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CN111365259A - Centrifugal Compressor and Refrigerant Circulation System with Diffuser Supply Flow Path - Google Patents

Centrifugal Compressor and Refrigerant Circulation System with Diffuser Supply Flow Path Download PDF

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Publication number
CN111365259A
CN111365259A CN201811595302.2A CN201811595302A CN111365259A CN 111365259 A CN111365259 A CN 111365259A CN 201811595302 A CN201811595302 A CN 201811595302A CN 111365259 A CN111365259 A CN 111365259A
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Prior art keywords
gas
supply flow
gas supply
main
centrifugal compressor
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Inventor
刘华
张治平
李宏波
钟瑞兴
周宇
陈玉辉
亓静利
叶文腾
刘胜
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Gree Electric Appliances Inc of Zhuhai
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Gree Electric Appliances Inc of Zhuhai
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Priority to CN201811595302.2A priority Critical patent/CN111365259A/en
Priority to PCT/CN2019/113032 priority patent/WO2020134434A1/en
Publication of CN111365259A publication Critical patent/CN111365259A/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
    • F04D17/00Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D17/08Centrifugal pumps
    • F04D17/10Centrifugal pumps for compressing or evacuating
    • 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
    • F04D29/05Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps
    • F04D29/056Bearings
    • F04D29/057Bearings hydrostatic; hydrodynamic
    • 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
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal 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
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/4206Casings; Connections of working fluid for radial or helico-centrifugal pumps 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
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/44Fluid-guiding means, e.g. diffusers
    • 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
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/44Fluid-guiding means, e.g. diffusers
    • F04D29/441Fluid-guiding means, e.g. diffusers 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
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • 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
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/668Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps damping or preventing mechanical vibrations
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C32/00Bearings not otherwise provided for
    • F16C32/06Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings

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

Abstract

本发明公开了一种离心式压缩机和冷媒循环系统。离心式压缩机包括具有容纳腔的壳体、可转动地设置于容纳腔内的主轴、扩压器、气体推力轴承和供气流道,供气流道包括开设于扩压器上且用于向气体推力轴承供气的扩压器供气流道。本发明的离心式压缩机通过在扩压器上开设扩压器供气流道以向气体推力轴承直接供气,结构简单且加工方便。

Figure 201811595302

The invention discloses a centrifugal compressor and a refrigerant circulation system. The centrifugal compressor includes a housing with an accommodating cavity, a main shaft rotatably arranged in the accommodating cavity, a diffuser, a gas thrust bearing and a supply flow channel, the supply flow channel including a diffuser opened on the diffuser and used for supplying gas to the gas. Diffuser supply runners for thrust bearing air supply. The centrifugal compressor of the present invention directly supplies gas to the gas thrust bearing by opening the diffuser supply flow channel on the diffuser, and has a simple structure and convenient processing.

Figure 201811595302

Description

具有扩压器供气流道的离心式压缩机和冷媒循环系统Centrifugal Compressor and Refrigerant Circulation System with Diffuser Supply Flow Path

技术领域technical field

本发明涉及静压气体轴承技术领域,特别涉及一种具有扩压器供气流道的离心式压缩机和冷媒循环系统。The invention relates to the technical field of static pressure gas bearings, in particular to a centrifugal compressor and a refrigerant circulation system with a diffuser supplying flow passage.

背景技术Background technique

由于气体静压轴承具有高精度、低摩擦、低振动、低噪音、寿命长、无污染等优点,因此在离心式压缩机得到广泛应用。气体静压轴承利用外部供压形成气膜来进行气体润滑,其承载力和刚度随供气压力的增大而增大。但是气体静压轴承的缺点是存在“气锤振动”现象,气锤振动将导致轴承不能正常工作,严重时可损坏轴承,而气锤振动现象与外部供压大小有直接关系,外部供气压力可改变轴承的内部压强,内部压强越高,气锤振动越严重。Due to the advantages of high precision, low friction, low vibration, low noise, long life and no pollution, gas static pressure bearings are widely used in centrifugal compressors. Aerostatic bearings use external supply pressure to form a gas film for gas lubrication, and their bearing capacity and stiffness increase with the increase of gas supply pressure. However, the disadvantage of the gas static pressure bearing is the phenomenon of "air hammer vibration". The air hammer vibration will cause the bearing to not work normally, and the bearing may be damaged in severe cases. The air hammer vibration phenomenon is directly related to the external pressure supply. The external air supply pressure The internal pressure of the bearing can be changed. The higher the internal pressure, the more serious the vibration of the air hammer.

