WO2024060878A1 - Fan, and communication device - Google Patents

Fan, and communication device Download PDF

Info

Publication number
WO2024060878A1
WO2024060878A1 PCT/CN2023/112952 CN2023112952W WO2024060878A1 WO 2024060878 A1 WO2024060878 A1 WO 2024060878A1 CN 2023112952 W CN2023112952 W CN 2023112952W WO 2024060878 A1 WO2024060878 A1 WO 2024060878A1
Authority
WO
WIPO (PCT)
Prior art keywords
fan
airflow
guide part
fan blade
side edge
Prior art date
Application number
PCT/CN2023/112952
Other languages
French (fr)
Chinese (zh)
Inventor
智博文
Original Assignee
中兴通讯股份有限公司
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 中兴通讯股份有限公司 filed Critical 中兴通讯股份有限公司
Publication of WO2024060878A1 publication Critical patent/WO2024060878A1/en

Links

Classifications

    • 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
    • F04D29/52Casings; Connections of working fluid for axial pumps
    • F04D29/54Fluid-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
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K7/00Constructional details common to different types of electric apparatus
    • H05K7/20Modifications to facilitate cooling, ventilating, or heating
    • 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
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction

Definitions

  • the present disclosure relates to the field of communication heat dissipation technology, and in particular to a fan and communication equipment.
  • the main purpose of the embodiments of the present disclosure is to provide a fan and communication equipment, aiming to solve the problem of high cooling fan noise in existing communication equipment.
  • a fan comprising:
  • a fan mechanism the fan mechanism includes fan blades
  • the housing is provided with an accommodation cavity, an airflow inlet, an airflow outlet and a plurality of guide grooves.
  • the airflow inlet and the airflow outlet are respectively connected with the accommodation cavity; all the guide grooves are provided with At one end of the air flow inlet, and each of the guide grooves extends from the air flow inlet along the inner wall of the accommodation cavity in the direction of the air flow outlet, and one of the two adjacent guide grooves extends There is a gap between them; the fan mechanism is accommodated in the accommodation cavity.
  • embodiments of the present disclosure also provide a communication device, and the technical solution adopted is as follows:
  • a communications device including:
  • Figure 1 is a schematic three-dimensional structural diagram of a fan provided by an embodiment of the present disclosure
  • Figure 2 is a schematic exploded structural diagram of a fan provided by an embodiment of the present disclosure
  • Figure 3 is a schematic cross-sectional view of a fan provided by an embodiment of the present disclosure.
  • Figure 4 is a schematic three-dimensional structural diagram of a housing provided by an embodiment of the present disclosure from one perspective;
  • Figure 5 is a partial enlarged schematic diagram of M in Figure 4.
  • Figure 6 is a schematic three-dimensional structural diagram of the housing provided by an embodiment of the present disclosure from another perspective;
  • Figure 7 is a schematic three-dimensional structural diagram of the fan mechanism provided by an embodiment of the present disclosure from one perspective;
  • Figure 8 is a schematic three-dimensional structural diagram of the fan mechanism provided by an embodiment of the present disclosure from another perspective;
  • Figure 9 is a simplified structural schematic diagram of a communication device provided by an embodiment of the present disclosure.
  • the fan 10 provided in this embodiment includes a fan mechanism 11 and a casing 12; wherein, the fan mechanism 11 includes fan blades 111; the casing 12 is provided with an accommodation cavity 120, an airflow inlet 1201, The airflow outlet 1202 and multiple guide grooves 1203, the airflow inlet 1201 and the airflow outlet 1202 are respectively connected with the accommodation cavity 120; all the guide grooves 1203 are located at one end of the airflow inlet 1201, and each guide groove 1203 is connected to the airflow inlet 1201.
  • the inlet 1201 extends along the inner wall of the accommodating cavity 120 in the direction of the air outlet 1202, and there is a gap between two adjacent guide grooves 1203; the fan mechanism 11 is accommodated in the accommodating cavity 120.
  • the fan 10 provided in this embodiment is provided with a guide groove 1203 at one end of the air inlet 1201, so it can guide the airflow entering the fan 10, and when the airflow passes through the guide groove 1203, air flow disturbance will occur.
  • the airflow close to the guide groove 1203 forms a turbulent boundary layer, while the airflow farther away from the guide groove 1203 forms a laminar flow layer, which can effectively reduce the resistance encountered by the airflow when entering the fan 10, thereby making it more efficient.
  • the fan provided in the embodiment of the present disclosure includes a housing and a fan mechanism, wherein the housing is provided with a The fan mechanism is accommodated in the accommodating cavity, and the airflow inlet and the airflow outlet are provided with a plurality of guide grooves at one end of the airflow inlet, and the guide grooves all extend from the airflow inlet along the inner wall of the accommodating cavity toward the direction where the airflow outlet is located.
  • the fan mechanism is accommodated in the accommodating cavity, and the airflow entering the accommodating cavity can be guided by providing a plurality of guide grooves, so that the airflow close to the side of the guide groove becomes a turbulent layer, so that the airflow has a turbulent layer and a laminar layer, which is conducive to reducing the resistance of the airflow flowing in the fan, increasing the airflow velocity, so that more airflow enters the fan at a more uniform velocity, and effectively reducing the noise of the airflow during the rotation of the fan.
