CN114810260B - Gravity energy storage system with buffering effect - Google Patents
Gravity energy storage system with buffering effect Download PDFInfo
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- 230000005484 gravity Effects 0.000 title claims abstract description 97
- 238000004146 energy storage Methods 0.000 title claims abstract description 24
- 230000003139 buffering effect Effects 0.000 title claims abstract description 18
- 238000007789 sealing Methods 0.000 claims abstract description 49
- 238000005338 heat storage Methods 0.000 claims abstract description 20
- 239000011232 storage material Substances 0.000 claims abstract description 20
- 238000003491 array Methods 0.000 claims abstract description 13
- 230000005672 electromagnetic field Effects 0.000 claims abstract description 12
- 238000004891 communication Methods 0.000 claims description 25
- 238000009423 ventilation Methods 0.000 claims description 25
- 238000002955 isolation Methods 0.000 claims description 10
- 239000012530 fluid Substances 0.000 claims description 9
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- 238000000034 method Methods 0.000 description 11
- 230000008569 process Effects 0.000 description 8
- 238000010586 diagram Methods 0.000 description 3
- 238000007906 compression Methods 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
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- 238000005381 potential energy Methods 0.000 description 2
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01K—STEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
- F01K27/00—Plants for converting heat or fluid energy into mechanical energy, not otherwise provided for
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03G—SPRING, WEIGHT, INERTIA OR LIKE MOTORS; MECHANICAL-POWER PRODUCING DEVICES OR MECHANISMS, NOT OTHERWISE PROVIDED FOR OR USING ENERGY SOURCES NOT OTHERWISE PROVIDED FOR
- F03G3/00—Other motors, e.g. gravity or inertia motors
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B41/00—Pumping installations or systems specially adapted for elastic fluids
- F04B41/02—Pumping installations or systems specially adapted for elastic fluids having reservoirs
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D20/00—Heat storage plants or apparatus in general; Regenerative heat-exchange apparatus not covered by groups F28D17/00 or F28D19/00
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J15/00—Systems for storing electric energy
- H02J15/006—Systems for storing electric energy in the form of pneumatic energy, e.g. compressed air energy storage [CAES]
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J15/00—Systems for storing electric energy
- H02J15/007—Systems for storing electric energy involving storage in the form of mechanical energy, e.g. fly-wheels
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Abstract
Description
技术领域technical field
本申请涉及电能存储技术领域,尤其涉及一种具有缓冲作用的重力储能系统。The present application relates to the technical field of electrical energy storage, and in particular, to a gravity energy storage system with a buffering effect.
背景技术Background technique
重力压缩空气储能是通过在竖井中设置重力块,重力块与竖井之间通过密封膜密封连接,位于重力块下方的竖井中形成密封的储气腔,用于高压气体的存储,通过将空气进行压缩后通入储气腔中,重力块向上移动,将压缩空气的能量部分转化为重力块的重力势能进行存储,在储能过程中压缩空气产生的热能通常是通过设置热交换单元进行热量的存储,但是热交换单元的设置使得储能系统复杂,并且在出现紧急情况时,重力块不受控向下加速运动会对竖井下方造成较大撞击。Gravity compressed air energy storage is to set a gravity block in the shaft, the gravity block and the shaft are sealed and connected by a sealing film, and a sealed air storage cavity is formed in the shaft under the gravity block for the storage of high-pressure gas. After being compressed, it is passed into the air storage chamber, and the gravity block moves upward, converting the energy of the compressed air into the gravitational potential energy of the gravity block for storage. During the energy storage process, the heat energy generated by the compressed air is usually heated by setting a heat exchange unit. However, the setting of the heat exchange unit makes the energy storage system complicated, and in the event of an emergency, the uncontrolled downward acceleration of the gravity block will cause a greater impact below the shaft.
发明内容SUMMARY OF THE INVENTION
本申请旨在至少在一定程度上解决相关技术中的技术问题之一。The present application aims to solve one of the technical problems in the related art at least to a certain extent.
