WO2023061271A1 - Impeller assembly and mixing apparatus - Google Patents

Impeller assembly and mixing apparatus Download PDF

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Publication number
WO2023061271A1
WO2023061271A1 PCT/CN2022/123953 CN2022123953W WO2023061271A1 WO 2023061271 A1 WO2023061271 A1 WO 2023061271A1 CN 2022123953 W CN2022123953 W CN 2022123953W WO 2023061271 A1 WO2023061271 A1 WO 2023061271A1
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WO
WIPO (PCT)
Prior art keywords
guide groove
impeller
baffle
impeller assembly
blade
Prior art date
Application number
PCT/CN2022/123953
Other languages
French (fr)
Chinese (zh)
Inventor
石桥
徐勇程
白淑娟
金旭东
Original Assignee
深圳市尚水智能设备有限公司
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by 深圳市尚水智能设备有限公司 filed Critical 深圳市尚水智能设备有限公司
Priority to US18/550,414 priority Critical patent/US20240189786A1/en
Priority to KR1020237035221A priority patent/KR20230155578A/en
Priority to EP22880210.4A priority patent/EP4292698A1/en
Priority to JP2023558648A priority patent/JP2024511147A/en
Publication of WO2023061271A1 publication Critical patent/WO2023061271A1/en

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01FMIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
    • B01F27/00Mixers with rotary stirring devices in fixed receptacles; Kneaders
    • B01F27/27Mixers with stator-rotor systems, e.g. with intermeshing teeth or cylinders or having orifices
    • B01F27/271Mixers with stator-rotor systems, e.g. with intermeshing teeth or cylinders or having orifices with means for moving the materials to be mixed radially between the surfaces of the rotor and the stator
    • B01F27/2711Mixers with stator-rotor systems, e.g. with intermeshing teeth or cylinders or having orifices with means for moving the materials to be mixed radially between the surfaces of the rotor and the stator provided with intermeshing elements
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01FMIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
    • B01F27/00Mixers with rotary stirring devices in fixed receptacles; Kneaders
    • B01F27/05Stirrers
    • B01F27/11Stirrers characterised by the configuration of the stirrers
    • B01F27/111Centrifugal stirrers, i.e. stirrers with radial outlets; Stirrers of the turbine type, e.g. with means to guide the flow
    • B01F27/1111Centrifugal stirrers, i.e. stirrers with radial outlets; Stirrers of the turbine type, e.g. with means to guide the flow with a flat disc or with a disc-like element equipped with blades, e.g. Rushton turbine
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01FMIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
    • B01F27/00Mixers with rotary stirring devices in fixed receptacles; Kneaders
    • B01F27/05Stirrers
    • B01F27/11Stirrers characterised by the configuration of the stirrers
    • B01F27/113Propeller-shaped stirrers for producing an axial flow, e.g. shaped like a ship or aircraft propeller
    • B01F27/1132Propeller-shaped stirrers for producing an axial flow, e.g. shaped like a ship or aircraft propeller with guiding tubes or tubular segments fixed to and surrounding the tips of the propeller blades, e.g. for supplementary mixing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01FMIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
    • B01F27/00Mixers with rotary stirring devices in fixed receptacles; Kneaders
    • B01F27/60Mixers with rotary stirring devices in fixed receptacles; Kneaders with stirrers rotating about a horizontal or inclined axis
    • B01F27/71Mixers with rotary stirring devices in fixed receptacles; Kneaders with stirrers rotating about a horizontal or inclined axis with propellers
    • B01F27/711Mixers with rotary stirring devices in fixed receptacles; Kneaders with stirrers rotating about a horizontal or inclined axis with propellers co-operating with stationary guiding means, e.g. baffles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01FMIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
    • B01F27/00Mixers with rotary stirring devices in fixed receptacles; Kneaders
    • B01F27/80Mixers with rotary stirring devices in fixed receptacles; Kneaders with stirrers rotating about a substantially vertical axis
    • B01F27/86Mixers with rotary stirring devices in fixed receptacles; Kneaders with stirrers rotating about a substantially vertical axis co-operating with deflectors or baffles fixed to the receptacle
    • B01F27/861Mixers with rotary stirring devices in fixed receptacles; Kneaders with stirrers rotating about a substantially vertical axis co-operating with deflectors or baffles fixed to the receptacle the baffles being of cylindrical shape, e.g. a mixing chamber surrounding the stirrer, the baffle being displaced axially to form an interior mixing chamber
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01FMIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
    • B01F35/00Accessories for mixers; Auxiliary operations or auxiliary devices; Parts or details of general application
    • B01F35/71Feed mechanisms
    • B01F35/717Feed mechanisms characterised by the means for feeding the components to the mixer
    • B01F35/7175Feed mechanisms characterised by the means for feeding the components to the mixer using propellers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01FMIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
    • B01F2215/00Auxiliary or complementary information in relation with mixing
    • B01F2215/04Technical information in relation with mixing
    • B01F2215/0413Numerical information
    • B01F2215/0418Geometrical information
    • B01F2215/0422Numerical values of angles