  • the fan is installed in the communication equipment, and the communication equipment has less noise when working, which is conducive to reducing the noise impact of the communication equipment working.
  • the housing 12 includes a housing body 121 and an annular boss 122.
  • the annular boss 122 is connected to the inner wall surface of the housing body 121 to form an airflow inlet 1201.
  • an airflow inlet 1201 is formed by an annular boss 122
  • the guide groove 1203 is located on the annular boss 122 facing away from the main body 121 of the shell
  • the fan mechanism 11 is located between the annular boss 122 of the accommodation cavity 120 and the airflow outlet 1202. , that is, the fan mechanism 11 is disposed in the accommodating cavity 120 , and is disposed at a portion of the accommodating cavity 120 between the annular boss 122 and the airflow outlet 1202 .
  • the housing 12 has a first end surface 1211 and a second end surface 1212.
  • the first end surface 1211 and the second end surface 1212 are arranged oppositely, wherein the airflow inlet 1201 is provided on the first end face 1211, and the air flow outlet 1202 is provided on the second end face 1212, so that the air flow can enter the accommodation cavity 120 from the outside of the fan 10 through the air flow inlet 1201, and then flow out from the air flow outlet 1202 driven by the rotation of the fan blade 111.
  • each guide groove 1203 includes a first guide part 12031 and a second guide part 12032.
  • the first guide part 12031 extends in an arc-shaped trajectory and is connected to the second guide part 12032.
  • the air guide portion 12032 is provided on the inner wall surface of the accommodation cavity 120 and the extension trajectory of the second air guide portion 12032 is parallel to the rotation center axis of the fan blade 111 .
  • the first guide part 12031 serves as the front groove structure where external airflow enters the fan 10. It is designed to extend in an arc-shaped trajectory, so that the airflow has a certain direction of rotation before entering the fan 10, which improves the airflow inlet 1201 of the fan 10.
  • the air flow direction is beneficial to making the noise generated by the airflow entering the fan 10 smaller, which is beneficial to improving the sound quality of the fan 10 .
  • the portion where the first end surface 1211 and the inner wall surface of the accommodation cavity 120 are connected to each other forms a chamfered slope
  • the first guide portion 12031 extends from the first end surface 1211 to the chamfered slope and connects with the second guide portion 12032 connection, so that when the airflow on the first end surface 1211 enters the airflow inlet 1201, the airflow layer close to the housing 12 is introduced into the airflow inlet 1201 by the first guide part 12031, so that the airflow layer close to the first guide part 12031 becomes into a turbulent layer.
  • the central axis of rotation of the fan blade 111 and the central axis of each second guide portion 12032 form a plane, and the first guide portion 12031 connected to the second guide portion 12032 is at a distance from the plane.
  • the gradually decreasing trend extends to the second air guide part 12032 and is connected with the second air guide part 12032, and the end connecting the first air guide part 12031 and the second air guide part 12032 is located at the front end of the rotation of the fan blade 111.
  • One end of the air guide portion 12031 away from the second air guide portion 12032 is located at the end of the rotation of the fan blade 111 .
  • the rotating front end of the fan blade 111 and the rotating end of the fan blade 111 respectively refer to the end of the fan blade 111 that faces the front of the rotation during the rotation of the fan blade 111.
  • the end facing away from the front of the rotation is called the end.
  • the width of each guide groove 1203 is between 1.0mm and 5mm, and the depth is between 0.2mm and 1.0mm.
  • the width of the guide groove 1203 and The depth is limited in size, which is conducive to the formation of a turbulent layer.
  • the distance between two adjacent guide grooves 1203 is between 1.0 mm and 10.0 mm, which is beneficial to the airflow entering the fan 10 forming a turbulent layer and stratosphere, and reducing airflow noise.
  • the maximum distance (D) from the fan blade 111 to the rotation center axis of the fan blade 111 and the minimum distance (d) from the groove bottom wall of the guide groove 1203 to the rotation center axis of the fan blade 111. ) is between 0 and 10mm, so that after the airflow entering through the airflow inlet 1201 forms a turbulent layer, the airflow in the turbulent layer completely flows to the fan blade 111 and passes through the airflow under the negative pressure generated by the rotation of the fan blade 111 Exit 1202 flows out.
  • the fan blade 111 has a first fan surface 1111 and a second fan surface 1112.
  • the first fan surface 1111 faces the airflow inlet 1201, and the second fan surface 1112 faces away from the airflow inlet 1201. (That is, toward the airflow outlet 1202), the fan blade 111 is provided with a plurality of recesses 1110.
  • the recesses 1110 are recessed from the first fan surface 1111 to the second fan surface 1112 or from the second fan surface 1112 to the first fan surface 1111.
  • the recesses 1110 are The design can destroy the laminar flow boundary layer flowing to the fan blade 111, causing the airflow to form a turbulent boundary layer in advance during the transition process, so as to effectively reduce the shape resistance of the fan blade 111 during the rotation process, so that the fan 10 can inhale more air , not only improves the operating efficiency of the fan 10, but also reduces the operating noise.
  • the first sector surface 1111 and the second sector surface 1112 are both distributed with pits 1110 .
  • the fan blade 111 has a first side edge, which is the front end of the fan blade 111 when rotating, and the pit 1110 is disposed close to the first side edge.
  • the fan blade 111 also has a second side edge.
  • the second side edge is the end of the fan blade 111 when it rotates. That is, the first side edge and the second side edge are two opposite edges.
