seat in FIG. 1 .
附图标记说明:Description of reference numbers:
1、飞轮; 2、摩擦限位端; 3、安装座;1. Flywheel; 2. Friction limit end; 3. Mounting seat;
4、减摩件; 5、润滑油; 6、容纳槽。4. Anti-friction parts; 5. Lubricating oil; 6. Accommodating groove.
具体实施方式Detailed ways
下面将结合附图对本发明的技术方案进行清楚、完整地描述,显然,所描述的实施例是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。The technical solutions of the present invention will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are a part of the embodiments of the present invention, but not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.
在本发明的描述中,需要说明的是,术语“中心”、“上”、“下”、“左”、“右”、“竖直”、“水平”、“内”、“外”等指示的方位或位置关系为基于附图所示的方位或位置关系,仅是为了便于描述本发明和简化描述,而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作,因此不能理解为对本发明的限制。此外,术语“第一”、“第二”、“第三”仅用于描述目的,而不能理解为指示或暗示相对重要性。In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. The indicated orientation or positional relationship is based on the orientation or positional relationship shown in the accompanying drawings, which is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the indicated device or element must have a specific orientation or a specific orientation. construction and operation, and therefore should not be construed as limiting the invention. Furthermore, the terms "first", "second", and "third" are used for descriptive purposes only and should not be construed to indicate or imply relative importance.
在本发明的描述中,需要说明的是,除非另有明确的规定和限定,术语“安装”、“相连”、“连接”应做广义理解,例如,可以是固定连接,也可以是可拆卸连接,或一体地连接;可以是机械连接,也可以是电连接;可以是直接相连,也可以通过中间媒介间接相连,可以是两个元件内部的连通。对于本领域的普通技术人员而言,可以具体情况理解上述术语在本发明中的具体含义。In the description of the present invention, it should be noted that the terms "installed", "connected" and "connected" should be understood in a broad sense, unless otherwise expressly specified and limited, for example, it may be a fixed connection or a detachable connection Connection, or integral connection; can be mechanical connection, can also be electrical connection; can be directly connected, can also be indirectly connected through an intermediate medium, can be internal communication between two elements. For those of ordinary skill in the art, the specific meanings of the above terms in the present invention can be understood in specific situations.
此外,下面所描述的本发明不同实施方式中所涉及的技术特征只要彼此之间未构成冲突就可以相互结合。In addition, the technical features involved in the different embodiments of the present invention described below can be combined with each other as long as they do not conflict with each other.
图1为本发明一个实施例中的飞轮跌落保护结构的示意图;如图1所示,本实施例提供一种飞轮跌落保护结构,包括,飞轮1,其下端面凸设有摩擦限位端2;防撞结构,位于飞轮1的下方,其上设有与摩擦限位端2正对设置的减摩件4,减摩件4朝向摩擦限位端2的一面为曲面。FIG. 1 is a schematic diagram of a flywheel drop protection structure in an embodiment of the present invention; as shown in FIG. 1 , the present embodiment provides a flywheel drop protection structure, including a