Definitions

  • the present application relates to the technical field of solid and liquid mixing equipment, in particular to an impeller assembly and a mixing device.
  • the airfoil of the inner blade and the flow channel of the fluid there is no special design for the airfoil of the inner blade and the flow channel of the fluid.
  • the blade has limited ability to work on the fluid, and the multi-layer baffle will greatly hinder the movement of the fluid, making it difficult to discharge the material. Therefore, it is necessary to use the baffle
  • the fluid is accelerated and expelled by the work of the discharge vanes on the outside of the plate.
  • the forced acceleration and discharge of the fluid by the discharge blade will cause large pressure fluctuations in the discharge chamber, causing pulsation of the discharge flow, generating large noise and vibration, and reducing the working efficiency of the dispersion device.
  • the purpose of this application is to provide an impeller assembly and a mixing device to solve the above-mentioned problems in the prior art, and to solve the problem of unstable discharge, vibration, etc. And noise, work efficiency is not high enough.
  • the present application provides an impeller assembly, including a relatively rotating impeller structure and a housing structure, the impeller structure includes a body, the surface of the body is provided with several backward curved blades along the circumference of the body, the body The lower part is provided with at least one layer of first baffles, and the first baffles are arranged on the outer sides of each of the backward curved blades, and the shell structure includes at least one layer of second baffles, and the second baffles are located on the The inner side and/or the outer side of the first baffle, the first baffle is provided with a number of first guide grooves, the second baffle is provided with a number of second guide grooves, the fluid flows from the inlet of the upper part of the body Enter, flow along the surface of the body, and flow out through the outlet of the lower part of the body, the first guide groove and the second guide groove, and the centerline of the first guide groove rotates to the impeller structure The direction is deflected in the opposite direction, and the center line of the second guide groove
  • the size of the body gradually increases from the upper part of the body to the lower part of the body, and the surface of the body is a curved surface.
  • the blade angle of the backward curved blade on any flow surface gradually decreases and then gradually increases from the inlet to the outlet, and the blade angle is the tangent of the surface arc of the backward curved blade and The included angle of the axial surface of the impeller structure.
  • the blade angle at the inlet is 20-80°, and the blade angle at the outlet is 0-30°.
  • the included angle between the centerline of the first guide groove and the radial direction of the central axis of the body is 15-50°.
  • the included angle between the centerline of the second guide groove and the radial direction of the central axis of the body is 35-80°.
  • the present application also provides a mixing device, including the impeller assembly.
  • the backward curved blade adopted in this application can achieve better coupling with the flow of fluid when it rotates, so that the backward curved blade arranged on the body can perform work on the fluid more efficiently; especially, it is found through simulation calculation that the backward curved blade can
  • the blade angle on the surface is designed to decrease first and then increase from the inlet to the outlet, which can make the backward curved blade work on the fluid more efficiently; on the other hand, by setting the first guide groove on the first baffle and the A second guide groove is provided to reduce kinetic energy loss when the fluid passes through the first baffle plate and the second baffle plate through the direction of the first guide groove and the second guide groove.
  • the fluid After the fluid is dispersed through the dispersion area between the first baffle and the second baffle, it still has enough kinetic energy to be discharged by centrifugal means, and there is no need to add discharge blades that work on the fluid, which greatly reduces the impact on the discharge.
  • the turbulence of the fluid in the material area keeps the fluid pressure in the discharge area uniform and stable, and the fluid can be discharged at a stable flow rate, eliminating the vibration and noise caused by pulsation.
  • Fig. 1 is the schematic diagram of the impeller assembly of the present application
  • Fig. 2 is A-A sectional view of Fig. 1;
  • Figure 3 is a partial enlarged view of I in Figure 2;
  • Fig. 4 is the structural representation of the impeller of the present application.
  • Fig. 5 is a schematic diagram of the shell structure of the present application.
  • 100-impeller assembly 100-impeller assembly, 1-impeller structure, 2-housing structure, 3-body, 4-backward curved blade, 5-first baffle, 6-second baffle, 7-first guide groove, 8 - Second guide slot.
  • the purpose of this application is to provide an impeller assembly and a mixing device to solve the above-mentioned problems in the prior art, and to solve the problem of unstable discharge, vibration, etc. And noise, work efficiency is not high enough.
  • this embodiment provides an impeller assembly 100, including a relatively rotating impeller structure 1 and a housing structure 2, the impeller structure 1 includes a body 3, and the surface of the body 3 is along the circumference of the body 3 Several backward curved blades 4 are provided, at least one layer of first baffles 5 is provided on the lower part of the body 3, and the first baffles 5 are arranged on the outside of each backward curved blade 4, and the shell structure 2 includes at least one layer of second baffles 6.
  • the second baffle 6 is located on the inside and/or outside of the first baffle 5.
  • the shell structure 2 is provided with two layers of second baffles 6 inside and outside, which are respectively located on the inside of the first baffle 5.
  • the second baffle 6 is nested and fastened on the periphery of the first baffle 5, and the first baffle 5 is provided with a plurality of first guide grooves 7 along the circumferential direction, and the first guide grooves 7 are evenly distributed on the first baffle plate 5, and a number of second guide grooves 8 are opened on the second baffle plate 6 of the inner and outer layers along the circumferential direction, and the second guide grooves 8 are evenly distributed on the second
  • the cross-sectional shape of the first guide groove 7 and the second guide groove 8 is similar to a rhombus, and the deflections of the first guide groove 7 and the second guide groove 8 are arranged alternately.
  • the upper end of the body 3 of 1 is provided with a fluid inlet, and the lower end of the body 3 of the impeller structure 1 is provided with a fluid outlet.
  • the outlet, the inner second guide groove 8, the first guide groove 7 and the outer second guide groove 8 flow out, and the centerline of the first guide groove 7 deflects to the opposite direction of the impeller structure 1's rotation direction , the center line of the second guide groove 8 deflects to the rotation direction of the impeller structure 1 .
  • the impeller structure 1 rotates clockwise around the axis of the body 3 based on the placement direction in FIG. 2 .
  • the size of the body 3 gradually increases from the upper part of the body 3 to the lower part of the body 3, the body 3 is in the shape of a truncated cone, and the surface of the body 3 is a curved surface.
  • the meridian channel line of the main body 3 from the inlet to the outlet is an inwardly bent arc-like curve.
  • the blade angle of the curved blade 4 on any flow surface gradually decreases from the inlet to the outlet and then gradually increases, and the blade angle is the tangent of the curved blade 4 surface arc and the axial surface of the impeller structure 1 Angle, and take a positive value.
  • the gap between the backward curved blade 4 and the casing changes continuously and smoothly from the inlet to the outlet.
  • the blade angle at the inlet is 20-80°
  • the blade angle at the outlet is 0-30°
  • the smallest blade angle is 0-30°.
  • the angular distribution of the blade angle is related to the aerodynamic load distribution of the backward-curved blade 4. According to the fluid simulation results in the backward-curved blade 4, the angular distribution of the blade angle is adjusted to achieve a better coupling between the fluid flow and the backward-curved blade 4, so as to ensure that the backward-curved blade 4 work efficiently on the fluid.
  • the included angle (ie ⁇ 2 ) between the centerline of the first guide groove 7 and the radial direction of the central axis of the body 3 is 15-50°.
  • the included angle (ie ⁇ 1 and ⁇ 3 ) between the center line of the second guide groove 8 and the radial direction of the center axis of the body 3 is 35-80°.
  • ⁇ 1 is the angle between the center line L1 and the radial line R1 of the second guide groove 8 inside
  • ⁇ 2 is the angle between the center line L2 and the radial line R2 of the first guide groove 7
  • ⁇ 3 is the angle between the centerline L3 of the second outer guide groove 8 and the radial line R3.
  • the radial line R1 , the radial line R2 and the radial line R3 are all radial lines starting from the central axis of the body 3 .
  • the intersection point of the centerline L1 of the second guide groove 8 of the second baffle plate 6 of the inner layer and the radial line R1 is located on the circumference where the inner wall of the second baffle plate 6 of the inner layer is located, and the centerline L2 of the first guide groove 7
  • the intersection point with the radial line R2 is located on the circumference where the inner wall of the first baffle plate 5 is located, and the intersection point with the center line L3 of the second guide groove 8 of the second baffle plate 6 of the outer layer and the radial line R3 is located at the second outer layer.
  • the direction of rotation of the impeller assembly 100 is shown by the arrow in Figure 3.
  • this embodiment controls the fluid load distribution of the backward curved blade 4 by adjusting the blade angle.
  • the distribution of the blade angle makes the rotation of the backward curved blade 4 and the flow of the fluid better Coupling, so that the backward curved blade 4 set on the body 3 can work on the fluid more efficiently;
  • by opening the first guide groove 7 on the first baffle 5 and the second guide groove 8 on the second baffle by opening the first guide groove 7 on the first baffle 5 and the second guide groove 8 on the second baffle , the kinetic energy loss when the fluid passes through the first baffle plate 5 and the second baffle plate 6 is reduced by the direction of the first guide groove 7 and the second guide groove 8 .
  • the second baffle plate 6 fixed on the housing structure 2 is stationary, and the center line of the second guide groove 8 deflects to the rotation direction of the impeller structure 1, which can make the fluid flow smoothly without changing the direction greatly. through the second guide groove 8.
  • the first baffle plate 5 fixed on the impeller structure 1 rotates together with the impeller structure 1, which can be regarded as the extension of the backward curved blade 4 except the first guide groove 7, and the first guide groove 7 also serves as Into a backbent structure, which is more conducive to doing work on the fluid.
  • the discharge vane that works on the fluid greatly reduces the disturbance of the fluid in the discharge area, so that the fluid pressure in the discharge area can be kept uniform and stable, and the fluid can be discharged at a stable flow rate, eliminating the vibration and vibration caused by pulsation noise.
  • This embodiment provides a mixing device including the impeller assembly 100 of the first embodiment.