为此,本申请的目的在于提出一种具有缓冲作用的重力储能系统,通过在竖井内壁和重力块外壁对应缠绕有导线圈阵列,通过电源给竖井内壁上的线圈阵列施加固定频率的交流电,产生向上的电磁力使在发生紧急情况时,重力块不受控向下加速运动,激发竖井内壁线圈电源快速启动供电并形成电磁场,在重力块外壁上的线圈中感应出反向电磁场,从而使重力块快速减速,减小坠落时对竖井下方的撞击动能,并且重力块中填充的蓄热材料,通过蓄热材料直接能够进行热交换,无需另外布置换热单元。For this reason, the purpose of this application is to propose a gravity energy storage system with a buffering effect, by correspondingly winding a conducting coil array on the inner wall of the shaft and the outer wall of the gravity block, and applying alternating current of a fixed frequency to the coil array on the inner wall of the shaft through a power supply, The upward electromagnetic force is generated, so that in the event of an emergency, the gravity block accelerates downward uncontrollably, and the coil power supply on the inner wall of the shaft is excited to quickly start the power supply and form an electromagnetic field, and a reverse electromagnetic field is induced in the coil on the outer wall of the gravity block, so that the The gravity block decelerates quickly, reducing the kinetic energy of the impact on the bottom of the shaft when it falls, and the heat storage material filled in the gravity block can directly exchange heat through the heat storage material, without the need for additional heat exchange units.
为达到上述目的,本申请提出的一种具有缓冲作用的重力储能系统,包括竖井;In order to achieve the above purpose, a gravity energy storage system with buffering function proposed in the present application includes a shaft;
所述竖井中活动插接有重力块,所述重力块与所述竖井侧壁之间通过密封膜密封连接,所述重力块、所述密封膜和所述竖井位于所述密封膜下方的空间之间围成储气腔;A gravity block is movably inserted into the shaft, the gravity block and the side wall of the shaft are sealed and connected by a sealing film, and the gravity block, the sealing film and the shaft are located in the space below the sealing film A gas storage cavity is enclosed between;
所述重力块包括壳体和填充在所述壳体中的蓄热材料,所述壳体底部设置有与所述储气腔相连通的第一通气孔,所述壳体顶部连接有空气压缩机组和空气膨胀机组;The gravity block includes a casing and a heat storage material filled in the casing, the bottom of the casing is provided with a first ventilation hole that communicates with the air storage cavity, and the top of the casing is connected with an air compression Units and air expansion units;
所述竖井内壁和所述壳体外壁对应缠绕有导线圈阵列,所述竖井内壁上的导线圈阵列按顺序与不同的电源连接,所述壳体外壁的各个导线圈自成闭路,以通过所述电源给所述竖井内壁上的导线圈阵列施加固定频率的交流电,在所述壳体外壁上的导线圈阵列中感应出反向环流,以使两组相反电流方向导线圈阵列形成反向的电磁场后,通过电磁力对所述重力块施加向上的作用力。The inner wall of the shaft and the outer wall of the casing are correspondingly wound with an array of conducting coils, the arrays of conducting coils on the inner wall of the shaft are connected to different power sources in sequence, and each conducting coil on the outer wall of the casing forms a closed circuit by itself, so as to pass through all the coils. The power supply applies alternating current of a fixed frequency to the conducting coil array on the inner wall of the shaft, and a reverse circulating current is induced in the conducting coil array on the outer wall of the casing, so that two sets of conducting coil arrays with opposite current directions form an opposite direction. After the electromagnetic field, an upward force is applied to the gravity block through electromagnetic force.
进一步地,所述壳体顶部设置有两个第二通气孔,两个所述第二通气孔处均设置有阀门,两个所述阀门分别连接有进气通道和出气通道,所述进气通道和所述出气通道分别连接所述空气压缩机组和所述空气膨胀机组。Further, the top of the casing is provided with two second ventilation holes, both of which are provided with valves, and the two valves are respectively connected with an air inlet channel and an air outlet channel. The passage and the air outlet passage are respectively connected to the air compressor unit and the air expansion unit.
进一步地,所述第一通气孔和所述第二通气孔处均设置有隔离网,以通过所述隔离网对所述蓄热材料进行阻挡。Further, isolation nets are provided at the first ventilation holes and the second ventilation holes, so as to block the heat storage material through the isolation nets.
