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CN116557337A - Sealing part and impeller equipment - Google Patents

Sealing part and impeller equipment Download PDF

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Publication number
CN116557337A
CN116557337A CN202310667344.7A CN202310667344A CN116557337A CN 116557337 A CN116557337 A CN 116557337A CN 202310667344 A CN202310667344 A CN 202310667344A CN 116557337 A CN116557337 A CN 116557337A
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CN
China
Prior art keywords
flow
impeller
combs
shaft
comb teeth
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
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CN202310667344.7A
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Chinese (zh)
Inventor
李英南
张雪辉
常学煜
王强
陈海生
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National Energy Large Scale Physical Energy Storage Technology R & D Center Of Bijie High Tech Industrial Development Zone
Institute of Engineering Thermophysics of CAS
Original Assignee
National Energy Large Scale Physical Energy Storage Technology R & D Center Of Bijie High Tech Industrial Development Zone
Institute of Engineering Thermophysics of CAS
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Application filed by National Energy Large Scale Physical Energy Storage Technology R & D Center Of Bijie High Tech Industrial Development Zone, Institute of Engineering Thermophysics of CAS filed Critical National Energy Large Scale Physical Energy Storage Technology R & D Center Of Bijie High Tech Industrial Development Zone
Priority to CN202310667344.7A priority Critical patent/CN116557337A/en
Publication of CN116557337A publication Critical patent/CN116557337A/en
Pending legal-status Critical Current

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/08Sealings
    • F04D29/10Shaft sealings
    • F04D29/102Shaft sealings especially adapted for elastic fluid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/08Sealings
    • F04D29/16Sealings between pressure and suction sides
    • F04D29/161Sealings between pressure and suction sides especially adapted for elastic fluid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/20Hydro energy

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

本发明公开了一种密封部件及叶轮设备,涉及领域密封技术领域。密封部件包括内侧面、内端面和外端面,内侧面朝向轴,内端面朝向机匣内部,外端面朝向机匣外部;内端面上设置有导流区,导流区绕密封部件的周向布置;导流区内设置有至少两个第一导流梳齿,第一导流梳齿为条状的片体,第一导流梳齿的长度方向从靠近内侧面向远离内侧面的方向延伸。本发明解决了现有的叶轮设备密封件的气封间隙激振严重技术的问题。

The invention discloses a sealing component and impeller equipment, and relates to the technical field of sealing. The sealing component includes an inner surface, an inner end surface and an outer end surface, the inner surface faces the shaft, the inner end surface faces the inside of the casing, and the outer end surface faces the outside of the casing; a diversion area is arranged on the inner end surface, and the flow diversion region is arranged around the circumference of the sealing member ; There are at least two first guide combs in the diversion area, the first guide combs are strip-shaped pieces, and the length direction of the first guide combs extends from the direction close to the inner side to the direction away from the inner side. The invention solves the technical problem of serious vibration excitation in the gas seal gap of the sealing part of the impeller equipment in the prior art.

Description

一种密封部件及叶轮设备A sealing component and impeller device

技术领域technical field

本发明涉及领域密封技术领域,尤其涉及一种密封部件及叶轮设备。The invention relates to the technical field of sealing, in particular to a sealing component and impeller equipment.

背景技术Background technique

叶轮设备是一种以连续旋转叶片为本体,使能量在流体工质与轴动力之间相互转换的动力机械。叶轮设备都包括叶轮、叶轮轴和缸体,在叶轮轴和缸体之间有密封件。叶轮是盘型转动件,叶轮轴为叶轮的中心轴,也是转动轴,并且伸出缸体,缸体也称为机匣。现有的在叶轮轴和缸体之间的密封件多使用迷宫密封,迷宫密封由一排环状密封梳齿组成,密封梳齿与轴或机匣之间存在很小的节流间隙。Impeller equipment is a power machine that uses continuous rotating blades as its body to convert energy between fluid working fluid and shaft power. The impeller equipment includes an impeller, an impeller shaft and a cylinder, and there is a seal between the impeller shaft and the cylinder. The impeller is a disc-shaped rotating part, and the impeller shaft is the central axis of the impeller, which is also the rotating shaft, and extends out of the cylinder, which is also called the casing. The existing seal between the impeller shaft and the cylinder body mostly uses a labyrinth seal. The labyrinth seal is composed of a row of ring-shaped sealing combs, and there is a small throttling gap between the sealing combs and the shaft or casing.