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  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Mixers Of The Rotary Stirring Type (AREA)

Abstract

The present application discloses an impeller assembly and a mixing apparatus and relates to the technical field of solid and liquid mixing devices. The impeller assembly comprises an impeller structure and a housing structure. The impeller structure comprises a body, and the surface of the body is provided with multiple backward-curved blades, the blade angles of the backward-curved blades on any flow surface first decreasing and then increasing from an inlet to an outlet. A first baffle is disposed on a lower portion of the body, and the housing structure comprises a second baffle. The first baffle is provided with a first guide groove, and the second baffle is provided with a second guide groove. A fluid enters from an inlet in an upper portion of the body, flows along the surface of the body, and flows out by means of an outlet in a lower portion of the body, the first guide groove and the second guide groove. The center line of the first guide groove is deflected towards a direction opposite to the direction of rotation of the impeller structure, and the center line of the second guide groove is deflected towards the direction of rotation of the impeller structure. The present application solves the problems that discharge is unstable, there is a large amount of vibration and noise, and the working efficiency is insufficient.

Description

一种叶轮组件及混合装置A kind of impeller assembly and mixing device
本申请要求在2021年10月13日提交中国专利局、申请号为202111190681.9、发明名称为“一种叶轮组件及混合装置”的中国专利申请的优先权,其全部内容通过引用结合在本申请中。This application claims the priority of the Chinese patent application with the application number 202111190681.9 and the title of the invention "An impeller assembly and mixing device" submitted to the China Patent Office on October 13, 2021, the entire contents of which are incorporated by reference in this application .
技术领域technical field
本申请涉及固体和液体混合设备技术领域,特别是涉及一种叶轮组件及混合装置。The present application relates to the technical field of solid and liquid mixing equipment, in particular to an impeller assembly and a mixing device.
背景技术Background technique
相关技术中对内侧叶片的叶型以及流体的流道没有特殊设计,叶片对流体的做功能力有限,且多层挡板对流体的运动产生较大的阻碍使得出料困难,因此需要利用挡板外侧的排料叶片的做功将流体加速并排出。但是排料叶片对流体的强制加速和排出会导致出料腔内的压力波动大,引起出料流量的脉动,产生大的噪音和振动,并降低了分散装置的工作效率。In the related art, there is no special design for the airfoil of the inner blade and the flow channel of the fluid. The blade has limited ability to work on the fluid, and the multi-layer baffle will greatly hinder the movement of the fluid, making it difficult to discharge the material. Therefore, it is necessary to use the baffle The fluid is accelerated and expelled by the work of the discharge vanes on the outside of the plate. However, the forced acceleration and discharge of the fluid by the discharge blade will cause large pressure fluctuations in the discharge chamber, causing pulsation of the discharge flow, generating large noise and vibration, and reducing the working efficiency of the dispersion device.
发明内容Contents of the invention
本申请的目的是提供一种叶轮组件及混合装置,以解决上述现有技术存在的问题,解决了固液混合物粘度大时采用离心式出料方式的分散装置容易出现的出料不稳定、振动和噪音大、工作效率不够高的问题。The purpose of this application is to provide an impeller assembly and a mixing device to solve the above-mentioned problems in the prior art, and to solve the problem of unstable discharge, vibration, etc. And noise, work efficiency is not high enough.
为实现上述目的,本申请提供了如下方案:In order to achieve the above object, the application provides the following scheme:
本申请提供了一种叶轮组件,包括相对转动的叶轮结构和壳体结构,所述叶轮结构包括本体,所述本体的表面沿所述本体的周向设置有若干后弯叶片,所述本体的下部设置有至少一层第一挡板,所述第一挡板设置在各所述后弯叶片的外侧,所述壳体结构包括至少一层第二挡板,所述第二挡板位于所述第一挡板的内侧和/或外侧,所述第一挡板上开设有若干第一导向槽,所述第二挡板上开设有若干第二导向槽,流体从所述本体上部的进口进入,沿所述本体的表面流动,通过所述本体的下部的出口、所述第一导向槽和所述第二导向槽流出,所述第一导向槽的中心线向所述叶轮结构的转动方向的反方向偏转,所述第二导向槽的中心线向所述叶轮结构的转动方向偏转。。The present application provides an impeller assembly, including a relatively rotating impeller structure and a housing structure, the impeller structure includes a body, the surface of the body is provided with several backward curved blades along the circumference of the body, the body The lower part is provided with at least one layer of first baffles, and the first baffles are arranged on the outer sides of each of the backward curved blades, and the shell structure includes at least one layer of second baffles, and the second baffles are located on the The inner side and/or the outer side of the first baffle, the first baffle is provided with a number of first guide grooves, the second baffle is provided with a number of second guide grooves, the fluid flows from the inlet of the upper part of the body Enter, flow along the surface of the body, and flow out through the outlet of the lower part of the body, the first guide groove and the second guide groove, and the centerline of the first guide groove rotates to the impeller structure The direction is deflected in the opposite direction, and the center line of the second guide groove is deflected to the rotation direction of the impeller structure. .