  • the first sector 1111 When the pit 1110 When set on the first sector 1111, the first sector 1111 has a first area 11110, and the first area 11110 extends from the first side edge to the second side edge and has a distance from the second side edge.
  • the first area 11110 occupies the first 30% to 40% of the area of the sector 1111, the pits 1110 are provided in the first area 11110.
  • a plurality of pits 1110 are arranged in at least one row and multiple columns, two adjacent ones There is a spacing between the pits 1110, which can effectively reduce the resistance of the air flow and improve the operating efficiency of the fan 10.
  • multiple pits 1110 can also be arranged in multiple rows and columns, and all the pits 1110 are arranged in the first area 11110. , which can ensure the structural strength and structural reliability of the fan blade 111.
  • the second sector 1112 also has a first area 11110, and the first area 11110 of the second sector 1112 is the same as the first area 11110 of the first sector 1111, and the first area 11110 of the second sector 1112 also has A plurality of pits 1110 are provided.
  • the structure of the pit 1110 is in the shape of a hemisphere, a cube, or a pyramid. When the pit 1110 is longitudinally sectioned, the cross-sectional surface is in an arc shape, a square shape, or a conical shape.
  • the fan 10 further includes a fixing member 13 .
  • the fixing member 13 is provided on the second end surface 1212 and is connected to the housing body 121 for packaging the fan mechanism 11 in the accommodating cavity 120 .
  • the fixing member 13 is provided with an exhaust port (not labeled in the figure) connected to the air flow outlet 1202 so that the air flow in the accommodation cavity 120 can be discharged.
  • the fixing member 13 includes an airflow grate 131 , and the airflow grate 131 is installed at the exhaust port, so that the airflow from the airflow outlet 1202 can be discharged out of the fan 10 through the airflow grate 131 .
  • an embodiment of the present disclosure also provides a communication device 20.
  • the communication device 20 includes the fan 10 of any of the above embodiments.
  • the fan 10 serves as a heat sink for the communication device 20. components, which can effectively reduce the noise of the communication device 20 during the heat dissipation process.
  • the communication device 20 includes a device body 21 , and the fan 10 is installed in the device body 21 to dissipate heat from components of the device body 21 that need to dissipate heat.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The embodiments of the present disclosure relate to the technical field of communication heat dissipation. Provided are a fan and a communication device. The fan comprises a fan mechanism and a housing, wherein the fan mechanism comprises fan blades; the housing is provided with an accommodation cavity, an airflow inlet, an airflow outlet and a plurality of flow guide slots, the airflow inlet and the airflow outlet being respectively in communication with the accommodation cavity; all the flow guide slots are formed at one end of the airflow inlet, each flow guide slot extends from the airflow inlet toward the airflow outlet along an inner wall surface of the accommodation cavity, and there is a gap between the two adjacent flow guide slots; and the fan mechanism is accommodated in the accommodation cavity.

Description

风机和通信设备Wind turbines and communication equipment
相关申请的交叉引用Cross-references to related applications
本公开基于2022年9月22日提交的发明创造名称为“风机和通信设备”的中国专利申请202222518495.X,并且要求该专利申请的优先权,通过引用将其所公开的内容全部并入本公开。This disclosure is based on Chinese patent application 202222518495.X, filed on September 22, 2022, with the invention name “Wind turbine and communication equipment”, and claims the priority of the patent application, and all the contents disclosed therein are incorporated into this disclosure by reference.
技术领域Technical field
本公开涉及通信散热技术领域,尤其涉及一种风机和通信设备。The present disclosure relates to the field of communication heat dissipation technology, and in particular to a fan and communication equipment.
背景技术Background technique
随着集成电路技术的不断发展,通信设备的体积变得越来越小,通信设备中的系统也愈加复杂,部件的密集导致通信设备具有高热密度,为了使得通信设备能够有效工作,需要对其进行有效的散热,因此需要在通信设备中加装多个风机,以实现有效散热,但是,现有通信设备的多个散热风机同时工作时,由于气流直接进入散热风机中并直接作用在扇叶上导致噪声较大。With the continuous development of integrated circuit technology, the size of communication equipment is becoming smaller and smaller, and the systems in communication equipment are becoming more and more complex. The density of components causes communication equipment to have high thermal density. In order for communication equipment to work effectively, it needs to be For effective heat dissipation, multiple fans need to be installed in the communication equipment to achieve effective heat dissipation. However, when multiple cooling fans of existing communication equipment work at the same time, the airflow directly enters the cooling fan and directly acts on the fan blades. leading to greater noise.
公开内容public content
本公开实施例的主要目的在于提供一种风机和通信设备,旨在解决现有通信设备散热风机噪声较大的问题。The main purpose of the embodiments of the present disclosure is to provide a fan and communication equipment, aiming to solve the problem of high cooling fan noise in existing communication equipment.