在实现本发明的过程中,发明人发现现有技术中至少存在如下问题:首先,本领域技术人员都知道迷宫密封必定存在泄漏间隙,无法做到完全密封。当轴在运转时存在偏心的时候,轴会出现震动,偏心程度越大,震动程度越大。此外,转轴在运行中不可避免的出现偏心,这使叶轮轴与密封件之间的密封间隙流道的宽窄不同,并且在设备运行时,流体工质(即被密封气体)将不断进入迷宫密封中,并由于转子的旋转,气流进入迷宫密封前会带有一定的周向速度,该周向流动的气流会导致在叶轮轴表面的压力分布不均,从而加剧了叶轮轴不稳定的振动,这种现象称为气封间隙激振,目前已多次出现叶轮设备因间隙气流激振而无法达到额定工作状态的问题。当然,转轴的偏心程度在一定范围内被视为安全运行范围。随着转轴的转速增加,上述的气封间隙激振越明显。现有技术中也可以通过增加检修维护转轴次数来避免气封间隙激振的出现,但该做法势必会增加使用成本。During the process of realizing the present invention, the inventors found that there are at least the following problems in the prior art: firstly, those skilled in the art know that there must be leakage gaps in the labyrinth seal, and a complete seal cannot be achieved. When the shaft is eccentric during operation, the shaft will vibrate, and the greater the degree of eccentricity, the greater the degree of vibration. In addition, the eccentricity of the rotating shaft is inevitable during operation, which makes the width of the sealing gap flow channel between the impeller shaft and the seal different, and when the equipment is running, the fluid working medium (that is, the sealed gas) will continue to enter the labyrinth seal Due to the rotation of the rotor, the airflow will have a certain circumferential velocity before entering the labyrinth seal. The circumferential flow of airflow will cause uneven pressure distribution on the surface of the impeller shaft, thereby aggravating the unstable vibration of the impeller shaft. This phenomenon is called air seal gap excitation. At present, there have been many problems that the impeller equipment cannot reach the rated working state due to the vibration of the gap air flow. Of course, the degree of eccentricity of the rotating shaft is considered as a safe operating range within a certain range. As the rotation speed of the rotating shaft increases, the vibration of the above-mentioned air seal gap becomes more obvious. In the prior art, the excitation vibration of the air seal gap can also be avoided by increasing the number of times of inspection and maintenance of the rotating shaft, but this method will inevitably increase the cost of use.

基于此,如何避免叶轮设备密封件的气封间隙激振现象,防止叶轮轴的转动不平稳是本领域技术人员亟待解决的技术问题。Based on this, how to avoid the excitation phenomenon of the air seal gap of the impeller equipment seal and prevent the impeller shaft from rotating unevenly is a technical problem to be solved urgently by those skilled in the art.

发明内容Contents of the invention

本发明的目的在于提供一种减小气封间隙激振的密封部件,以保证穿过密封部件的轴能够长期平稳运转。The object of the present invention is to provide a sealing component that reduces the vibration of the air seal gap, so as to ensure that the shaft passing through the sealing component can run smoothly for a long time.

为达此目的,一方面,提供了一种密封部件,固定在机匣的轴孔内,包括内侧面、内端面和外端面,所述内侧面朝向轴,所述内端面朝向机匣内部,所述外端面朝向机匣外部;所述内端面上设置有导流区,所述导流区绕所述密封部件的周向布置;所述导流区内设置有至少两个第一导流梳齿,所述第一导流梳齿为条状的片体,所述第一导流梳齿的长度方向从靠近所述内侧面向远离所述内侧面的方向延伸。To achieve this purpose, on the one hand, a sealing component is provided, which is fixed in the shaft hole of the casing, and includes an inner surface, an inner end surface and an outer end surface, the inner surface faces the shaft, and the inner end surface faces the inside of the casing, The outer end faces toward the outside of the casing; a guide area is provided on the inner end face, and the guide area is arranged around the circumference of the sealing member; at least two first guide areas are arranged in the guide area Comb teeth, the first guide comb teeth are strip-shaped pieces, and the length direction of the first guide comb teeth extends from a direction close to the inner surface to a direction away from the inner surface.

进一步地,所述导流区设置在所述内端面靠近所述内侧面处。Further, the guide area is arranged on the inner end surface close to the inner surface.