进一步地,所述竖井的底部侧壁开有多个连通腔,所述连通腔的底部设置有压力缸;Further, a plurality of communication cavities are opened on the bottom side wall of the vertical shaft, and a pressure cylinder is provided at the bottom of the communication cavities;
所述连通腔中设置有杠杆,所述杠杆的一端铰接有曲柄,另一端位于所述重力块的下方;A lever is arranged in the communication cavity, one end of the lever is hinged with a crank, and the other end is located below the gravity block;
所述曲柄的底端连接有活塞,所述活塞活动插接在所述压力缸中,所述活塞与所述压力缸之间密封,所述活塞下方的所述压力缸中形成密封腔,所述密封腔中填充有可压缩气体,以通过向所述储气腔中通入气体带动所述活塞向下移动,使得所述杠杆一端向上升起对所述重力块提供向上的辅助力。The bottom end of the crank is connected with a piston, the piston is movably inserted into the pressure cylinder, the piston and the pressure cylinder are sealed, and a sealing cavity is formed in the pressure cylinder below the piston, so The sealed cavity is filled with compressible gas, so that the piston is moved downward by passing gas into the gas storage cavity, so that one end of the lever is lifted upward to provide an upward auxiliary force to the gravity block.
进一步地,所述活塞上方的所述压力缸中灌充有粘性压力液,以通过所述粘性压力液实现所述活塞和所述压力缸之间的密封。Further, the pressure cylinder above the piston is filled with viscous pressure fluid, so as to realize the sealing between the piston and the pressure cylinder through the viscous pressure fluid.
进一步地,所述连通腔中设置有支座,所述杠杆安装在所述支座上。Further, a support is provided in the communication cavity, and the lever is mounted on the support.
进一步地,所述壳体的底端侧壁开有延伸至底面的容纳槽,所述杠杆的一端伸入所述容纳槽中。Further, an accommodating groove extending to the bottom surface is formed on the side wall of the bottom end of the casing, and one end of the lever extends into the accommodating groove.
进一步地,所述连通腔设置有多个,多个所述连通腔中的杠杆等角度设置在所述壳体周侧,每个所述连通腔中均设置有所述压力缸。Further, there are a plurality of the communication chambers, the levers in the plurality of communication chambers are equiangularly arranged on the peripheral side of the casing, and each of the communication chambers is provided with the pressure cylinder.
进一步地,所述竖井为圆柱筒状结构;Further, the shaft is a cylindrical tubular structure;
所述壳体为圆柱状结构,所述壳体的外壁面周侧设置有多个呈竖直分布的平滑凹槽;The casing is a cylindrical structure, and a plurality of vertically distributed smooth grooves are arranged on the peripheral side of the outer wall surface of the casing;
所述密封膜为套设在所述壳体外部的环形筒状结构,所述密封膜的外径等于所述竖井的内径,所述密封膜从中间将上部向内翻折后形成外环和内环连接组成的环形鞍面结构,翻折后得到的所述内环周侧形成褶皱凸起,所述外环的底端与所述竖井内壁密封连接,所述内环的底端与所述壳体的外壁密封连接,所述褶皱凸起与所述平滑凹槽贴合。The sealing film is an annular cylindrical structure sleeved on the outside of the casing, the outer diameter of the sealing film is equal to the inner diameter of the vertical shaft, and the sealing film is folded from the middle to form the outer ring and the upper part. The annular saddle surface structure formed by the connection of the inner ring, the inner ring obtained after folding is formed into a folded protrusion, the bottom end of the outer ring is sealed with the inner wall of the shaft, and the bottom end of the inner ring is connected to the inner wall of the shaft. The outer walls of the casing are sealed and connected, and the corrugated protrusions fit with the smooth grooves.
进一步地,所述密封膜的环形筒状结构为上下等径的圆柱面结构。Further, the annular cylindrical structure of the sealing film is a cylindrical surface structure with equal diameters up and down.
本申请附加的方面和优点将在下面的描述中部分给出,部分将从下面的描述中变得明显,或通过本申请的实践了解到。Additional aspects and advantages of the present application will be set forth, in part, in the following description, and in part will be apparent from the following description, or learned by practice of the present application.
附图说明Description of drawings
本申请上述的和/或附加的方面和优点从下面结合附图对实施例的描述中将变得明显和容易理解,其中:The above and/or additional aspects and advantages of the present application will become apparent and readily understood from the following description of embodiments taken in conjunction with the accompanying drawings, wherein:
图1是本申请一实施例提出的具有缓冲作用的重力储能系统的局部结构示意图;FIG. 1 is a schematic diagram of a partial structure of a gravity energy storage system with a buffering effect proposed in an embodiment of the present application;
图2是本申请具有缓冲作用的重力储能系统的局部结构示意图。FIG. 2 is a partial structural schematic diagram of the gravity energy storage system with buffering effect of the present application.