发明内容SUMMARY OF THE INVENTION

本发明的目的在于提供一种离心式压缩机和冷媒循环系统,以简化离心式压缩机的气体轴承的供气流道。The purpose of the present invention is to provide a centrifugal compressor and a refrigerant circulation system, so as to simplify the air supply passage of the gas bearing of the centrifugal compressor.

本发明第一方面提供一种离心式压缩机,包括:A first aspect of the present invention provides a centrifugal compressor, comprising:

壳体,具有容纳腔;a shell with an accommodating cavity;

主轴,可转动地设置于容纳腔内;The main shaft is rotatably arranged in the accommodating cavity;

扩压器;diffuser;

气体推力轴承;和gas thrust bearings; and

供气流道,包括开设于扩压器上且用于向气体推力轴承供气的扩压器供气流道。The air supply channel includes a diffuser air supply channel opened on the diffuser and used for supplying air to the gas thrust bearing.

在一些实施例中,离心式压缩机还包括气体径向轴承,供气流道还包括开设于壳体上且用于向气体推力轴承和/或气体径向轴承供气的壳体供气流道。In some embodiments, the centrifugal compressor further includes a gas radial bearing, and the air supply channel further includes a housing supply air channel opened on the housing and used for supplying air to the gas thrust bearing and/or the gas radial bearing.

在一些实施例中,壳体供气流道包括独立设置的两个主供气流道段,两个主供气流道段包括第一主供气流道段和第二主供气流道段,第一主供气流道段向气体推力轴承供气,第二主供气流道段向气体径向轴承供气。In some embodiments, the housing supply air channel includes two independent main supply air channel segments, the two main supply air channel segments include a first main supply air channel segment and a second main supply air channel segment, the first main supply air channel segment The gas supply channel section supplies gas to the gas thrust bearing, and the second main supply gas channel section supplies gas to the gas radial bearing.

在一些实施例中,离心式压缩机包括推力盘以及分别设置于推力盘的轴向两侧的两个气体推力轴承,第一主供气流道段向两个气体推力轴承的一个直接供气,第一主供气流道段与扩压器供气流道连通以向另一个气体推力轴承供气。In some embodiments, the centrifugal compressor includes a thrust disk and two gas thrust bearings disposed on both axial sides of the thrust disk respectively, and the first main supply flow passage section directly supplies gas to one of the two gas thrust bearings, The first main supply runner section communicates with the diffuser supply runner for supplying gas to another gas thrust bearing.

在一些实施例中,壳体供气流道包括一个主供气流道段,主供气流道段向气体推力轴承和气体径向轴承共同供气。In some embodiments, the housing supply runner includes a main supply runner segment that jointly supplies gas to the gas thrust bearing and the gas radial bearing.

在一些实施例中,壳体供气通道还包括与主供气流道段连通的两个支供气流道段,两个支供气流道段中的一个与扩压器供气流道连通以向气体推力轴承供气,两个支供气流道段中的另一个向气体径向轴承供气。In some embodiments, the housing gas supply channel further includes two branch supply gas channel segments in communication with the main supply gas channel segment, one of the two branch supply gas channel segments in communication with the diffuser supply gas channel for supplying gas to the gas The thrust bearing is supplied with gas, and the other of the two branch gas flow passage sections is supplied with gas to the gas radial bearing.