进一步地,两个所述第一导流梳齿的间距从靠近所述内侧面到远离所述内侧面的方向上逐渐增加。Further, the distance between the two first guide combs gradually increases from the direction close to the inner surface to the direction away from the inner surface.

进一步地,所述第一导流梳齿呈弧形,所有的所述第一导流梳齿的圆心相对于所述第一导流梳齿均在同侧。Further, the first guide combs are arc-shaped, and the centers of all the first guide combs are on the same side relative to the first guide combs.

进一步地,所有的所述第一导流梳齿组成旋涡状。Further, all the first guide comb teeth form a vortex shape.

进一步地,还包括至少两个第二导流梳齿,所述第二导流梳齿为条状的片体,所述第二导流梳齿与所述第一导流梳齿交叉布置。Further, at least two second guide combs are included, the second guide combs are strip-shaped pieces, and the second guide combs are arranged to intersect with the first guide combs.

进一步地,所述第二导流梳齿呈环形,所述第二导流梳齿绕所述密封部件的周向布置。Further, the second guide combs are ring-shaped, and the second guide combs are arranged around the circumference of the sealing member.

进一步地,所述第二导流梳齿有多个,两两所述第二导流梳齿依次套设。Further, there are a plurality of second diversion combs, and two of the second diversion combs are nested in sequence.

进一步地,所述导流区可以是平面、弧形面或者斜面。Further, the diversion area may be a plane, an arc or an inclined plane.

有益效果:Beneficial effect:

本方案提供了一种密封部件,固定在机匣的轴孔内,包括内侧面、内端面和外端面,内侧面朝向轴,内端面朝向机匣内部,外端面朝向机匣外部。在内端面上设置有导流区,导流区绕密封部件的周向布置。导流区内设置有至少两个第一导流梳齿,第一导流梳齿为条状的片体,第一导流梳齿的一端从导流区的内端延伸到外端,导流区的内端为靠近内侧面的端部。This solution provides a sealing component, which is fixed in the shaft hole of the casing, including an inner surface, an inner end surface and an outer end surface, the inner surface faces the shaft, the inner end surface faces the inside of the casing, and the outer end surface faces the outside of the casing. A flow guide area is provided on the inner end surface, and the flow guide area is arranged around the circumference of the sealing component. At least two first diversion combs are arranged in the diversion area, the first diversion combs are strip-shaped pieces, one end of the first diversion comb extends from the inner end to the outer end of the diversion area, The inner end of the flow area is the end near the inner side.

本方案的密封部件在使用时,由于其内端面上设置有导流区,导流区上设有至少两个第一导流梳齿,两个第一导流梳齿之间形成流道,当叶轮轴转动时,有部分泄漏气体将进入上述流道内,在第一导流梳齿的作用下,降低了气流向密封部件的内侧面流动的能量,故泄漏气流在密封部件的内侧面与轴之间的间隙的流通将减小。从而,本方案的密封部件具有密封性能好、减轻气封间隙激振、保证轴的平稳转动的技术效果。When the sealing part of this solution is in use, since a diversion area is provided on its inner end surface, at least two first diversion combs are arranged on the diversion region, and a flow channel is formed between the two first diversion combs. When the impeller shaft rotates, part of the leakage gas will enter the above-mentioned flow channel, and under the action of the first guide comb, the energy of the air flow to the inner surface of the sealing part is reduced, so the leakage air flows between the inner surface of the sealing part and the inner surface of the sealing part. The circulation in the gap between the shafts will be reduced. Therefore, the sealing component of the present solution has the technical effects of good sealing performance, reducing the excitation of the air seal gap, and ensuring the smooth rotation of the shaft.

附图说明Description of drawings

图1是本申请的密封部件的结构示意图;Fig. 1 is the structural representation of the sealing part of the present application;

图2是图1中的轴向视图;Fig. 2 is the axial view in Fig. 1;

图3是图2中A-A的截面图;Fig. 3 is a sectional view of A-A in Fig. 2;

图4是安装在叶轮设备上的密封部件的局部示意图。Fig. 4 is a partial schematic view of a sealing member mounted on the impeller device.

图中:100-内侧面;200-内端面;210-导流区;211-第一导流梳齿;212-第二导流梳齿;110-第三梳齿;300-外端面;400-外侧面;500-轴。In the figure: 100-inner surface; 200-inner end face; 210-diversion area; 211-first diversion comb; 212-second diversion comb; 110-third comb; 300-outer end face; 400 -outer side; 500-axis.