图中,1、竖井;11、储气腔;12、连通腔;13、压力缸;14、密封腔;15、粘性压力液;2、重力块;21、壳体;22、蓄热材料;23、第一通气孔;24、第二通气孔;25、隔离网;26、容纳槽;27、平滑凹槽;28、第三通气孔;3、密封膜;31、外环;32、内环;4、空气压缩机组;5、空气膨胀机组;6、杠杆;7、曲柄;8、活塞;9、支座。In the figure, 1, shaft; 11, air storage chamber; 12, communication chamber; 13, pressure cylinder; 14, sealing chamber; 15, viscous pressure fluid; 2, gravity block; 21, shell; 22, heat storage material; 23, the first vent hole; 24, the second vent hole; 25, the isolation net; 26, the accommodating groove; 27, the smooth groove; 28, the third vent hole; Ring; 4. Air compressor unit; 5. Air expansion unit; 6. Lever; 7. Crank; 8. Piston; 9. Support.
具体实施方式Detailed ways
下面详细描述本申请的实施例,所述实施例的示例在附图中示出,其中自始至终相同或类似的标号表示相同或类似的元件或具有相同或类似功能的元件。下面通过参考附图描述的实施例是示例性的,仅用于解释本申请,而不能理解为对本申请的限制。相反,本申请的实施例包括落入所附加权利要求书的精神和内涵范围内的所有变化、修改和等同物。The following describes in detail the embodiments of the present application, examples of which are illustrated in the accompanying drawings, wherein the same or similar reference numerals refer to the same or similar elements or elements having the same or similar functions throughout. The embodiments described below with reference to the accompanying drawings are exemplary and are only used to explain the present application, but should not be construed as a limitation on the present application. On the contrary, the embodiments of the present application include all changes, modifications and equivalents falling within the spirit and scope of the appended claims.
图1是本申请一实施例提出的一种具有缓冲作用的重力储能系统的结构示意图。FIG. 1 is a schematic structural diagram of a gravity energy storage system with buffer function proposed by an embodiment of the present application.
参阅图1和图2,一种具有缓冲作用的重力储能系统,包括竖井1,竖井1中活动插接有重力块2,重力块2与竖井1侧壁之间通过密封膜3密封连接,重力块2、密封膜3和竖井1位于密封膜3下方的空间之间围成储气腔11;Referring to FIGS. 1 and 2, a gravity energy storage system with buffering function includes a
重力块2包括壳体21和填充在壳体21中的蓄热材料22,壳体21底部设置有与储气腔11相连通的第一通气孔23,壳体21顶部连接有空气压缩机组4和空气膨胀机组5,使得空气压缩机组4压缩后得到的高温高压空气通过蓄热材料22后将热量存储在蓄热材料22中,然后通过第一通气孔23进入储气腔11中,在释能过程中,储气腔11中的压缩空气进入壳体21中后经过蓄热材料22时吸收蓄热材料22中存储的热量,然后进入空气膨胀机组5中进行做功,通过重力块2自身即可实现热交换,无需另外设置热交换单元进行热交换,节省空间和成本。The
另外,竖井1内壁和壳体21外壁对应缠绕有导线圈阵列,竖井1内壁上的导线圈阵列按顺序与不同的电源连接,壳体21外壁的各个导线圈自成闭路,以通过电源给竖井1内壁上的导线圈阵列施加固定频率的交流电,在壳体21外壁上的导线圈阵列中感应出反向环流,以使两组相反电流方向导线圈阵列形成反向的电磁场后,通过电磁力对重力块2施加向上的作用力,在压缩储能过程中,需要采用提升措施将重力块2向上提起,通过电源给竖井1内壁上的线圈阵列施加固定频率的交流电,在重力块2外壁上的线圈中感应出反向环流,两组相反电流方向线圈形成反向的电磁场后,通过电磁力使重力块2向上运动,从而减小启动瞬间重力块2需要的提升力,同时通过空气压缩机组4向储气腔11中通入压缩气体,重力块2向上移动至最高限位,在释能过程中,储气腔11中的气体通入空气膨胀机组5中进行做功发电,重力块2向下移动,使得重力块2的重力势能也转化为部分电能,另外,发生事故时,重力块2不受控向下加速运动,激发竖井1内壁线圈电源快速启动供电并形成电磁场,在重力块2外壁上的线圈中感应出反向电磁场,对重力块2形成向上的作用力,从而使重力块2快速减速,减小坠落时对竖井1下方的撞击动能。In addition, the inner wall of the