一种风机,包括:A fan, comprising:
风扇机构,所述风扇机构包括扇叶;A fan mechanism, the fan mechanism includes fan blades;
壳体,所述壳体设有容纳腔、气流进口、气流出口以及多个导流槽,所述气流进口和所述气流出口分别与所述容纳腔连通;所有的所述导流槽均设于所述气流进口的一端,且每个所述导流槽均自所述气流进口沿所述容纳腔的内壁面向所述气流出口所在的方向延伸,相邻的两个所述导流槽之间具有间隔;所述风扇机构收容于所述容纳腔中。The housing is provided with an accommodation cavity, an airflow inlet, an airflow outlet and a plurality of guide grooves. The airflow inlet and the airflow outlet are respectively connected with the accommodation cavity; all the guide grooves are provided with At one end of the air flow inlet, and each of the guide grooves extends from the air flow inlet along the inner wall of the accommodation cavity in the direction of the air flow outlet, and one of the two adjacent guide grooves extends There is a gap between them; the fan mechanism is accommodated in the accommodation cavity.
基于上述的风机,本公开实施例还提供一种通信设备,其所采用的技术方案如下:Based on the above-mentioned wind turbine, embodiments of the present disclosure also provide a communication device, and the technical solution adopted is as follows:
一种通信设备,包括:A communications device including:
上述任一项所述的风机。The fan described in any of the above.
附图说明Description of the drawings
为了更清楚地说明本申请实施例技术方案,下面将对实施例描述中所需要使用的附图作简单地介绍,显而易见地,下面描述中的附图是本申请的一些实施例,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 of the embodiments of the present application, the drawings required for use in the description of the embodiments will be briefly introduced below. Obviously, the drawings described below are some embodiments of the present application. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying any creative work.
图1为本公开实施例提供的风机的立体结构示意图;Figure 1 is a schematic three-dimensional structural diagram of a fan provided by an embodiment of the present disclosure;
图2为本公开实施例提供的风机的爆炸结构示意图;Figure 2 is a schematic exploded structural diagram of a fan provided by an embodiment of the present disclosure;
图3为本公开实施例提供的风机的剖视示意图;Figure 3 is a schematic cross-sectional view of a fan provided by an embodiment of the present disclosure;
图4为本公开实施例提供的壳体的一个视角的立体结构示意图;Figure 4 is a schematic three-dimensional structural diagram of a housing provided by an embodiment of the present disclosure from one perspective;
图5为图4中M处的局部放大示意图; Figure 5 is a partial enlarged schematic diagram of M in Figure 4;
图6为本公开实施例提供的壳体的另一视角的立体结构示意图;Figure 6 is a schematic three-dimensional structural diagram of the housing provided by an embodiment of the present disclosure from another perspective;
图7为本公开实施例提供的风扇机构的一个视角的立体结构示意图;Figure 7 is a schematic three-dimensional structural diagram of the fan mechanism provided by an embodiment of the present disclosure from one perspective;
图8为本公开实施例提供的风扇机构的另一个视角的立体结构示意图;Figure 8 is a schematic three-dimensional structural diagram of the fan mechanism provided by an embodiment of the present disclosure from another perspective;
图9为本公开实施例提供的通信设备的简化结构示意图。Figure 9 is a simplified structural schematic diagram of a communication device provided by an embodiment of the present disclosure.
附图标号说明:
10、风机;
11、风扇机构;111、扇叶;1110、凹坑;1111、第一扇面;11110、第一区域;1112、第
二扇面;11101、第一侧边缘;11102、第二侧边缘;
12、壳体;120、容纳腔;1201、气流进口;1202、气流出口;1203、导流槽;12031、
第一导流部;12032、第二导流部;121、壳主体;1211、第一端面;1212、第二端面;122、环形凸台;
13、固定件;131、气流篦子;
20、通信设备;21、设备主体。
Explanation of reference numbers:
10. Fan;
11. Fan mechanism; 111. Fan blades; 1110. Dimples; 1111. First fan surface; 11110. First area; 1112. Second fan surface; 11101. First side edge; 11102. Second side edge;
12. Shell; 120. Accommodation cavity; 1201. Air flow inlet; 1202. Air flow outlet; 1203. Diversion groove; 12031.
First guide part; 12032, second guide part; 121, shell main body; 1211, first end face; 1212, second end face; 122, annular boss;
13. Fixings; 131. Air flow grate;
20. Communication equipment; 21. Equipment body.
具体实施方式Detailed ways
下面将结合本公开实施例中的附图,对本公开实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例是本公开一部分实施例,而不是全部的实施例。基于本公开中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本公开保护的范围。The technical solutions in the embodiments of the present disclosure will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present disclosure. Obviously, the described embodiments are part of the embodiments of the present disclosure, rather than all of the embodiments. Based on the embodiments in this disclosure, all other embodiments obtained by those of ordinary skill in the art without creative efforts fall within the scope of protection of this disclosure.
附图中所示的流程图仅是示例说明,不是必须包括所有的内容和操作/步骤,也不是必须按所描述的顺序执行。例如,有的操作/步骤还可以分解、组合或部分合并,因此实际执行的顺序有可能根据实际情况改变。The flowcharts shown in the accompanying drawings are only examples and do not necessarily include all the contents and operations/steps, nor must they be executed in the order described. For example, some operations/steps may also be decomposed, combined or partially merged, so the actual execution order may change according to actual conditions.
应当理解,在此本公开说明书中所使用的术语仅仅是出于描述特定实施例的目的而并不意在限制本公开。如在本公开说明书和所附权利要求书中所使用的那样,除非上下文清楚地指明其它情况,否则单数形式的“一”、“一个”及“该”意在包括复数形式。It should be understood that the terms used in this disclosure are only for the purpose of describing specific embodiments and are not intended to limit the disclosure. As used in this disclosure and the appended claims, unless the context clearly indicates otherwise, the singular forms "a", "an" and "the" are intended to include plural forms.