在一些实施例中,离心式压缩机还包括推力盘以及分别设置于推力盘的轴向两侧的两个气体推力轴承,壳体供气通道还包括与主供气流道段连通的三个支供气流道段,三个支供气流道段包括第一支供气流道段、第二支供气流道段和第三支供气流道段,第一支供气流道段向两个气体推力轴承的一个气体推力轴承直接供气,第二支供气流道段与扩压器供气流道连通以向另一个气体推力轴承供气,第三支供气流道段向气体径向轴承供气。In some embodiments, the centrifugal compressor further includes a thrust disc and two gas thrust bearings respectively disposed on both axial sides of the thrust disc, and the housing air supply channel further includes three branches communicating with the main supply air channel section. The supply air passage section, the three branch air supply passage sections include the first air supply air passage section, the second air supply air passage section and the third air supply air passage section, and the first air supply air passage section is directed to the two gas thrust bearings. One of the gas thrust bearing is directly supplied with gas, the second gas supply channel section is connected with the diffuser supply gas channel to supply gas to the other gas thrust bearing, and the third gas supply channel section supplies gas to the gas radial bearing.

在一些实施例中,主供气流道段的供气压力可调节地设置。In some embodiments, the supply pressure of the main supply runner segment is adjustable.

在一些实施例中,主供气流道段的供气压力被配置为根据容纳腔的压力和/或主轴的振动来调节。In some embodiments, the air supply pressure of the main air supply runner segment is configured to be adjusted according to the pressure of the containment chamber and/or the vibration of the main shaft.

在一些实施例中,主供气流道段的供气压力被配置为根据容纳腔的压力和/或主轴动平衡径向振动位移来调节。In some embodiments, the air supply pressure of the main air supply channel segment is configured to be adjusted according to the pressure of the receiving cavity and/or the dynamic balance radial vibration displacement of the main shaft.

在一些实施例中,离心式压缩机还包括与主供气流道段连接的节流阀,节流阀动作来控制主供气流道段的供气压力。In some embodiments, the centrifugal compressor further includes a throttle valve connected to the main supply flow passage section, and the throttle valve acts to control the supply air pressure of the main supply flow passage section.

本发明第二方面提供一种冷媒循环系统,包括如本发明第一方面任一项提供的离心式压缩机。A second aspect of the present invention provides a refrigerant circulation system, comprising the centrifugal compressor provided in any one of the first aspects of the present invention.

基于本发明提供的技术方案,离心式压缩机包括具有容纳腔的壳体、可转动地设置于容纳腔内的主轴、扩压器、气体推力轴承和供气流道,供气流道包括开设于扩压器上且用于向气体推力轴承供气的扩压器供气流道。本发明的离心式压缩机通过在扩压器上开设扩压器供气流道以向气体推力轴承直接供气,结构简单且加工方便。Based on the technical solution provided by the present invention, the centrifugal compressor includes a casing with an accommodating cavity, a main shaft rotatably arranged in the accommodating cavity, a diffuser, a gas thrust bearing and a supply flow channel, the supply flow channel includes a flow channel opened in the expansion cavity A diffuser supply flow passage on the compressor and used to supply gas to the gas thrust bearing. The centrifugal compressor of the present invention directly supplies gas to the gas thrust bearing by opening the diffuser supply flow passage on the diffuser, and has a simple structure and convenient processing.

通过以下参照附图对本发明的示例性实施例的详细描述,本发明的其它特征及其优点将会变得清楚。Other features and advantages of the present invention will become apparent from the following detailed description of exemplary embodiments of the present invention with reference to the accompanying drawings.

附图说明Description of drawings

此处所说明的附图用来提供对本发明的进一步理解,构成本申请的一部分,本发明的示意性实施例及其说明用于解释本发明,并不构成对本发明的不当限定。在附图中:The accompanying drawings described herein are used to provide a further understanding of the present invention and constitute a part of the present application. The exemplary embodiments of the present invention and their descriptions are used to explain the present invention and do not constitute an improper limitation of the present invention. In the attached image:

图1为本发明一实施例的气体推力轴承的供气流道示意图;FIG. 1 is a schematic diagram of a supply flow passage of a gas thrust bearing according to an embodiment of the present invention;

图2为本发明一实施例的气体径向轴承的供气流道示意图;2 is a schematic diagram of a gas supply flow passage of a gas radial bearing according to an embodiment of the present invention;

图3为本发明另一实施例的气体推力轴承和气体径向轴承的供气流道的结构示意图。FIG. 3 is a schematic structural diagram of the gas supply flow passages of the gas thrust bearing and the gas radial bearing according to another embodiment of the present invention.