可选地,所述本体的尺寸从所述本体的上部逐渐向所述本体的下部增大,所述本体的表面为曲面。Optionally, the size of the body gradually increases from the upper part of the body to the lower part of the body, and the surface of the body is a curved surface.
可选地,所述后弯叶片在任一个流面上的叶片角从所述进口向所述出口先逐渐减小后逐渐增大,所述叶片角为所述后弯叶片表面弧线的切线与所述叶轮结构的轴面的夹角。Optionally, the blade angle of the backward curved blade on any flow surface gradually decreases and then gradually increases from the inlet to the outlet, and the blade angle is the tangent of the surface arc of the backward curved blade and The included angle of the axial surface of the impeller structure.
可选地,所述进口处的所述叶片角的角度为20-80°,所述出口处的所述叶片角的角度为0-30°。Optionally, the blade angle at the inlet is 20-80°, and the blade angle at the outlet is 0-30°.
可选地,所述第一导向槽的中心线与所述本体中心轴线的径向之间的夹角为15-50°。Optionally, the included angle between the centerline of the first guide groove and the radial direction of the central axis of the body is 15-50°.
可选地,所述第二导向槽的中心线与所述本体中心轴线的径向之间的夹角为35-80°。Optionally, the included angle between the centerline of the second guide groove and the radial direction of the central axis of the body is 35-80°.
本申请还提供了一种混合装置,包括所述的叶轮组件。The present application also provides a mixing device, including the impeller assembly.
本申请相对于现有技术取得了以下技术效果:Compared with the prior art, the present application has achieved the following technical effects:
本申请采用的后弯叶片旋转时能够与流体的流动达到较佳耦合,使得设置在本体上的后弯叶片更高效地对流体做功;特别是,通过仿真计算发现,将后弯叶片在任一个流面上的叶片角设计成从进口到出口先减小后增大可以使得后弯叶片更高效地对流体做功;另一方面通过在第一挡板上开设第一导向槽、第二挡板上开设第二导向槽,通过第一导向槽和第二导向槽的方向来减小流体通过第一挡板和第二挡板时的动能损失。流体在通过第一挡板和第二挡板之间的分散区进行分散后仍然具有足够的动能通过离心的方式进行出料,无需再增加对流体做功的排料叶片,极大减少了对排料区流体的扰动,使得排料区的流体压力能够保持均匀和稳定,流体能够以稳定的流速出料,消除了脉动导致的振动和噪音。The backward curved blade adopted in this application can achieve better coupling with the flow of fluid when it rotates, so that the backward curved blade arranged on the body can perform work on the fluid more efficiently; especially, it is found through simulation calculation that the backward curved blade can The blade angle on the surface is designed to decrease first and then increase from the inlet to the outlet, which can make the backward curved blade work on the fluid more efficiently; on the other hand, by setting the first guide groove on the first baffle and the A second guide groove is provided to reduce kinetic energy loss when the fluid passes through the first baffle plate and the second baffle plate through the direction of the first guide groove and the second guide groove. After the fluid is dispersed through the dispersion area between the first baffle and the second baffle, it still has enough kinetic energy to be discharged by centrifugal means, and there is no need to add discharge blades that work on the fluid, which greatly reduces the impact on the discharge. The turbulence of the fluid in the material area keeps the fluid pressure in the discharge area uniform and stable, and the fluid can be discharged at a stable flow rate, eliminating the vibration and noise caused by pulsation.
附图说明Description of drawings
为了更清楚地说明本申请实施例或现有技术中的技术方案,下面将对实施例中所需要使用的附图作简单地介绍,显而易见地,下面描述中的附图仅仅是本申请的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其他的附图。In order to more clearly illustrate the technical solutions in the embodiments of the present application or the prior art, the following will briefly introduce the accompanying drawings required in the embodiments. Obviously, the accompanying drawings in the following description are only some of the present application. Embodiments, for those of ordinary skill in the art, other drawings can also be obtained based on these drawings without any creative effort.
图1为本申请的叶轮组件示意图;Fig. 1 is the schematic diagram of the impeller assembly of the present application;
图2为图1的A-A剖视图;Fig. 2 is A-A sectional view of Fig. 1;
图3为图2中Ⅰ处局部放大图;Figure 3 is a partial enlarged view of I in Figure 2;
图4为本申请的叶轮结构示意图;Fig. 4 is the structural representation of the impeller of the present application;
图5为本申请的壳体结构示意图;Fig. 5 is a schematic diagram of the shell structure of the present application;
其中:100-叶轮组件,1-叶轮结构,2-壳体结构,3-本体,4-后弯叶片,5-第一挡板,6-第二挡板,7-第一导向槽,8-第二导向槽。Among them: 100-impeller assembly, 1-impeller structure, 2-housing structure, 3-body, 4-backward curved blade, 5-first baffle, 6-second baffle, 7-first guide groove, 8 - Second guide slot.
具体实施方式Detailed ways
下面将结合本申请实施例中的附图,对本申请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申请一部分实施例,而不是全部的实施例。基于本申请中的实施例,本领域普通技术人员在没有付出创造性劳动的前提下所获得的所有其他实施例,都属于本申请保护的范围。The following will clearly and completely describe the technical solutions in the embodiments of the application with reference to the drawings in the embodiments of the application. Apparently, the described embodiments are only some of the embodiments of the application, not all of them. Based on the embodiments in this application, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the scope of protection of this application.