具体实施方式Detailed ways

为使本发明解决的技术问题、采用的技术方案和达到的技术效果更加清楚,下面将结合附图对本发明实施例的技术方案做进一步的详细描述,显然,所描述的实施例仅仅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。In order to make the technical problems solved by the present invention, the technical solutions adopted and the technical effects achieved clearer, the technical solutions of the embodiments of the present invention will be further described in detail below in conjunction with the accompanying drawings. Obviously, the described embodiments are only the technical solutions of the present invention. Some, but not all, embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without making creative efforts belong to the protection scope of the present invention.

在本发明的描述中,除非另有明确的规定和限定,术语“相连”、“连接”、“固定”应做广义理解,例如,可以是固定连接,也可以是可拆卸连接,或成一体;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或两个元件的相互作用关系。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, unless otherwise clearly specified and limited, the terms "connected", "connected" and "fixed" should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integrated ; It can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediary, and it can be the internal communication of two components or the interaction relationship between two components. Those of ordinary skill in the art can understand the specific meanings of the above terms in the present invention in specific situations.

在本发明中,除非另有明确的规定和限定,第一特征在第二特征之“上”或之“下”可以包括第一和第二特征直接接触,也可以包括第一和第二特征不是直接接触而是通过它们之间的另外的特征接触。而且,第一特征在第二特征“之上”、“上方”和“上面”包括第一特征在第二特征正上方和斜上方,或仅仅表示第一特征水平高度高于第二特征。第一特征在第二特征“之下”、“下方”和“下面”包括第一特征在第二特征正下方和斜下方,或仅仅表示第一特征水平高度小于第二特征。In the present invention, unless otherwise clearly specified and limited, a first feature being "on" or "under" a second feature may include direct contact between the first and second features, and may also include the first and second features Not in direct contact but through another characteristic contact between them. Moreover, "above", "above" and "above" the first feature on the second feature include that the first feature is directly above and obliquely above the second feature, or simply means that the first feature is horizontally higher than the second feature. "Below", "beneath" and "under" the first feature to the second feature include that the first feature is directly below and obliquely below the second feature, or simply means that the first feature has a lower level than the second feature.

实施例一:Embodiment one:

如图1-图4所示,本实施例提供了一种密封部件,固定在机匣的轴孔内,轴从密封部件内孔穿出。密封部件包括内侧面100、内端面200和外端面300,内侧面100朝向轴500,内端面200朝向机匣内部,外端面300朝向机匣外部。内端面200上设置有导流区210,导流区210绕密封部件的周向布置。导流区210内设置有至少两个第一导流梳齿211,第一导流梳齿211为条状的片体,第一导流梳齿211的长度方向从靠近内侧面100向远离内侧面100的方向延伸。As shown in FIGS. 1-4 , this embodiment provides a sealing component, which is fixed in the shaft hole of the casing, and the shaft passes through the inner hole of the sealing component. The sealing component includes an inner surface 100 , an inner end surface 200 and an outer end surface 300 , the inner surface 100 faces the shaft 500 , the inner end surface 200 faces inside the casing, and the outer end surface 300 faces outside the casing. A flow guide area 210 is provided on the inner end surface 200, and the flow guide area 210 is arranged around the circumference of the sealing component. At least two first guide combs 211 are arranged in the guide area 210. The first guide combs 211 are strip-shaped pieces. The length direction of the first guide combs 211 is from close to the inner surface 100 to away from the inside The direction of the side 100 extends.

本方案的密封部件在使用时,由于其内端面200上设置有导流区210,导流区210上设有至少两个第一导流梳齿211,两个第一导流梳齿211之间形成流道,当轴500(例如,叶轮轴)转动时,有部分泄漏气体将进入上述流道内,在第一导流梳齿的作用下,降低了气流向密封部件的内侧面100流动的能量,故泄漏气流在密封部件的内侧面100与轴500之间的间隙的流通将减小。从而,本实施例的密封部件具有减轻气封间隙激振、保证轴的平稳转动的技术效果。When the sealing part of this solution is in use, since the inner end surface 200 is provided with a diversion area 210, the diversion area 210 is provided with at least two first diversion combs 211, between the two first diversion combs 211 When the shaft 500 (for example, the impeller shaft) rotates, part of the leakage gas will enter the above-mentioned flow channel, and under the action of the first guide comb teeth, the flow of the gas to the inner surface 100 of the sealing member is reduced. Energy, so the circulation of the leakage air flow in the gap between the inner surface 100 of the sealing member and the shaft 500 will be reduced. Therefore, the sealing component of this embodiment has the technical effect of alleviating the excitation of the air seal gap and ensuring the smooth rotation of the shaft.