本公开实施例提供的风机10及其零部件如图1至图8所示。The fan 10 and its components provided by the embodiment of the present disclosure are shown in Figures 1 to 8.
请参阅图1、图2以及图3,本实施例提供的风机10包括风扇机构11和壳体12;其中,风扇机构11包括扇叶111;壳体12设有容纳腔120、气流进口1201、气流出口1202以及多个导流槽1203,气流进口1201和气流出口1202分别与容纳腔120连通;所有的导流槽1203均设于气流进口1201的一端,且每个导流槽1203均自气流进口1201沿容纳腔120的内壁面向气流出口1202所在的方向延伸,相邻的两个导流槽1203之间具有间隔;风扇机构11收容于容纳腔120中。本实施例提供的风机10,由于在气流进口1201的一端设有导流槽1203,因此可以对进入风机10的气流起到导流作用,而气流在通过导流槽1203时,会出现气流扰动而使得靠近导流槽1203一侧的气流形成湍流边界层,而距离导流槽1203较远的气流则形成层流层,因而能够有效降低气流进入风机10过程中所受到的阻力,从而更有利于更多的气流进入风机10,并且在气流进入风机10过程中,还能有效减小气流流速不均形成的流速梯度,使得气流以更加均匀的流速通过壳体12进入风机10,有效地降低了气流在风机10转动过程中的噪声。Please refer to Figure 1, Figure 2 and Figure 3. The fan 10 provided in this embodiment includes a fan mechanism 11 and a casing 12; wherein, the fan mechanism 11 includes fan blades 111; the casing 12 is provided with an accommodation cavity 120, an airflow inlet 1201, The airflow outlet 1202 and multiple guide grooves 1203, the airflow inlet 1201 and the airflow outlet 1202 are respectively connected with the accommodation cavity 120; all the guide grooves 1203 are located at one end of the airflow inlet 1201, and each guide groove 1203 is connected to the airflow inlet 1201. The inlet 1201 extends along the inner wall of the accommodating cavity 120 in the direction of the air outlet 1202, and there is a gap between two adjacent guide grooves 1203; the fan mechanism 11 is accommodated in the accommodating cavity 120. The fan 10 provided in this embodiment is provided with a guide groove 1203 at one end of the air inlet 1201, so it can guide the airflow entering the fan 10, and when the airflow passes through the guide groove 1203, air flow disturbance will occur. The airflow close to the guide groove 1203 forms a turbulent boundary layer, while the airflow farther away from the guide groove 1203 forms a laminar flow layer, which can effectively reduce the resistance encountered by the airflow when entering the fan 10, thereby making it more efficient. It is beneficial for more airflow to enter the fan 10, and during the process of the airflow entering the fan 10, it can also effectively reduce the flow velocity gradient caused by uneven airflow speed, so that the airflow enters the fan 10 through the casing 12 at a more uniform flow speed, effectively reducing the The noise caused by the airflow during the rotation of the fan 10 is eliminated.
相对于一般技术而言,本公开实施例提供的风机,包括壳体和风扇机构,壳体设有容纳 腔、气流进口和气流出口,并且在气流进口的一端设有多个导流槽,并且导流槽均自气流进口沿容纳腔的内壁面向气流出口所在的方向延伸,风扇机构收容于容纳腔中,通过设置多个导流槽,可以对进入容纳腔的气流进行导流,使得靠近导流槽一侧的气流变成湍流层,从而气流具有湍流层和层流层,有利于降低气流在风机中流动的阻力,增大气流流速,从而使得更多的气流以较为均匀的流速进入风机,有效地降低气流在风机转动过程中的噪声。将风机安装在通信设备中,通信设备工作时,具有较小的噪声,从而有利于减小通信设备工作的噪声影响。Compared with the general technology, the fan provided in the embodiment of the present disclosure includes a housing and a fan mechanism, wherein the housing is provided with a The fan mechanism is accommodated in the accommodating cavity, and the airflow inlet and the airflow outlet are provided with a plurality of guide grooves at one end of the airflow inlet, and the guide grooves all extend from the airflow inlet along the inner wall of the accommodating cavity toward the direction where the airflow outlet is located. The fan mechanism is accommodated in the accommodating cavity, and the airflow entering the accommodating cavity can be guided by providing a plurality of guide grooves, so that the airflow close to the side of the guide groove becomes a turbulent layer, so that the airflow has a turbulent layer and a laminar layer, which is conducive to reducing the resistance of the airflow flowing in the fan, increasing the airflow velocity, so that more airflow enters the fan at a more uniform velocity, and effectively reducing the noise of the airflow during the rotation of the fan. The fan is installed in the communication equipment, and the communication equipment has less noise when working, which is conducive to reducing the noise impact of the communication equipment working.