各附图标记分别代表:Each reference number represents:

1、壳体;2、堵头;3、推力盘;4、锁紧螺钉;5、叶轮;6、第一气体推力轴承;7、扩压器;8、第二气体推力轴承;9、气体径向轴承;10、主轴;11、主供气流道段;12、挡圈。1. Shell; 2. Plug; 3. Thrust disc; 4. Locking screw; 5. Impeller; 6. First gas thrust bearing; 7. Diffuser; 8. Second gas thrust bearing; 9, Gas Radial bearing; 10. Main shaft; 11. Main supply air passage section; 12. Retaining ring.

具体实施方式Detailed ways

下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,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。以下对至少一个示例性实施例的描述实际上仅仅是说明性的,决不作为对本发明及其应用或使用的任何限制。基于本发明中的实施例,本领域普通技术人员在没有作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 in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, but not all of the embodiments. The following description of at least one exemplary embodiment is merely illustrative in nature and is in no way intended to limit the invention, its application, or uses. 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.

除非另外具体说明,否则在这些实施例中阐述的部件和步骤的相对布置、数字表达式和数值不限制本发明的范围。同时,应当明白,为了便于描述,附图中所示出的各个部分的尺寸并不是按照实际的比例关系绘制的。对于相关领域普通技术人员已知的技术、方法和设备可能不作详细讨论,但在适当情况下,所述技术、方法和设备应当被视为授权说明书的一部分。在这里示出和讨论的所有示例中,任何具体值应被解释为仅仅是示例性的,而不是作为限制。因此,示例性实施例的其它示例可以具有不同的值。应注意到:相似的标号和字母在下面的附图中表示类似项,因此,一旦某一项在一个附图中被定义,则在随后的附图中不需要对其进行进一步讨论。The relative arrangement of the components and steps, the numerical expressions and numerical values set forth in these embodiments do not limit the scope of the invention unless specifically stated otherwise. Meanwhile, it should be understood that, for the convenience of description, the dimensions of various parts shown in the accompanying drawings are not drawn in an actual proportional relationship. Techniques, methods, and devices known to those of ordinary skill in the relevant art may not be discussed in detail, but where appropriate, such techniques, methods, and devices should be considered part of the authorized description. In all examples shown and discussed herein, any specific value should be construed as illustrative only and not as limiting. Accordingly, other examples of exemplary embodiments may have different values. It should be noted that like numerals and letters refer to like items in the following figures, so once an item is defined in one figure, it does not require further discussion in subsequent figures.

为了便于描述,在这里可以使用空间相对术语,如“在……之上”、“在……上方”、“在……上表面”、“上面的”等,用来描述如在图中所示的一个器件或特征与其他器件或特征的空间位置关系。应当理解的是,空间相对术语旨在包含除了器件在图中所描述的方位之外的在使用或操作中的不同方位。例如,如果附图中的器件被倒置,则描述为“在其他器件或构造上方”或“在其他器件或构造之上”的器件之后将被定位为“在其他器件或构造下方”或“在其他器件或构造之下”。因而,示例性术语“在……上方”可以包括“在……上方”和“在……下方”两种方位。该器件也可以其他不同方式定位(旋转90度或处于其他方位),并且对这里所使用的空间相对描述作出相应解释。For ease of description, spatially relative terms, such as "on", "over", "on the surface", "above", etc., may be used herein to describe what is shown in the figures. The spatial positional relationship of one device or feature shown to other devices or features. It should be understood that spatially relative terms are intended to encompass different orientations of the device in use or operation in addition to the orientation depicted in the figures. For example, if the device in the figures is turned over, elements described as "above" or "over" other devices or features would then be oriented "below" or "over" the other devices or features under other devices or constructions". Thus, the exemplary term "above" can encompass both an orientation of "above" and "below." The device may also be otherwise oriented (rotated 90 degrees or at other orientations) and the spatially relative descriptions used herein interpreted accordingly.

如图1至图3所示,本发明实施例的离心式压缩机包括:As shown in FIG. 1 to FIG. 3 , the centrifugal compressor of the embodiment of the present invention includes:

壳体1,具有容纳腔;Shell 1, with an accommodating cavity;

主轴10,可转动地设置于容纳腔内;The main shaft 10 is rotatably arranged in the accommodating cavity;

扩压器7;Diffuser 7;

气体推力轴承;和gas thrust bearings; and

供气流道,包括开设于扩压器7上且用于向气体推力轴承供气的扩压器供气流道71。The air supply channel includes a diffuser air supply channel 71 opened on the diffuser 7 and used for supplying air to the gas thrust bearing.