进一步地,如图1-图2所示,导流区210设置在内端面200的靠近内侧面100处。导流区210设在靠近轴500内端面200上。进一步地,所述第一导流梳齿211的一端从所述内侧面100与所述内端面200的交界处向外(也就是说,向外侧面400)延伸。Further, as shown in FIGS. 1-2 , the diversion area 210 is disposed near the inner surface 100 of the inner end surface 200 . The guide area 210 is disposed on the inner end surface 200 close to the shaft 500 . Further, one end of the first guide comb 211 extends outward from the junction of the inner surface 100 and the inner end surface 200 (that is, to the outer surface 400 ).

进一步地,如图1-图2所示,两个第一导流梳齿211的间距在靠近内侧面100到远离内侧面100(也就是说,靠近外侧面400)的方向上逐渐增加。Further, as shown in FIGS. 1-2 , the distance between the two first guide combs 211 gradually increases from the direction of approaching the inner surface 100 to away from the inner surface 100 (that is, approaching the outer surface 400 ).

进一步地,如图1-图2所示,第一导流梳齿211呈弧形,所有的第一导流梳齿211的圆心相对于第一导流梳齿211均在同侧。进一步地,所有的第一导流梳齿211组成旋涡状的。旋涡状的第一导流梳齿211更有利于将流体往内端面200导流,使流体沿着内端面200向与内侧面100近似垂直的方向流动,进而减少进入内侧面100的流体,进而减轻了气封间隙激振现象,保证轴的平稳转动。Further, as shown in FIGS. 1-2 , the first guide combs 211 are arc-shaped, and the centers of circles of all the first guide combs 211 are on the same side relative to the first guide combs 211 . Further, all the first guide combs 211 form a spiral shape. The vortex-shaped first diversion comb 211 is more conducive to diverting the fluid to the inner end surface 200, so that the fluid flows along the inner end surface 200 in a direction approximately perpendicular to the inner surface 100, thereby reducing the fluid entering the inner surface 100, and further The vibration phenomenon of the air seal gap is alleviated, and the smooth rotation of the shaft is ensured.

进一步地,如图1-图3所示,密封部件还包括至少两个第二导流梳齿212,第二导流梳齿212为条状的片体,第二导流梳齿212与第一导流梳齿211交叉布置。至少两个第一导流梳齿与至少两个第二导流梳齿形成至少一个节流腔体,节流腔体内有膨胀空间。泄漏气流依次进入各个节流腔体的膨胀空间内,在膨胀空间产生剧烈的湍流旋涡,上述的湍流旋涡把泄漏气流的机械能不可逆地转化为内能,向环境耗散,使泄漏气流的机械能不断下降,进而减小泄漏气体的泄漏量,提高密封性能。本实施例的密封部件,由于在第一导流梳齿211的结构上进一步设置第二导流梳齿212,提高了密封性能,减轻了气封间隙激振现象,进而保证轴的长时间地平稳地转动,使用在高速旋转的轴上时上述技术效果更为明显。Further, as shown in FIGS. 1-3 , the sealing component also includes at least two second guide combs 212 , the second guide combs 212 are strip-shaped sheets, and the second guide combs 212 are connected to the second guide combs. A diversion comb 211 is arranged in a crossed manner. At least two first guide combs and at least two second guide combs form at least one throttling cavity, and there is an expansion space in the throttling cavity. The leaked air flow enters the expansion space of each throttling cavity in turn, and a violent turbulent vortex is generated in the expansion space. The above-mentioned turbulent vortex irreversibly converts the mechanical energy of the leaked air flow into internal energy, and dissipates it to the environment, so that the mechanical energy of the leaked air flow continues Decrease, thereby reducing the leakage of leakage gas and improving the sealing performance. In the sealing part of this embodiment, since the second guide comb 212 is further provided on the structure of the first guide comb 211, the sealing performance is improved, the vibration phenomenon of the air seal gap is reduced, and the long-term maintenance of the shaft is ensured. Rotate smoothly, and the above-mentioned technical effect is more obvious when used on a high-speed rotating shaft.