本申请的目的是提供一种叶轮组件及混合装置,以解决上述现有技术存在的问题,解决了固液混合物粘度大时采用离心式出料方式的分散装置容易出现的出料不稳定、振动和噪音大、工作效率不够高的问题。The purpose of this application is to provide an impeller assembly and a mixing device to solve the above-mentioned problems in the prior art, and to solve the problem of unstable discharge, vibration, etc. And noise, work efficiency is not high enough.
为使本申请的上述目的、特征和优点能够更加明显易懂,下面结合附图和具体实施方式对本申请作进一步详细的说明。In order to make the above objects, features and advantages of the present application more obvious and comprehensible, the present application will be further described in detail below in conjunction with the accompanying drawings and specific implementation methods.
实施例一Embodiment one
如图1-图5所示:本实施例提供了一种叶轮组件100,包括相对转动的叶轮结构1和壳体结构2,叶轮结构1包括本体3,本体3的表面沿本体3的周向设置有若干后弯叶片4,本体3的下部设置有至少一层第一挡板5,第一挡板5设置在各后弯叶片4的外侧,壳体结构2包括至少一层第二挡板6,第二挡板6位于第一挡板5的内侧和/或外侧,本实施例中,壳体结构2设置有内外两层的第二挡板6,分别位于第一挡板5的内侧和外侧,所述第二挡板6嵌套、扣合在所述第一挡板5的外围,第一挡板5上沿周向开设有若干第一导向槽7,所述第一导向槽7均匀分布在所述第一挡板5上,内外两层的第二挡板6上分别沿周向开设有若干第二导向槽8,所述第二导向槽8均匀分布在所述第二挡板6上,第一导向槽7和第二导向槽8的截面形状类似于菱形,所述第一导向槽7和所述第二导向槽8的偏向交错设置,该叶轮组件100在叶轮结构1的本体3上端处设置有流体的入 口,在叶轮结构1的本体3下端处设置有流体的出口,流体从本体3上部的进口进入,沿本体3的表面流动,依次通过本体3的下部的出口、内侧的所述第二导向槽8、所述第一导向槽7和外侧的所述第二导向槽8流出,第一导向槽7的中心线向叶轮结构1的转动方向的反方向偏转,第二导向槽8的中心线向叶轮结构1的转动方向偏转。As shown in Figures 1-5: this embodiment provides an impeller assembly 100, including a relatively rotating impeller structure 1 and a housing structure 2, the impeller structure 1 includes a body 3, and the surface of the body 3 is along the circumference of the body 3 Several backward curved blades 4 are provided, at least one layer of first baffles 5 is provided on the lower part of the body 3, and the first baffles 5 are arranged on the outside of each backward curved blade 4, and the shell structure 2 includes at least one layer of second baffles 6. The second baffle 6 is located on the inside and/or outside of the first baffle 5. In this embodiment, the shell structure 2 is provided with two layers of second baffles 6 inside and outside, which are respectively located on the inside of the first baffle 5. and the outer side, the second baffle 6 is nested and fastened on the periphery of the first baffle 5, and the first baffle 5 is provided with a plurality of first guide grooves 7 along the circumferential direction, and the first guide grooves 7 are evenly distributed on the first baffle plate 5, and a number of second guide grooves 8 are opened on the second baffle plate 6 of the inner and outer layers along the circumferential direction, and the second guide grooves 8 are evenly distributed on the second On the baffle plate 6, the cross-sectional shape of the first guide groove 7 and the second guide groove 8 is similar to a rhombus, and the deflections of the first guide groove 7 and the second guide groove 8 are arranged alternately. The upper end of the body 3 of 1 is provided with a fluid inlet, and the lower end of the body 3 of the impeller structure 1 is provided with a fluid outlet. The outlet, the inner second guide groove 8, the first guide groove 7 and the outer second guide groove 8 flow out, and the centerline of the first guide groove 7 deflects to the opposite direction of the impeller structure 1's rotation direction , the center line of the second guide groove 8 deflects to the rotation direction of the impeller structure 1 .
本实施例中,以图2的摆放方向为准,叶轮结构1围绕本体3的轴线沿顺时针方向转动。In this embodiment, the impeller structure 1 rotates clockwise around the axis of the body 3 based on the placement direction in FIG. 2 .
本实施例中,本体3的尺寸从本体3的上部向本体3的下部逐渐增大,本体3呈截锥体,本体3的表面为曲面。本体3从进口到出口的子午流道线为向内弯曲的类圆弧形曲线。In this embodiment, the size of the body 3 gradually increases from the upper part of the body 3 to the lower part of the body 3, the body 3 is in the shape of a truncated cone, and the surface of the body 3 is a curved surface. The meridian channel line of the main body 3 from the inlet to the outlet is an inwardly bent arc-like curve.
本实施例中,后弯叶片4在任一个流面上的叶片角从进口向出口先逐渐减小后逐渐增大,叶片角为后弯叶片4表面弧线的切线与叶轮结构1的轴面的夹角,且取正值。In this embodiment, the blade angle of the curved blade 4 on any flow surface gradually decreases from the inlet to the outlet and then gradually increases, and the blade angle is the tangent of the curved blade 4 surface arc and the axial surface of the impeller structure 1 Angle, and take a positive value.
本实施例中,后弯叶片4与壳体之间的间隙从进口到出口是连续平滑变化的。In this embodiment, the gap between the backward curved blade 4 and the casing changes continuously and smoothly from the inlet to the outlet.
本实施例中,进口处的叶片角的角度为20-80°,出口处的叶片角的角度为0-30°,最小的叶片角的角度为0-30°。叶片角的角度分布与后弯叶片4的气动载荷分布相关,根据后弯叶片4中流体仿真结果,调整叶片角的角度分布使流体流动与后弯叶片4达到较佳耦合,以保证后弯叶片4对流体高效做功。In this embodiment, the blade angle at the inlet is 20-80°, the blade angle at the outlet is 0-30°, and the smallest blade angle is 0-30°. The angular distribution of the blade angle is related to the aerodynamic load distribution of the backward-curved blade 4. According to the fluid simulation results in the backward-curved blade 4, the angular distribution of the blade angle is adjusted to achieve a better coupling between the fluid flow and the backward-curved blade 4, so as to ensure that the backward-curved blade 4 work efficiently on the fluid.