本发明实施例的离心式压缩机通过在扩压器7上开设扩压器供气流道71以向气体推力轴承直接供气,结构简单且加工方便。In the centrifugal compressor of the embodiment of the present invention, the diffuser supply flow passage 71 is provided on the diffuser 7 to directly supply gas to the gas thrust bearing, and the structure is simple and the processing is convenient.

本发明实施例的压缩机还包括连接于主轴10端部的叶轮5、扩压器7、推力盘3、分别设置于推力盘3的轴向两侧的第一气体推力轴承6和第二气体推力轴承8以及用于将主轴10可转动地支撑于壳体1内的气体径向轴承9。具体地,叶轮5通过叶轮锁紧螺钉4与主轴10固定连接。The compressor of the embodiment of the present invention further includes an impeller 5 connected to the end of the main shaft 10 , a diffuser 7 , a thrust disc 3 , a first gas thrust bearing 6 and a second gas thrust bearing respectively disposed on both axial sides of the thrust disc 3 . The thrust bearing 8 and the gas radial bearing 9 for rotatably supporting the main shaft 10 in the housing 1 . Specifically, the impeller 5 is fixedly connected to the main shaft 10 through the impeller locking screw 4 .

本实施例的气体推力轴承和气体径向轴承均包括多孔介质。供气流道将气体流通至多孔介质。Both the gas thrust bearing and the gas radial bearing of this embodiment include porous media. The supply flow channel circulates the gas to the porous medium.

本实施例的供气流道还包括开设于壳体1上的壳体供气流道。The air supply channel of this embodiment further includes a housing air supply air channel opened on the housing 1 .

如图1和图2所示,本实施例的壳体供气流道包括两个主供气流道段,两个主供气流道段分别为第一主供气流道段11A和第二主供气流道段11B,第一主供气流道段11A向气体推力轴承供气(图1示出),第二主供气流道段11B向气体径向轴承9供气(图2示出)。如图1所示,第一主供气流道段11A与扩压器供气流道71连通以向第一气体推力轴承6供气,第一主供气流道段11A直接向第二气体推力轴承8供气。气体经过推力轴承内部节流进入到推力轴承与推力盘3之间的间隙内并形成具有压力的气膜,气膜作用在推力盘3上抵消系统轴向力。气体进入气体径向轴承9与主轴10之间的间隙,与旋转动压效应一起形成楔形气膜,润滑支承主轴10。As shown in FIG. 1 and FIG. 2 , the housing air supply air passage in this embodiment includes two main air supply air passage sections, and the two main air supply air passage sections are the first main air supply air passage section 11A and the second main air supply air passage section 11A respectively. In the channel section 11B, the first main supply flow channel section 11A supplies gas to the gas thrust bearing (shown in FIG. 1 ), and the second main supply flow channel section 11B supplies gas to the gas radial bearing 9 (shown in FIG. 2 ). As shown in FIG. 1 , the first main supply flow passage section 11A communicates with the diffuser supply flow passage 71 to supply air to the first gas thrust bearing 6 , and the first main supply flow passage section 11A directly supplies the second gas thrust bearing 8 gas supply. The gas passes through the internal throttle of the thrust bearing and enters into the gap between the thrust bearing and the thrust plate 3 and forms a gas film with pressure, and the gas film acts on the thrust plate 3 to offset the axial force of the system. The gas enters the gap between the gas radial bearing 9 and the main shaft 10 , and forms a wedge-shaped gas film together with the effect of rotational dynamic pressure, which lubricates and supports the main shaft 10 .