进一步地,如图1-图3所示,第二导流梳齿212呈环形,第二导流梳齿212绕所述密封部件的周向布置。第一导流梳齿211与第二导流梳齿212交叉,此时第二导流梳齿212呈环形,当第一导流梳齿211、第二导流梳齿212均至少有两组时,在导流区210内形成多个上述的节流腔体,进一步提高密封部件的性能。Further, as shown in FIGS. 1-3 , the second guide combs 212 are annular, and the second guide combs 212 are arranged around the circumference of the sealing component. The first diversion comb 211 intersects with the second diversion comb 212. At this time, the second diversion comb 212 is ring-shaped. When the first diversion comb 211 and the second diversion comb 212 have at least two groups At this time, a plurality of the above-mentioned throttling cavities are formed in the guide area 210 to further improve the performance of the sealing component.

进一步地,如图1-图3所示,第二导流梳齿212呈环形时,并且第二导流梳齿212有多个,此时两两第二导流梳齿212依次套设。优选地,所有的第二导流梳齿212同心布置,优选地,所有的第二导流梳齿212的圆心与密封部件的中心轴共线。Further, as shown in FIGS. 1-3 , when the second guide combs 212 are ring-shaped, and there are multiple second guide combs 212 , at this time, two second guide combs 212 are nested in sequence. Preferably, all the second guide combs 212 are arranged concentrically, and preferably, the centers of all the second guide combs 212 are collinear with the central axis of the sealing component.

进一步地,如图1-图3所示,导流区210设置在密封部件的内端面200上,位于内端面200和内侧面100的交界处,导流区210可以是平面、弧形面或者斜面。Further, as shown in FIGS. 1-3 , the diversion area 210 is arranged on the inner end surface 200 of the sealing component, at the junction of the inner end surface 200 and the inner surface 100, and the diversion area 210 can be a plane, an arc surface or inclined plane.

进一步地,如图1-图3所示,内侧面100上有至少两个第三梳齿110,所第三梳齿110为条状片体,所述第三梳齿绕所述密封部件的周向布置,优选地,所述第三梳齿首尾相接。至少两个第三梳齿由所述内端面200至外端面300依次并排布置。优选地,内侧面100上有多个第三梳齿,每个第三梳齿并排等距布置。Further, as shown in Figures 1-3, there are at least two third comb teeth 110 on the inner surface 100, the third comb teeth 110 are strip-like pieces, and the third comb teeth wrap around the sealing member. Arranged in the circumferential direction, preferably, the third comb teeth are connected end to end. At least two third comb teeth are arranged side by side sequentially from the inner end surface 200 to the outer end surface 300 . Preferably, there are a plurality of third comb teeth on the inner surface 100, and each third comb tooth is arranged side by side and equidistant.

实施例二:Embodiment two:

如图4所述,本实施例公开了一种叶轮设备,包括实施例一中的任一种密封部件,叶轮设备还包括叶轮、叶轮轴和缸体,叶轮设置在叶轮轴上,叶轮轴位于缸体内,缸体设置有轴孔,叶轮轴从轴孔穿出,密封部件设在轴孔处,导流区朝向叶轮的背面,即密封部件的导流区靠近叶轮的背面,也即叶轮上没有工作叶片的一侧。本实施例的叶轮设备可以是轴流式,径流式,混流式,组合式。优选地,本实施例的叶轮设备为径流式,或者离心式。实施例一中的任一种密封部件用在径流式叶轮设备上时,密封部件的导流区朝向缸体内,位于叶轮背面,轴端密封之前,固定在轴端密封侧,叶轮设备在工作中处于静止状态。叶轮设备的缸体内的工作介质通常为气体且工作压力较高,但由于工作介质经过密封部件的两个第一导流梳齿之间形成流道,一部分的工作介质被导向与轴垂直的平面内,此时进入内侧面的工作介质将大幅减少,进而减轻了气封间隙激振现象,保证轴的平稳转动,同时也提高了密封效果。As shown in Figure 4, this embodiment discloses a kind of impeller equipment, including any one of the sealing components in Embodiment 1, the impeller equipment also includes an impeller, an impeller shaft and a cylinder, the impeller is arranged on the impeller shaft, and the impeller shaft is located at In the cylinder body, the cylinder body is provided with a shaft hole, the impeller shaft passes through the shaft hole, the sealing part is arranged at the shaft hole, and the diversion area faces the back of the impeller, that is, the diversion area of the sealing part is close to the back of the impeller, that is, the impeller on the side without working blades. The impeller device in this embodiment can be of axial flow type, radial flow type, mixed flow type, or combined type. Preferably, the impeller device in this embodiment is a radial flow type or a centrifugal type. When any of the sealing components in Embodiment 1 is used on the radial flow impeller equipment, the guide area of the sealing component faces the cylinder and is located on the back of the impeller. Before the shaft end is sealed, it is fixed on the shaft end sealing side. The impeller equipment is working in a static state. The working medium in the cylinder of the impeller equipment is usually gas and the working pressure is relatively high, but because the working medium passes through the two first guide comb teeth of the sealing part to form a flow channel, a part of the working medium is guided to the shaft perpendicular to the shaft. In the plane, the working medium entering the inner surface will be greatly reduced at this time, thereby reducing the vibration phenomenon of the air seal gap, ensuring the smooth rotation of the shaft, and improving the sealing effect at the same time.