请参阅图3、图4、图5以及图6,在一些实施方式中,壳体12包括壳主体121和环形凸台122,环形凸台122与壳主体121的内壁面连接以形成气流进口1201,由环形凸台122围合形成气流进口1201,导流槽1203背对壳主体121设于环形凸台122,风扇机构11设于容纳腔120之环形凸台122至气流出口1202之间的部位,即风扇机构11设置在容纳腔120中,并且设置在容纳腔120位于环形凸台122至气流出口1202之间的部位。这样的结构设计,风扇机构11旋转时,在容纳腔120中形成负压,以使得气流经由环形凸台122围合形成的气流进口1201进入容纳腔120,并经由气流出口1202排出。Please refer to Figures 3, 4, 5 and 6. In some embodiments, the housing 12 includes a housing body 121 and an annular boss 122. The annular boss 122 is connected to the inner wall surface of the housing body 121 to form an airflow inlet 1201. , an airflow inlet 1201 is formed by an annular boss 122, the guide groove 1203 is located on the annular boss 122 facing away from the main body 121 of the shell, and the fan mechanism 11 is located between the annular boss 122 of the accommodation cavity 120 and the airflow outlet 1202. , that is, the fan mechanism 11 is disposed in the accommodating cavity 120 , and is disposed at a portion of the accommodating cavity 120 between the annular boss 122 and the airflow outlet 1202 . With such a structural design, when the fan mechanism 11 rotates, a negative pressure is formed in the accommodation cavity 120 , so that the airflow enters the accommodation cavity 120 through the airflow inlet 1201 formed by the annular boss 122 and is discharged through the airflow outlet 1202 .
请参阅图3、图4、图5以及图6,在一些实施方式中,壳体12具有第一端面1211和第二端面1212,第一端面1211和第二端面1212相对设置,其中,气流进口1201设于第一端面1211,而气流出口1202设于第二端面1212,从而可以使得气流从风机10外部经过气流进口1201进入容纳腔120后,在扇叶111旋转带动下,从气流出口1202流出。在一些实施方式中,每个导流槽1203包括第一导流部12031和第二导流部12032,第一导流部12031呈弧形轨迹延伸并与第二导流部12032连接,第二导流部12032设于容纳腔120的内壁面并且第二导流部12032的延伸轨迹与扇叶111的旋转中心轴平行。第一导流部12031作为外部气流进入风机10的前段槽结构,其设计成呈弧形轨迹延伸,使得气流在进入风机10之前,便具有一定的旋向,改善了风机10气流进口1201处的气流流向,从而有利于使得进入风机10的气流所产生的噪声变得更小,有利于改善风机10的声音品质。在一些实施方式中,第一端面1211和容纳腔120的内壁面相互连接的部位形成倒角斜面,第一导流部12031自第一端面1211向倒角斜面延伸并与第二导流部12032连接,从而可以使得第一端面1211的气流在进入气流进口1201时,靠近壳体12的气流层由第一导流部12031导入气流进口1201,以使得靠近第一导流部12031的气流层变成湍流层。在一些实施方式中,扇叶111之旋转中心轴和每个第二导流部12032之中心轴形成一个平面,与第二导流部12032连接的第一导流部12031以与该平面的距离逐渐减小的趋势向第二导流部12032延伸并与第二导流部12032连接,并且第一导流部12031与第二导流部12032连接的一端位于扇叶111旋转的前端,第一导流部12031远离第二导流部12032的一端位于扇叶111旋转的末端。这样的结构设计,有利于流入气流进口1201的气流以预旋的方式进入风机10,起到降噪的作用。需要说明的是,在本公开的实施例中,扇叶111旋转的前端和扇叶111旋转的末端,分别是指一个扇叶111在旋转过程中,扇叶111朝向旋转前方的一端叫做前端,而背对旋转前方的一端叫做末端。Please refer to Figure 3, Figure 4, Figure 5 and Figure 6. In some embodiments, the housing 12 has a first end surface 1211 and a second end surface 1212. The first end surface 1211 and the second end surface 1212 are arranged oppositely, wherein the airflow inlet 1201 is provided on the first end face 1211, and the air flow outlet 1202 is provided on the second end face 1212, so that the air flow can enter the accommodation cavity 120 from the outside of the fan 10 through the air flow inlet 1201, and then flow out from the air flow outlet 1202 driven by the rotation of the fan blade 111. . In some embodiments, each guide groove 1203 includes a first guide part 12031 and a second guide part 12032. The first guide part 12031 extends in an arc-shaped trajectory and is connected to the second guide part 12032. The air guide portion 12032 is provided on the inner wall surface of the accommodation cavity 120 and the extension trajectory of the second air guide portion 12032 is parallel to the rotation center axis of the fan blade 111 . The first guide part 12031 serves as the front groove structure where external airflow enters the fan 10. It is designed to extend in an arc-shaped trajectory, so that the airflow has a certain direction of rotation before entering the fan 10, which improves the airflow inlet 1201 of the fan 10. The air flow direction is beneficial to making the noise generated by the airflow entering the fan 10 smaller, which is beneficial to improving the sound quality of the fan 10 . In some embodiments, the portion where the first end surface 1211 and the inner wall surface of the accommodation cavity 120 are connected to each other forms a chamfered slope, and the first guide portion 12031 extends from the first end surface 1211 to the chamfered slope and connects with the second guide portion 12032 connection, so that when the airflow on the first end surface 1211 enters the airflow inlet 1201, the airflow layer close to the housing 12 is introduced into the airflow inlet 1201 by the first guide part 12031, so that the airflow layer close to the first guide part 12031 becomes into a turbulent layer. In some embodiments, the central axis of rotation of the fan blade 111 and the central axis of each second guide portion 12032 form a plane, and the first guide portion 12031 connected to the second guide portion 12032 is at a distance from the plane. The gradually decreasing trend extends to the second air guide part 12032 and is connected with the second air guide part 12032, and the end connecting the first air guide part 12031 and the second air guide part 12032 is located at the front end of the rotation of the fan blade 111. One end of the air guide portion 12031 away from the second air guide portion 12032 is located at the end of the rotation of the fan blade 111 . Such a structural design is conducive to the airflow flowing into the airflow inlet 1201 entering the fan 10 in a pre-rotating manner, thereby reducing noise. It should be noted that in the embodiment of the present disclosure, the rotating front end of the fan blade 111 and the rotating end of the fan blade 111 respectively refer to the end of the fan blade 111 that faces the front of the rotation during the rotation of the fan blade 111. The end facing away from the front of the rotation is called the end.