在一些实施例中,壳体21顶部设置有两个第二通气孔24,两个第二通气孔24处均设置有阀门,两个阀门分别连接有进气通道和出气通道,进气通道和所述出气通道分别连接空气压缩机组4和空气膨胀机组5,使得压缩空气向壳体21中通气时,进气通道处的阀门打开,出气通道处的阀门关闭,通入壳体21中的压缩空气进入壳体21后通过第一通气孔23进入储气腔11中,在释能时,进气通道处的阀门关闭,出气通道处的阀门打开,此时储气腔11中的压缩空气进入壳体21中后只能通过出气通道通入空气膨胀机组5中。In some embodiments, two second ventilation holes 24 are provided at the top of the
由于壳体21中填充有蓄热材料22,为了防止蓄热材料22从第一通气孔23和第二通气孔24处洒出,可以在第一通气孔23和第二通气孔24处均设置隔离网25,以通过隔离网25对蓄热材料22进行阻挡,另外,壳体21可以分成筒体和盖体,盖体固定在筒体顶部,第一通气孔23设置在筒体的底部,并且在盖体上开两个第二通气孔24,并且在第一通气孔23处和两个第二通气孔24处均固定隔离网25,隔离网25上的网孔小于蓄热材料22的直径,由于隔离网25的阻挡能够防止蓄热材料22洒出,并且气体还能够通过隔离网25上的网孔。Since the
在一些实施例中,为了充分利用储气腔11中压缩空气的压力,实现对重力块2向上的作用力,可以在竖井1的底部侧壁开有多个连通腔12,连通腔12的底部设置有压力缸13,并且连通腔12中设置有杠杆6,杠杆6的一端铰接有曲柄7,另一端位于重力块2的下方,曲柄7的底端连接有活塞8,活塞8活动插接在压力缸13中,活塞8与压力缸13之间密封,活塞8下方的压力缸13中形成密封腔14,密封腔14中填充有可压缩气体,以通过向储气腔11中通入气体带动活塞8向下移动,使得杠杆6一端向上升起对重力块2提供向上的辅助力,也就是说,当向储气腔11中通入压缩空气,储气腔11中的压缩空气通过连通腔12进入活塞8上方的压力缸13中,在压缩空气的压力作用下活塞8向下移动对压力缸13中的可压缩气体进行压缩,根据杠杆原理,活塞8向下移动过程中通过曲柄7带动杠杆6的一端向下移动,杠杆6的另一端向上翘起,翘起的一端向上移动过程中作用于重力块2给重力块2施加向上的力,为重力块2向上启动提供辅助力,便于重力块2的启动,通过杠杆6和导线圈的共同作用,能够大大提高对重力块2向上移动的作用力,减小重力块2向上移动时所需的外力。In some embodiments, in order to make full use of the pressure of the compressed air in the air storage cavity 11 and realize the upward force on the
在一些实施例中,活塞8上方的压力缸13中灌充有粘性压力液15,以通过粘性压力液15实现活塞8和压力缸13之间的密封,利用液体密封效果较好,在初始状态时,作用于活塞8上的粘性压力液的重力加上储气腔11中的空气压力与密封腔14中的可压缩气体对活塞8向上的压力平衡,进而使得杠杆6处于水平状态。In some embodiments, the
为了适应杠杆6在连通腔12中的工作,可以在连通腔12中设置有支座9,杠杆6安装在支座9上,也就是说杠杆6可以铰接在支座9上,使得杠杆6和支座9的连接处形成支点。In order to adapt to the work of the lever 6 in the
在一些实施例中,壳体21的底端侧壁开有延伸至底面的容纳槽26,容纳槽26可以为延伸至壳体21底部外壁的环形槽,使得多个连通腔12中的杠杆6的一端均能够伸入容纳槽26中,当杠杆6靠近重力块2的一端升起时,能够在容纳槽26中直接作用于壳体21,对重力块2施加向上的作用力,为了保障壳体21中的压缩空气仍能够顺利的进入储气腔11中,第一通气孔23是直接垂直贯穿壳体21底部,在第一通气孔23的侧壁可以开设多个与第一通气孔23相连通的第三通气孔28,多个第三通气孔28与储气腔11相连通,使得壳体21中的压缩空气可以通过第一通气孔23以及第三通气孔28进入储气腔11中。In some embodiments, the bottom end sidewall of the
另外,连通腔12横向设置,直接在竖井1的侧壁上垂直施工一段形成连通腔12,然后在连通腔12远离竖井1的一端地面上开设压力缸13,压力缸13和竖井1均为竖直设置。In addition, the
在一些实施例中,连通腔12可以设置多个,多个连通腔12中的杠杆6等角度设置在壳体21周侧,每个连通腔12中均设置有压力缸13,通过多个连通腔12中设置的杠杆6同时能够对重力块2施加向上的作用力,并且由于多个连通腔12中的杠杆6等角度设置在重力块2周侧,使得多个杠杆6一端对重力块2向上的辅助力均匀,当连通腔12设置多个时,此时重力块2底端侧壁上可以对应设置多个容纳槽26。In some embodiments, a plurality of
需要说明的是,竖井1中密封膜的设置可以有多种。It should be noted that, there may be various arrangements of the sealing film in the