本实施例中,第一导向槽7的中心线与本体3的中心轴线的径向之间的夹角(即β 2)为15-50°。第二导向槽8的中心线与本体3的中心轴线的径向之间的夹角(即β 1和β 3)为35-80°。具体参见图3,β 1为内侧的第二导向槽8的中心线L1与径向线R1之间的角度,β 2为第一导向槽7的中心线L2与径向线R2之间的角度,β 3为外侧的第二导向槽8的中心线L3与径向线R3之间的角。径向线R1、径向线R2和径向线R3均是从本体3的中心轴线出发的沿半径方向的线。内层的第二挡板6的第二导向槽8的中心线L1与径向线R1的交点位于内层的第二挡板6的内壁所在的圆周上,第一导向槽7的中心线L2与径向线R2的交点位于第一挡板5的内壁所在 的圆周上,外层的第二挡板6的第二导向槽8的中心线L3与径向线R3的交点位于外层的第二挡板6的内壁所在的圆周上。 In this embodiment, the included angle (ie β 2 ) between the centerline of the first guide groove 7 and the radial direction of the central axis of the body 3 is 15-50°. The included angle (ie β 1 and β 3 ) between the center line of the second guide groove 8 and the radial direction of the center axis of the body 3 is 35-80°. Specifically referring to Fig. 3, β 1 is the angle between the center line L1 and the radial line R1 of the second guide groove 8 inside, and β 2 is the angle between the center line L2 and the radial line R2 of the first guide groove 7 , β3 is the angle between the centerline L3 of the second outer guide groove 8 and the radial line R3. The radial line R1 , the radial line R2 and the radial line R3 are all radial lines starting from the central axis of the body 3 . The intersection point of the centerline L1 of the second guide groove 8 of the second baffle plate 6 of the inner layer and the radial line R1 is located on the circumference where the inner wall of the second baffle plate 6 of the inner layer is located, and the centerline L2 of the first guide groove 7 The intersection point with the radial line R2 is located on the circumference where the inner wall of the first baffle plate 5 is located, and the intersection point with the center line L3 of the second guide groove 8 of the second baffle plate 6 of the outer layer and the radial line R3 is located at the second outer layer. On the circumference where the inner wall of the second baffle plate 6 is located.
叶轮组件100的转动方向如图3中箭头所示,本实施例一方面通过调整叶片角来控制后弯叶片4的流体载荷分布,叶片角分布使后弯叶片4旋转与流体的流动达到较佳耦合,使得设置在本体3上的后弯叶片4更高效地对流体做功;另一方面通过在第一挡板5上开设第一导向槽7、第二挡板6上开设第二导向槽8,通过第一导向槽7和第二导向槽8的方向来减小流体通过第一挡板5和第二挡板6时的动能损失。具体地,固定在壳体结构2上的第二挡板6是静止的,第二导向槽8的中心线向叶轮结构1的转动方向偏转,这可以使得流体不用大幅度改变方向就能够顺利地通过第二导向槽8。固定在叶轮结构1上的第一挡板5随叶轮结构1一起转动,这可将除第一导向槽7之外的剩余部分看作是后弯叶片4的延伸,第一导向槽7也做成后弯的结构,这更有利于对流体做功。The direction of rotation of the impeller assembly 100 is shown by the arrow in Figure 3. On the one hand, this embodiment controls the fluid load distribution of the backward curved blade 4 by adjusting the blade angle. The distribution of the blade angle makes the rotation of the backward curved blade 4 and the flow of the fluid better Coupling, so that the backward curved blade 4 set on the body 3 can work on the fluid more efficiently; on the other hand, by opening the first guide groove 7 on the first baffle 5 and the second guide groove 8 on the second baffle , the kinetic energy loss when the fluid passes through the first baffle plate 5 and the second baffle plate 6 is reduced by the direction of the first guide groove 7 and the second guide groove 8 . Specifically, the second baffle plate 6 fixed on the housing structure 2 is stationary, and the center line of the second guide groove 8 deflects to the rotation direction of the impeller structure 1, which can make the fluid flow smoothly without changing the direction greatly. through the second guide groove 8. The first baffle plate 5 fixed on the impeller structure 1 rotates together with the impeller structure 1, which can be regarded as the extension of the backward curved blade 4 except the first guide groove 7, and the first guide groove 7 also serves as Into a backbent structure, which is more conducive to doing work on the fluid.
流体在通过第一挡板5和第二挡板6之间的分散区进行分散后仍然具有足够的动能通过离心的方式进行出料,无需在最外层的第二挡板6的外侧再增加对流体做功的排料叶片,这极大减少了对排料区流体的扰动,使得排料区的流体压力能够保持均匀和稳定,流体能够以稳定的流速出料,消除了脉动导致的振动和噪音。After the fluid is dispersed through the dispersion area between the first baffle plate 5 and the second baffle plate 6, it still has enough kinetic energy to be discharged by centrifugation, and there is no need to add more The discharge vane that works on the fluid greatly reduces the disturbance of the fluid in the discharge area, so that the fluid pressure in the discharge area can be kept uniform and stable, and the fluid can be discharged at a stable flow rate, eliminating the vibration and vibration caused by pulsation noise.
实施例二Embodiment two
本实施例提供了一种包括实施例一的叶轮组件100的混合装置。This embodiment provides a mixing device including the impeller assembly 100 of the first embodiment.
本说明书中应用了具体实施例对本申请的原理及实施方式进行了阐述,以上实施例的说明只是用于帮助理解本申请的方法及其核心思想;同时,对于本领域的一般技术人员,依据本申请的思想,在具体实施方式及应用范围上均会有改变之处。综上所述,本说明书内容不应理解为对本申请的限制。In this description, the application of specific examples to illustrate the principle and implementation of the application, the description of the above examples is only used to help understand the method of the application and its core idea; meanwhile, for those of ordinary skill in the art, according to this The idea of the application will have changes in the specific implementation method and application range. To sum up, the contents of this specification should not be understood as limiting the application.