进一步地,密封部件的导流区包括第一导流梳齿和第二导流梳齿时,两个第一导流梳齿与两个第二导流梳齿形成至少一个节流腔体,叶轮设备的工作介质进入节流腔体后将产生巨大的湍流漩涡,湍流漩涡在此过程中把流体的机械能不可逆的转化成内能,向环境耗散,使流体的机械能不断下降,进一步降低了气封间隙激振现象。Further, when the diversion area of the sealing component includes first diversion combs and second diversion combs, the two first diversion combs and the two second diversion combs form at least one throttling cavity, When the working medium of the impeller equipment enters the throttling chamber, a huge turbulent vortex will be generated. In the process, the turbulent vortex irreversibly converts the mechanical energy of the fluid into internal energy and dissipates it to the environment, which makes the mechanical energy of the fluid continuously decrease, further reducing the Gas seal gap excitation phenomenon.

当密封部件的结构为:第一导流梳齿211呈弧形,所有的第一导流梳齿211的圆心相对于第一导流梳齿211均在同侧时。进一步地,所有的第一导流梳齿211组成旋涡状时。优选地,密封部件上第一导流梳齿所组成旋涡的旋向和叶轮轴的转向相反。如图4所示,当叶轮轴500顺时针旋转时,第一导流梳齿211的弯曲方向朝逆时针方向。叶轮轴500顺时针旋转(如图4中的A方向)将带动其周围的工作介质也顺时针旋转,当工作介质遇到上第一导流梳齿时,其流动方向会发生改变,此时进入密封部件的内侧面100的工作介质与叶轮轴的转动方向相反(如图4中的B方向),此时,进入密封部件的内侧面100的工作介质的流向与被轴500带动的气流方向相反,降低了工作介质的周向流动能量,进入密封部件的内侧面100的工作介质的机械能将不可逆的转化成内能,进一步减少密封部件的内侧面100的工作介质,从而提高密封部件的密封性能,同时降低气封间隙激振现象。When the structure of the sealing component is: the first guide combs 211 are arc-shaped, and the circle centers of all the first guide combs 211 are on the same side relative to the first guide combs 211 . Further, all the first guide combs 211 form a vortex shape. Preferably, the direction of rotation of the vortex formed by the first guide comb teeth on the sealing member is opposite to the direction of rotation of the impeller shaft. As shown in FIG. 4 , when the impeller shaft 500 rotates clockwise, the bending direction of the first guide comb 211 is counterclockwise. The clockwise rotation of the impeller shaft 500 (direction A in Figure 4) will drive the surrounding working medium to also rotate clockwise. When the working medium encounters the first guide comb, its flow direction will change. At this time The working medium entering the inner surface 100 of the sealing member is opposite to the direction of rotation of the impeller shaft (as shown in the B direction in Figure 4 ). On the contrary, the circumferential flow energy of the working medium is reduced, and the mechanical energy of the working medium entering the inner surface 100 of the sealing component will be irreversibly converted into internal energy, further reducing the working medium on the inner surface 100 of the sealing component, thereby improving the sealing of the sealing component Performance, while reducing the vibration phenomenon of the air seal gap.

显然,本发明的上述实施例仅仅是为了清楚说明本发明所作的举例,而并非是对本发明的实施方式的限定。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。凡在本发明的精神和原则之内所作的任何修改、等同替换和改进等,均应包含在本发明权利要求的保护范围之内。Apparently, the above-mentioned embodiments of the present invention are only examples for clearly illustrating the present invention, rather than limiting the implementation of the present invention. For those of ordinary skill in the art, other changes or changes in different forms can be made on the basis of the above description. It is not necessary and impossible to exhaustively list all the implementation manners here. All modifications, equivalent replacements and improvements made within the spirit and principles of the present invention shall be included within the protection scope of the claims of the present invention.