具体的,其中,摩擦限位端2可以为柱状结构,多根柱状对称分布在飞轮1的转轴的两侧,摩擦限位端2也可以为环状结构,摩擦限位端2的延伸方向与飞轮1的转轴的延伸方向保持一致。其中,防撞结构的主体可以平板状结构,也可以为带沟槽的平板状结构。其中,减摩件4可以粘接在防撞结构朝向飞轮1的一面,减摩件4与摩擦限位端2的下端面相对齐设置,使得飞轮1跌落后,减摩件4与摩擦限位端2可以更好的接触。其中,减摩件4的硬度可以小于摩擦限位端2的硬度,这样在摩擦时可以通过磨损减摩件4而保护摩擦限位端2。减摩件4朝向摩擦限位端2的一面设置呈曲面结构,曲面凸起的部分可先与摩擦限位端接触并发生摩擦,对于飞轮1的撞击可以起到缓冲作用,从而更好的保护飞轮1。Specifically, the
本发明提供的飞轮跌落保护结构,当飞轮1跌落后,飞轮1下端面设置的摩擦限位端2与飞轮1下方的减摩件4接触,避免飞轮1直接与壳体发生摩擦,从而保护飞轮1和壳体不受损坏;而且减摩件4与摩擦限位端2的接触面为曲面,曲面凸起的部分可先与摩擦限位端接触并发生摩擦,对于飞轮1的撞击可以起到缓冲作用,从而更好的保护飞轮1。In the flywheel drop protection structure provided by the present invention, when the
本实施例中,减摩件4为巴氏合金。巴氏合金的特点是在软相基体上均匀分布着硬相质点,软相基体使巴氏合金具有非常好的嵌藏性、顺应性和抗咬合性,并在磨合后,软基体内凹,硬质点外凸,使滑动面之间形成微小间隙,成为贮油空间和润滑油通道,利于减摩。如此设置,由巴氏合金制成的减摩件4质地软,可以减小飞轮1的损伤。In this embodiment, the
图2为图1中的安装座的俯视图;如图2所示,本实施例中,防撞结构还包括安装座3,安装座3上设有开口朝向摩擦限位端2方向设置的容纳槽6,减摩件4置于容纳槽6内。其中,该安装座3可以为环形板,飞轮1的转轴从安装座3的中间通孔内穿过。安装座3远离转轴的外侧可以粘接或者焊接在壳体的内壁。其中,当摩擦限位端2呈圆环形且与飞轮1同轴设置时,对应的,容纳槽6呈圆环形且与飞轮1同轴设置,对应的,减摩件4呈圆环形且与飞轮1同轴设置。其中,摩擦限位端2可以略微伸进容纳槽6的开口内,且与容纳槽6的侧壁之间具有间隙,摩擦限位端2的高度不小于容纳槽6的深度,以免飞轮1上除了摩擦限位端2之外的其他位置与容纳槽6接触发生磨损。FIG. 2 is a top view of the mounting seat in FIG. 1 ; as shown in FIG. 2 , in this embodiment, the anti-collision structure further includes a mounting
图3为图1中的安装座的放大示意图,如图3所示,本实施例中,曲面为具有凹陷区的凹凸起伏面。凹凸起伏面的凹陷区上存放有润滑油5。其中,润滑油5可以起到一定的润滑作用,减小飞轮1跌落后与减摩件4之间的摩擦力,从而减小损伤。而且,如果减摩件4为光面结构,则摩擦限位端2与减摩件4之间的接触面无法存储较多的润滑油5,而减摩件4如果具有凹陷区,则可以容纳更多润滑油5,使摩擦限位端2与减摩件4的接触面能够保有一定量的润滑油5,有利于提高润滑效果。FIG. 3 is an enlarged schematic view of the mounting seat in FIG. 1 . As shown in FIG. 3 , in this embodiment, the curved surface is a concave-convex surface with a concave area. Lubricating
一种飞轮储能系统,包括上述的飞轮跌落保护结构。A flywheel energy storage system includes the above-mentioned flywheel drop protection structure.
使用时,遇到突然断电或者轴系失稳等突发状况,引起飞轮1跌落时,飞轮1上的摩擦限位端2落入容纳槽6内,摩擦限位端2与容纳槽6内的减摩件4发生摩擦,由巴氏合金制成的减摩件4质地软,一方面可以起到一定的缓冲作用,另一方面在润滑油5的作用下可以减小飞轮1的磨损,从而避免飞轮1与壳体发生直接摩擦,以起到保护飞轮1的目的。During use, in the event of a sudden power failure or shaft system instability and other emergencies, when the
显然,上述实施例仅仅是为清楚地说明所作的举例,而并非对实施方式的限定。对于所属领域的普通技术人员来说,在上述说明的基础上还可以做出其它不同形式的变化或变动。这里无需也无法对所有的实施方式予以穷举。而由此所引伸出的显而易见的变化或变动仍处于本发明创造的保护范围之中。Obviously, the above-mentioned embodiments are only examples for clear description, and are not intended to limit the implementation manner. For those of ordinary skill in the art, changes or modifications in other different forms can also be made on the basis of the above description. There is no need and cannot be exhaustive of all implementations here. And the obvious changes or changes derived from this are still within the protection scope of the present invention.
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CN113241890A (en) | 2021-08-10 |
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