请参阅图1、图3、图5,在一些实施方式中,每个导流槽1203的宽度在1.0mm~5mm之间,深度在0.2mm~1.0mm之间,导流槽1203的宽度和深度的尺寸限定,有利于形成湍流层。在一些实施方式中,相邻的两个导流槽1203之间的间距在1.0mm~10.0mm之间,从而有利于进入风机10的气流形成湍流层和平流层,降低气流噪音。 Please refer to Figure 1, Figure 3, and Figure 5. In some embodiments, the width of each guide groove 1203 is between 1.0mm and 5mm, and the depth is between 0.2mm and 1.0mm. The width of the guide groove 1203 and The depth is limited in size, which is conducive to the formation of a turbulent layer. In some embodiments, the distance between two adjacent guide grooves 1203 is between 1.0 mm and 10.0 mm, which is beneficial to the airflow entering the fan 10 forming a turbulent layer and stratosphere, and reducing airflow noise.
请参阅图3,在一些实施方式中,扇叶111至扇叶111之旋转中心轴的最大距离(D)与导流槽1203的槽底壁至扇叶111之旋转中心轴的最小距离(d)的差值在0~10mm之间,以使得经由气流进口1201进入的气流,在形成湍流层后,湍流层的气流完全流至扇叶111并在扇叶111旋转产生的负压下经由气流出口1202流出。Please refer to Figure 3. In some embodiments, the maximum distance (D) from the fan blade 111 to the rotation center axis of the fan blade 111 and the minimum distance (d) from the groove bottom wall of the guide groove 1203 to the rotation center axis of the fan blade 111. ) is between 0 and 10mm, so that after the airflow entering through the airflow inlet 1201 forms a turbulent layer, the airflow in the turbulent layer completely flows to the fan blade 111 and passes through the airflow under the negative pressure generated by the rotation of the fan blade 111 Exit 1202 flows out.
请参阅图7、图8以及图3,在一些实施方式中,扇叶111具有第一扇面1111和第二扇面1112,第一扇面1111朝向气流进口1201,而第二扇面1112背对气流进口1201(即朝向气流出口1202),扇叶111设有多个凹坑1110,凹坑1110自第一扇面1111向第二扇面1112凹陷或者自第二扇面1112向第一扇面1111凹陷,凹坑1110的设计,可以破坏流至扇叶111的层流边界层,使得气流在转捩过程中提前形成湍流边界层,以有效降低扇叶111旋转过程中的形状阻力,使得风机10可以吸入更多的空气,不但提升了风机10的运行效率,而且还降低了运转的噪声。在一些实施方式中,第一扇面1111和第二扇面1112均分布有凹坑1110。在一些实施方式中,扇叶111具有第一侧边缘,第一侧边缘为扇叶111旋转时的前端,凹坑1110靠近第一侧边缘设置。在一些实施方式中,扇叶111还具有第二侧边缘,第二侧边缘为扇叶111旋转时的末端,即第一侧边缘和第二侧边缘为相对的两个边缘,当凹坑1110设置在第一扇面1111时,第一扇面1111具有第一区域11110,且第一区域11110自第一侧边缘向第二侧边缘延伸且与第二侧边缘具有间距,第一区域11110占第一扇面1111面积的30%~40%,凹坑1110设于第一区域11110,沿第一侧边缘至第二侧边缘的方向,多个凹坑1110呈至少一行多列设置,相邻的两个凹坑1110之间具有间距,这样可有效降低气流的阻力,提高风机10运行效率,当然,多个凹坑1110也可以呈多行多列设置,所有的凹坑1110设置在第一区域11110内,可以保障扇叶111的结构强度和结构可靠性。在一些实施方式中,第二扇面1112也具有第一区域11110,并且第二扇面1112的第一区域11110与第一扇面1111的第一区域11110相同,第二扇面1112的第一区域11110上也设有多个凹坑1110。在一些实施方式中,凹坑1110的结构呈半球形或者立方体形或者椎体形,纵剖凹坑1110时,剖切面呈圆弧形或者方形或者锥形。Please refer to Figures 7, 8 and 3. In some embodiments, the fan blade 111 has a first fan surface 1111 and a second fan surface 1112. The first fan surface 1111 faces the airflow inlet 1201, and the second fan surface 1112 faces away from the airflow inlet 1201. (That is, toward the airflow outlet 1202), the fan blade 111 is provided with a plurality of recesses 1110. The recesses 1110 are recessed from the first fan surface 1111 to the second fan surface 1112 or from the second fan surface 1112 to the first fan surface 1111. The recesses 1110 are The design can destroy the laminar flow boundary layer flowing to the fan blade 111, causing the airflow to form a turbulent boundary layer in advance during the transition process, so as to effectively reduce the shape resistance of the fan blade 111 during the rotation process, so that the fan 10 can inhale more air , not only improves the operating efficiency of the fan 10, but also reduces the operating noise. In some embodiments, the first sector surface 1111 and the second sector surface 1112 are both distributed with pits 1110 . In some embodiments, the fan blade 111 has a first side edge, which is the front end of the fan blade 111 when rotating, and the pit 1110 is disposed close to the first side edge. In some embodiments, the fan blade 111 also has a second side edge. The second side edge is the end of the fan blade 111 when it rotates. That is, the first side edge and the second side edge are two opposite edges. When the pit 1110 When set on the first sector 1111, the first sector 1111 has a first area 11110, and the first area 11110 extends from the first side edge to the second side edge and has a distance from the second side edge. The first area 11110 occupies the first 30% to 