Claims (10)

1. A sealing component, characterized in that the sealing component is fixed in a shaft hole of a casing and comprises an inner side surface, an inner end surface and an outer end surface, wherein the inner side surface faces the shaft, the inner end surface faces the inside of the casing, and the outer end surface faces the outside of the casing;
the inner end face is provided with a diversion area, and the diversion area is arranged around the circumference of the sealing part;
at least two first flow guiding comb teeth are arranged in the flow guiding area, the first flow guiding comb teeth are strip-shaped sheet bodies, and the length direction of the first flow guiding comb teeth extends from the direction close to the inner side face to the direction far away from the inner side face.
2. The seal of claim 1, wherein the flow directing region is disposed at the inner end surface proximate the inner side surface.
3. The seal of claim 1 wherein the spacing of two of said first guide fingers increases progressively from closer to said inner side to farther from said inner side.
4. The seal of claim 1 wherein said first flow-directing comb teeth are arcuate with the center of all of said first flow-directing comb teeth being on the same side relative to said first flow-directing comb teeth.
5. The seal of claim 4 wherein all of said first flow directing combs are formed as a vortex.
6. The seal of claim 1, further comprising at least two second flow-directing combs, the second flow-directing combs being strip-shaped sheets, the second flow-directing combs being disposed crosswise to the first flow-directing combs.
7. The seal of claim 6, wherein the second flow guide comb teeth are annular in shape, the second flow guide comb teeth being disposed about a circumference of the seal.
8. The sealing member according to claim 7, wherein a plurality of second guide comb teeth are provided, and each of the second guide comb teeth is sleeved in sequence.
9. The seal of claim 1 wherein the flow directing region is planar, arcuate or beveled.
10. An impeller apparatus comprising the sealing member of any one of claims 1 to 9, further comprising an impeller, an impeller shaft and a cylinder, said impeller being disposed on said impeller shaft, said impeller shaft being disposed within said cylinder, said cylinder being provided with a shaft bore from which said impeller shaft extends, said sealing member being disposed at said shaft bore, said flow guiding region being oriented toward the back of said impeller.
CN202310667344.7A 2023-06-07 2023-06-07 Sealing part and impeller equipment Pending CN116557337A (en)

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Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010077882A (en) * 2008-09-25 2010-04-08 Toyota Motor Corp Labyrinth seal structure for multistage turbine
US20100119367A1 (en) * 2007-06-06 2010-05-13 Akihiro Nakaniwa Sealing device for rotary fluid machine, and rotary fluid machine
JP2014141912A (en) * 2013-01-23 2014-08-07 Mitsubishi Heavy Ind Ltd Rotary machine
JP2015090144A (en) * 2013-11-07 2015-05-11 三菱重工業株式会社 Seal device and rotary machine
JP2017160860A (en) * 2016-03-10 2017-09-14 株式会社日立製作所 Turbo machine
JP2020029797A (en) * 2018-08-21 2020-02-27 株式会社酉島製作所 One-side suction pump
CN220037024U (en) * 2023-06-07 2023-11-17 毕节高新技术产业开发区国家能源大规模物理储能技术研发中心 A sealing component and impeller equipment

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100119367A1 (en) * 2007-06-06 2010-05-13 Akihiro Nakaniwa Sealing device for rotary fluid machine, and rotary fluid machine
JP2010077882A (en) * 2008-09-25 2010-04-08 Toyota Motor Corp Labyrinth seal structure for multistage turbine
JP2014141912A (en) * 2013-01-23 2014-08-07 Mitsubishi Heavy Ind Ltd Rotary machine
JP2015090144A (en) * 2013-11-07 2015-05-11 三菱重工業株式会社 Seal device and rotary machine
JP2017160860A (en) * 2016-03-10 2017-09-14 株式会社日立製作所 Turbo machine
JP2020029797A (en) * 2018-08-21 2020-02-27 株式会社酉島製作所 One-side suction pump
CN220037024U (en) * 2023-06-07 2023-11-17 毕节高新技术产业开发区国家能源大规模物理储能技术研发中心 A sealing component and impeller equipment

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