Claims (7)

  1. 一种叶轮组件,其特征在于:包括相对转动的叶轮结构和壳体结构,所述叶轮结构包括本体,所述本体的表面沿所述本体的周向设置有若干后弯叶片,所述本体的下部设置有至少一层第一挡板,所述第一挡板设置在各所述后弯叶片的外侧,所述壳体结构包括至少一层第二挡板,所述第二挡板位于所述第一挡板的内侧和/或外侧,所述第一挡板上开设有若干第一导向槽,所述第二挡板上开设有若干第二导向槽,流体从所述本体上部的进口进入,沿所述本体的表面流动,通过所述本体的下部的出口、所述第一导向槽和所述第二导向槽流出,所述第一导向槽的中心线向所述叶轮结构的转动方向的反方向偏转,所述第二导向槽的中心线向所述叶轮结构的转动方向偏转。An impeller assembly, characterized in that it includes a relatively rotating impeller structure and a housing structure, the impeller structure includes a body, the surface of the body is provided with several backward curved blades along the circumference of the body, the body The lower part is provided with at least one layer of first baffles, and the first baffles are arranged on the outer sides of each of the backward curved blades, and the shell structure includes at least one layer of second baffles, and the second baffles are located on the The inner side and/or the outer side of the first baffle, the first baffle is provided with a number of first guide grooves, the second baffle is provided with a number of second guide grooves, the fluid flows from the inlet of the upper part of the body Enter, flow along the surface of the body, and flow out through the outlet of the lower part of the body, the first guide groove and the second guide groove, and the centerline of the first guide groove rotates to the impeller structure The direction is deflected in the opposite direction, and the center line of the second guide groove is deflected to the rotation direction of the impeller structure.
  2. 根据权利要求1所述的叶轮组件,其特征在于:所述本体的尺寸从所述本体的上部向所述本体的下部逐渐增大,所述本体的表面为曲面。The impeller assembly according to claim 1, wherein the size of the body gradually increases from the upper part of the body to the lower part of the body, and the surface of the body is a curved surface.
  3. 根据权利要求1所述的叶轮组件,其特征在于:所述后弯叶片在任一个流面上的叶片角从所述进口向所述出口先逐渐减小后逐渐增大,所述叶片角为所述后弯叶片表面弧线的切线与所述叶轮结构的轴面的夹角。The impeller assembly according to claim 1, characterized in that: the blade angle of the backward curved blade on any flow surface gradually decreases and then gradually increases from the inlet to the outlet, and the blade angle is the Describe the included angle between the tangent to the curved blade surface arc and the axial surface of the impeller structure.
  4. 根据权利要求3所述的叶轮组件,其特征在于:所述进口处的所述叶片角的角度为20-80°,所述出口处的所述叶片角的角度为0-30°。The impeller assembly according to claim 3, wherein the blade angle at the inlet is 20-80°, and the blade angle at the outlet is 0-30°.
  5. 根据权利要求1所述的叶轮组件,其特征在于:所述第一导向槽的中心线与所述本体中心轴线的径向之间的夹角为15-50°。The impeller assembly according to claim 1, characterized in that: the included angle between the centerline of the first guide groove and the radial direction of the central axis of the body is 15-50°.
  6. 根据权利要求1所述的叶轮组件,其特征在于:所述第二导向槽的中心线与所述本体中心轴线的径向之间的夹角为35-80°。The impeller assembly according to claim 1, wherein the included angle between the centerline of the second guide groove and the radial direction of the central axis of the body is 35-80°.
  7. 一种混合装置,其特征在于:包括如权利要求1-6任一项所述的叶轮组件。A mixing device, characterized by comprising the impeller assembly according to any one of claims 1-6.
PCT/CN2022/123953 2021-10-13 2022-10-09 Impeller assembly and mixing apparatus WO2023061271A1 (en)