作为一种可能的情况,竖井1为圆柱筒状结构,壳体21为圆柱状结构,壳体21的外壁面周侧设置有多个呈竖直分布的平滑凹槽27,其中竖直方向与壳体21的轴向方向一致,密封膜3为套设在壳体21外部的环形筒状结构,密封膜的外径等于竖井1的内径,密封膜从中间将上部向内翻折后形成外环31和内环32连接组成的环形鞍面结构,翻折后得到的内环32周侧形成褶皱凸起,外环31的底端与竖井1内壁密封连接,内环32的底端与壳体21的外壁密封连接,褶皱凸起与平滑凹槽27贴合,由于壳体21的外径小于密封膜的内径,密封膜在翻折后形成的内环32位于外环31内侧,密封膜为筒状结构,翻折后的内环32为了适应环向空间大小,会出现褶皱凸起,通过设置平滑凹槽27使得密封膜在固定时能够将褶皱凸起凹陷于平滑凹槽27内,从而增大壳体21环向外壁与密封膜相接的长度,使得密封膜固定在壳体21周侧的长度增大,在壳体21上下移动过程中密封膜的外环31和内环32始终保持与竖井1内壁、壳体21外壁的良好贴合,提升了壳体21与密封膜直接的贴合结合位点,提升了密封膜与壳体21的贴合紧密型,并且由于密封膜的外径与竖井1的内径相同,进而使得密封膜的外环31能够完全贴合在竖井1内壁上,使得密封膜的外环31与竖井1之间结合紧密,利用刚性壁面为密封膜提供刚性支撑,提高了密封膜使用安全性、可靠性和寿命。As a possible situation, the
另外,密封膜的环形筒状结构为上下等径的圆柱面结构,方便密封膜的加工。In addition, the annular cylindrical structure of the sealing film is a cylindrical surface structure with equal diameters up and down, which facilitates the processing of the sealing film.
另外,壳体21周侧设置平滑凹槽27后,通过控制平滑凹槽27的深度和数量,使得壳体21在平滑凹槽27处环向的周长增大(例如,壳体21的筒体为圆柱筒结构,在平滑凹槽27处与圆柱筒轴线垂直的截面处的环向周长就是壳体21在平滑凹槽27处的环向的周长,并且密封膜外壁环向周长就是密封膜环形筒状结构的外筒端面周长),内环32的褶皱凸起的部分能够贴合在平滑凹槽27中,使得内环32与壳体21之间贴合,褶皱凸起与平滑凹槽27贴合,壳体21能够对密封膜进行支撑,提高了密封膜使用安全性、可靠性和寿命。In addition, after the
上述实施例中记载的一种具有缓冲作用的重力储能系统的具体储气方法如下:The specific gas storage method of a kind of gravity energy storage system with buffering effect recorded in the above embodiment is as follows:
在初始状态时,作用于活塞8上的粘性压力液的重力加上储气腔11中的空气压力与密封腔14中的可压缩气体对活塞8向上的压力平衡,进而使得杠杆6处于水平状态;In the initial state, the gravity of the viscous pressure liquid acting on the
储能时,电动机通电带动空气压缩机组4对气体压缩做功,将常温常压空气压缩后得到高温高压空气,高温高压空气通入重力块2中通过蓄热材料22后将热量存储在蓄热材料22中得到低温高压气体,低温高压气体通入储气腔11中,储气腔11中的压缩空气通过连通腔12进入到压力缸13中,对活塞8施加向下的压力,使得活塞8在压力缸13中向下移动,移动过程中通过曲柄7拉动杠杆6的一端向下移动,杠杆6的另一端向上抬升,抬升的过程中对重力块2施加向上的辅助力,同时通过电源给竖井1内壁上的导线圈阵列施加固定频率的交流电,在壳体21外壁上的导线圈阵列中感应出反向环流,以使两组相反电流方向导线圈阵列形成反向的电磁场后,通过电磁力对重力块2施加向上的作用力,重力块2向上移动至最高限位,重力块2向上移动过程中杠杆6靠近重力块2的一端也向上移动至一定位置后停止,保持倾斜的状态;When storing energy, the electric motor is energized to drive the air compressor unit 4 to compress the gas to do work, compress the normal temperature and normal pressure air to obtain high temperature and high pressure air, and the high temperature and high pressure air passes into the
释能时,储气腔11中的压缩气体进入重力块2中,吸收蓄热材料22中存储的热量,得到的高温高压气体通过出气通道进入空气膨胀机组5中进行做功,带动发电机发电,重力块2向下移动,当重力块2移动至与杠杆6抬升的一端接触时,通过杠杆6抬升的一端对重力块2进行支撑缓冲,使得重力块2能够缓慢向下移动,发生事故时,重力块2不受控向下加速运动,激发竖井1内壁线圈电源快速启动供电并形成电磁场,在重力块2外壁上的线圈中感应出反向电磁场,对重力块2形成向上的作用力,从而使重力块2快速减速,并且杠杆6也会对重力块2有一定的支撑作用,减小坠落时对竖井1下方的撞击动能。When releasing energy, the compressed gas in the air storage chamber 11 enters the