具体地,扩压器供气流道71包括相互垂直设置的第一扩压器供气流道和第二扩压器供气流道,其中,第一扩压器供气流道竖直设置且其端部设置有堵头2以防止气体泄漏;第二扩压器供气流道沿轴向设置并且开口设置于扩压器的端面上以便于与壳体1上的主供气流道段连通。Specifically, the diffuser supply flow channel 71 includes a first diffuser supply flow channel and a second diffuser supply flow channel which are arranged perpendicular to each other, wherein the first diffuser supply flow channel is vertically arranged and its end is A plug 2 is provided to prevent gas leakage; the second diffuser supply flow channel is arranged in the axial direction and the opening is arranged on the end face of the diffuser so as to communicate with the main supply flow channel section on the housing 1 .

本实施例的壳体供气流道分别设置两个主供气流道段,第一主供气流道段11A向气体推力轴承供气,第二主供气流道段11B向气体径向轴承供气,也就是说气体推力轴承和气体径向轴承分开供气且两个主供气流道段的供气压力可调节地设置,防止气锤振动产生,提高系统稳定性。而且本实施例的离心压缩机通过在扩压器7和壳体1上钻孔来形成供气流道,结构形式简单且加工方便。In this embodiment, two main air supply air passages are respectively set in the housing air supply air passage. The first main air supply air passage segment 11A supplies air to the gas thrust bearing, and the second main air supply air passage segment 11B supplies air to the gas radial bearing. That is to say, the gas thrust bearing and the gas radial bearing are separately supplied with gas, and the gas supply pressures of the two main supply air passage sections are set in an adjustable manner, so as to prevent the vibration of the gas hammer and improve the stability of the system. Moreover, in the centrifugal compressor of this embodiment, the air supply passage is formed by drilling holes on the diffuser 7 and the casing 1, and the structure is simple and the processing is convenient.

如图3所示,在另一实施例中,壳体供气流道包括一个主供气流道段11,该主供气流道段11为气体推力轴承和气体径向轴承共同供气,因此只要调节该主供气流道段11的供气压力就可以调节所有轴承的供气压力,调节方便。As shown in FIG. 3 , in another embodiment, the housing supply flow channel includes a main supply flow channel section 11 , and the main supply flow channel section 11 jointly supplies gas for the gas thrust bearing and the gas radial bearing, so as long as the adjustment is made The air supply pressure of the main air supply air passage section 11 can adjust the air supply pressure of all the bearings, and the adjustment is convenient.

具体地,如图3所示,本实施例的壳体供气流道包括与所述主供气流道段11连通的两个支供气流道段,两个支供气流道段中的一个与扩压器供气流道连通以向所述气体推力轴承供气,两个支供气流道段中的另一个向气体径向轴承9供气。Specifically, as shown in FIG. 3 , the housing air supply flow channel of this embodiment includes two branch supply air channel sections that communicate with the main supply air channel section 11 , and one of the two branch supply air channel sections is connected to the expansion channel section 11 . The compressor supply runners communicate to supply gas to the gas thrust bearing, and the other of the two branch supply runner segments supplies gas to the gas radial bearing 9 .

由于本实施例的离心式压缩机包括两个气体推力轴承,因此壳体供气流道包括与主供气流道段11连通的三个支供气流道段。Since the centrifugal compressor of this embodiment includes two gas thrust bearings, the housing supply flow channel includes three branch supply flow channel sections that communicate with the main supply flow channel section 11 .

三个支供气流道段包括第一支供气流道段、第二支供气流道段和第三支供气流道段,第一支供气流道段向两个气体推力轴承的一个气体推力轴承直接供气,第二支供气流道段与扩压器供气流道71连通以向另一个气体推力轴承供气,第三支供气流道段向气体径向轴承9供气。The three branch air supply passage sections include a first air supply air passage section, a second air supply air passage section and a third air supply air passage section, and the first air supply air passage section is directed to one gas thrust bearing of the two gas thrust bearings. For direct gas supply, the second gas supply channel section is communicated with the diffuser gas supply channel 71 to supply gas to another gas thrust bearing, and the third gas supply channel section supplies gas to the gas radial bearing 9 .