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KR1020237035221A KR20230155578A (en) 2021-10-13 2022-10-09 Impeller assembly and mixing device
EP22880210.4A EP4292698A1 (en) 2021-10-13 2022-10-09 Impeller assembly and mixing apparatus
JP2023558648A JP2024511147A (en) 2021-10-13 2022-10-09 Impeller assembly and mixing equipment

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Publication number Priority date Publication date Assignee Title
RU2033252C1 (en) * 1992-05-06 1995-04-20 Геннадий Александрович Сайпеев Rotor hydraulic-shock-operated apparatus
RU2158629C1 (en) * 1999-04-27 2000-11-10 Закрытое акционерное общество "Катализаторная компания" Rotary dispersing apparatus
CN1386983A (en) * 2002-06-06 2002-12-25 孙敏超 Efficient propeller with blades curled backward for centrifugal propeller machinery
RU2208472C1 (en) * 2002-05-13 2003-07-20 Саушкин Сергей Александрович Rotary dispersing apparatus (versions)
CN113828187A (en) * 2021-10-13 2021-12-24 深圳市尚水智能设备有限公司 Impeller assembly and mixing device

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2033252C1 (en) * 1992-05-06 1995-04-20 Геннадий Александрович Сайпеев Rotor hydraulic-shock-operated apparatus
RU2158629C1 (en) * 1999-04-27 2000-11-10 Закрытое акционерное общество "Катализаторная компания" Rotary dispersing apparatus
RU2208472C1 (en) * 2002-05-13 2003-07-20 Саушкин Сергей Александрович Rotary dispersing apparatus (versions)
CN1386983A (en) * 2002-06-06 2002-12-25 孙敏超 Efficient propeller with blades curled backward for centrifugal propeller machinery
CN113828187A (en) * 2021-10-13 2021-12-24 深圳市尚水智能设备有限公司 Impeller assembly and mixing device

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