需要说明的是,在本申请的描述中,术语“第一”、“第二”等仅用于描述目的,而不能理解为指示或暗示相对重要性。此外,在本申请的描述中,除非另有说明,“多个”的含义是两个或两个以上。It should be noted that, in the description of the present application, the terms "first", "second" and the like are only used for the purpose of description, and should not be construed as indicating or implying relative importance. Also, in the description of this application, unless otherwise specified, "plurality" means two or more.
流程图中或在此以其他方式描述的任何过程或方法描述可以被理解为,表示包括一个或更多个用于实现特定逻辑功能或过程的步骤的可执行指令的代码的模块、片段或部分,并且本申请的优选实施方式的范围包括另外的实现,其中可以不按所示出或讨论的顺序,包括根据所涉及的功能按基本同时的方式或按相反的顺序,来执行功能,这应被本申请的实施例所属技术领域的技术人员所理解。Any description of a process or method in the flowcharts or otherwise described herein may be understood to represent a module, segment or portion of code comprising one or more executable instructions for implementing a specified logical function or step of the process , and the scope of the preferred embodiments of the present application includes alternative implementations in which the functions may be performed out of the order shown or discussed, including performing the functions substantially concurrently or in the reverse order depending upon the functions involved, which should It is understood by those skilled in the art to which the embodiments of the present application belong.
在本说明书的描述中,参考术语“一个实施例”、“一些实施例”、“示例”、“具体示例”、或“一些示例”等的描述意指结合该实施例或示例描述的具体特征、结构、材料或者特点包含于本申请的至少一个实施例或示例中。在本说明书中,对上述术语的示意性表述不一定指的是相同的实施例或示例。而且,描述的具体特征、结构、材料或者特点可以在任何的一个或多个实施例或示例中以合适的方式结合。In the description of this specification, description with reference to the terms "one embodiment," "some embodiments," "example," "specific example," or "some examples", etc., mean specific features described in connection with the embodiment or example , structure, material or feature is included in at least one embodiment or example of the present application. In this specification, schematic representations of the above terms do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
尽管上面已经示出和描述了本申请的实施例,可以理解的是,上述实施例是示例性的,不能理解为对本申请的限制,本领域的普通技术人员在本申请的范围内可以对上述实施例进行变化、修改、替换和变型。Although the embodiments of the present application have been shown and described above, it should be understood that the above embodiments are exemplary and should not be construed as limitations to the present application. Embodiments are subject to variations, modifications, substitutions and variations.
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