本实施例的主供气流道段的供气压力可调节地设置。具体地,本实施例的主供气流道段的供气压力根据容纳腔的压力和主轴的振动来调节。在压缩机运行过程中可以根据容纳腔的压力和主轴的振动来调节主供气流道段的供气压力从而调节轴承的刚度和承载能力,防止气锤振动产生。The air supply pressure of the main air supply air passage section of this embodiment can be set in an adjustable manner. Specifically, the air supply pressure of the main air supply air passage section in this embodiment is adjusted according to the pressure of the accommodating cavity and the vibration of the main shaft. During the operation of the compressor, the air supply pressure of the main air supply passage section can be adjusted according to the pressure of the accommodating chamber and the vibration of the main shaft, so as to adjust the stiffness and bearing capacity of the bearing and prevent the occurrence of air hammer vibration.

在具体实施例中,可以根据主轴动平衡径向振动位移来对主供气流道段的供气压力进行调节。In a specific embodiment, the air supply pressure of the main air supply channel section can be adjusted according to the dynamic balance radial vibration displacement of the main shaft.

在一些实施例中,离心式压缩机还包括与主供气流道段连接的节流阀,节流阀动作来控制主供气流道段的供气压力。In some embodiments, the centrifugal compressor further includes a throttle valve connected to the main supply flow passage section, and the throttle valve acts to control the supply air pressure of the main supply flow passage section.

如图1所示,本实施例的离心式压缩机还包括设置于气体径向轴承9端部的挡圈12。As shown in FIG. 1 , the centrifugal compressor of this embodiment further includes a retaining ring 12 disposed at the end of the gas radial bearing 9 .

最后应当说明的是:以上实施例仅用以说明本发明的技术方案而非对其限制;尽管参照较佳实施例对本发明进行了详细的说明,所属领域的普通技术人员应当理解:依然可以对本发明的具体实施方式进行修改或者对部分技术特征进行等同替换;而不脱离本发明技术方案的精神,其均应涵盖在本发明请求保护的技术方案范围当中。Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention and not to limit them; although the present invention has been described in detail with reference to the preferred embodiments, those of ordinary skill in the art should understand: The specific embodiments of the invention are modified or some technical features are equivalently replaced; without departing from the spirit of the technical solutions of the present invention, all of them should be included in the scope of the technical solutions claimed in the present invention.

Claims (12)

1. A centrifugal compressor, comprising:
a housing (1) having a receiving cavity;
the main shaft (10) is rotatably arranged in the accommodating cavity;
a diffuser (7);
a gas thrust bearing; and
and the gas supply flow channel comprises a diffuser gas supply flow channel (71) which is arranged on the diffuser (7) and used for supplying gas to the gas thrust bearing.
2. A centrifugal compressor according to claim 1, further comprising a gas radial bearing (9), the gas supply channel further comprising a housing gas supply channel opening on the housing (1) and serving to supply gas to the gas thrust bearing and/or the gas radial bearing (9).
3. The centrifugal compressor according to claim 2, wherein the housing gas supply flow passage comprises two main gas supply flow passage sections (11) provided independently, the two main gas supply flow passage sections comprising a first main gas supply flow passage section (11A) and a second main gas supply flow passage section (11B), the first main gas supply flow passage section (11A) supplying gas to the gas thrust bearing, the second main gas supply flow passage section (11B) supplying gas to the gas radial bearing (9).
4. A centrifugal compressor according to claim 3, comprising a thrust disc (3) and two of said gas thrust bearings respectively disposed on both axial sides of said thrust disc (3), said first main gas supply flow path section (11A) supplying gas directly to one of said two gas thrust bearings, said first main gas supply flow path section (11A) communicating with said gas supply flow path (71) to supply gas to the other gas thrust bearing.
5. A centrifugal compressor according to claim 2, wherein the housing gas supply channel comprises a main gas supply channel section (11), the main gas supply channel section (11) supplying gas to both the gas thrust bearing and the gas radial bearing (9).
6. The centrifugal compressor according to claim 5, wherein the housing gas supply passage further comprises two branch gas supply flow path sections communicating with the main gas supply flow path section (11), one of the two branch gas supply flow path sections communicating with the diffuser gas supply flow path (71) to supply gas to the gas thrust bearing, and the other of the two branch gas supply flow path sections supplying gas to the gas radial bearing (9).
7. The centrifugal compressor according to claim 5, wherein the centrifugal compressor further comprises a thrust disk (3) and two of the gas thrust bearings respectively disposed at axial both sides of the thrust disk (3), the housing gas supply passage further comprises three branch gas supply flow passage sections communicated with the main gas supply flow passage section (11), the three branch gas supply flow passage sections comprise a first branch gas supply flow passage section, a second branch gas supply flow passage section and a third branch gas supply flow passage section, the first branch gas supply flow passage section directly supplies gas to one of the two gas thrust bearings, the second branch gas supply flow passage section is communicated with the diffuser gas supply flow passage (71) to supply gas to the other gas thrust bearing, and the third branch gas supply flow passage section supplies gas to the gas radial bearing.
8. A centrifugal compressor according to any one of claims 3 to 7, characterized in that the supply pressure of the main supply flow channel section (11) is adjustably set.
9. A centrifugal compressor according to claim 8, characterized in that the supply air pressure of the main supply flow channel section (11) is configured to be adjusted in dependence of the pressure of the receiving chamber and/or the vibration of the main shaft.
10. A centrifugal compressor according to claim 8, characterized in that the supply air pressure of the main supply flow channel section (11) is configured to be adjusted in dependence of the pressure of the receiving chamber and/or the main shaft dynamic balance radial vibration displacement.
11. A centrifugal compressor according to claim 8, further comprising a throttle valve connected to the main gas supply channel section (11), the throttle valve acting to control the gas supply pressure of the main gas supply channel section (11).
12. A refrigerant circulation system comprising a centrifugal compressor according to any one of claims 1 to 11.
CN201811595302.2A 2018-12-25 2018-12-25 Centrifugal Compressor and Refrigerant Circulation System with Diffuser Supply Flow Path Pending CN111365259A (en)

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Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN202280648U (en) * 2011-10-31 2012-06-20 珠海格力电器股份有限公司 Bearing for centrifugal compressor, centrifugal compressor and air conditioning system
US20140286599A1 (en) * 2012-01-03 2014-09-25 New Way Machine Components, Inc. Air bearing for use as seal
CN104948478A (en) * 2014-03-26 2015-09-30 霍尼韦尔国际公司 Electric motor-driven compressor having a heat shield forming a wall of a diffuser
CN106015032A (en) * 2016-06-28 2016-10-12 杭州万辰机电科技有限公司 Centrifugal compressor
KR20170058082A (en) * 2015-11-18 2017-05-26 한온시스템 주식회사 Air blower for vehicle
CN209340165U (en) * 2018-12-25 2019-09-03 珠海格力电器股份有限公司 Centrifugal compressor with diffuser air supply flow channel and refrigerant circulating system

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006020102A1 (en) * 2006-04-29 2007-10-31 Leybold Vacuum Gmbh Lubricant-free vacuum pump used as a turbo molecular pump comprises a gas bearing surface facing a shaft and/or a gas bearing rotor and having a hard layer
KR101712723B1 (en) * 2015-03-25 2017-03-07 한국기계연구원 Apparatus for controlling thrust and cooling bearing using compressed air
CN106369056B (en) * 2016-12-05 2019-06-21 中国工程物理研究院机械制造工艺研究所 Turbocharger
CN108999793A (en) * 2018-08-12 2018-12-14 西安交通大学 A kind of centrifugal compressor
CN209340163U (en) * 2018-12-25 2019-09-03 珠海格力电器股份有限公司 Compressor for optimizing internal space

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN202280648U (en) * 2011-10-31 2012-06-20 珠海格力电器股份有限公司 Bearing for centrifugal compressor, centrifugal compressor and air conditioning system
US20140286599A1 (en) * 2012-01-03 2014-09-25 New Way Machine Components, Inc. Air bearing for use as seal
CN104948478A (en) * 2014-03-26 2015-09-30 霍尼韦尔国际公司 Electric motor-driven compressor having a heat shield forming a wall of a diffuser
KR20170058082A (en) * 2015-11-18 2017-05-26 한온시스템 주식회사 Air blower for vehicle
CN106015032A (en) * 2016-06-28 2016-10-12 杭州万辰机电科技有限公司 Centrifugal compressor
CN209340165U (en) * 2018-12-25 2019-09-03 珠海格力电器股份有限公司 Centrifugal compressor with diffuser air supply flow channel and refrigerant circulating system

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