40% of the area of the sector 1111, the pits 1110 are provided in the first area 11110. Along the direction from the first side edge to the second side edge, a plurality of pits 1110 are arranged in at least one row and multiple columns, two adjacent ones There is a spacing between the pits 1110, which can effectively reduce the resistance of the air flow and improve the operating efficiency of the fan 10. Of course, multiple pits 1110 can also be arranged in multiple rows and columns, and all the pits 1110 are arranged in the first area 11110. , which can ensure the structural strength and structural reliability of the fan blade 111. In some embodiments, the second sector 1112 also has a first area 11110, and the first area 11110 of the second sector 1112 is the same as the first area 11110 of the first sector 1111, and the first area 11110 of the second sector 1112 also has A plurality of pits 1110 are provided. In some embodiments, the structure of the pit 1110 is in the shape of a hemisphere, a cube, or a pyramid. When the pit 1110 is longitudinally sectioned, the cross-sectional surface is in an arc shape, a square shape, or a conical shape.
请参阅图2,在一些实施方式中,风机10还包括固定件13,固定件13设于第二端面1212,并且与壳主体121连接,以用于将风扇机构11封装在容纳腔120中。在一些实施方式中,固定件13设有与气流出口1202连通的排气口(图中未标示),以使得容纳腔120中的气流可以排出。在一些实施方式中,固定件13包括气流篦子131,气流篦子131安装于排气口,从而气流出口1202的气流可以经由气流篦子131排出风机10外。Please refer to FIG. 2 . In some embodiments, the fan 10 further includes a fixing member 13 . The fixing member 13 is provided on the second end surface 1212 and is connected to the housing body 121 for packaging the fan mechanism 11 in the accommodating cavity 120 . In some embodiments, the fixing member 13 is provided with an exhaust port (not labeled in the figure) connected to the air flow outlet 1202 so that the air flow in the accommodation cavity 120 can be discharged. In some embodiments, the fixing member 13 includes an airflow grate 131 , and the airflow grate 131 is installed at the exhaust port, so that the airflow from the airflow outlet 1202 can be discharged out of the fan 10 through the airflow grate 131 .
请参阅图9以及图1至图8,基于上述风机10,本公开实施例还提供一种通信设备20,该通信设备20包括上述任意实施方式的风机10,该风机10作为通信设备20的散热部件,可以有效降低通信设备20在散热过程中的噪音。在一些实施方式中,通信设备20包括设备主体21,风机10安装于设备主体21中,以用于对设备主体21需要进行散热的部件进行散热。Please refer to Figure 9 and Figures 1 to 8. Based on the above-mentioned fan 10, an embodiment of the present disclosure also provides a communication device 20. The communication device 20 includes the fan 10 of any of the above embodiments. The fan 10 serves as a heat sink for the communication device 20. components, which can effectively reduce the noise of the communication device 20 during the heat dissipation process. In some embodiments, the communication device 20 includes a device body 21 , and the fan 10 is installed in the device body 21 to dissipate heat from components of the device body 21 that need to dissipate heat.
上述本公开实施例序号仅仅为了描述,不代表实施例的优劣。以上所述,仅为本公开的具体实施例,但本公开的保护范围并不局限于此,任何熟悉本技术领域的技术人员在本公开揭露的技术范围内,可轻易想到各种等效的修改或替换,这些修改或替换都应涵盖在本公开的保护范围之内。因此,本公开的保护范围应以权利要求的保护范围为准。 The above serial numbers of the embodiments of the present disclosure are only for description and do not represent the advantages and disadvantages of the embodiments. The above are only specific embodiments of the present disclosure, but the protection scope of the present disclosure is not limited thereto. Any person familiar with the technical field can easily think of various equivalent methods within the technical scope disclosed in the present disclosure. Modifications or substitutions, these modifications or substitutions should be covered by the protection scope of this disclosure. Therefore, the protection scope of the present disclosure should be subject to the protection scope of the claims.

Claims (11)

  1. 一种风机,包括:A fan includes:
    风扇机构,所述风扇机构包括扇叶;A fan mechanism, the fan mechanism includes fan blades;
    壳体,所述壳体设有容纳腔、气流进口、气流出口以及多个导流槽,所述气流进口和所述气流出口分别与所述容纳腔连通;所有的所述导流槽均设于所述气流进口的一端,且每个所述导流槽均自所述气流进口沿所述容纳腔的内壁面向所述气流出口所在的方向延伸,相邻的两个所述导流槽之间具有间隔;所述风扇机构收容于所述容纳腔中。A shell, wherein the shell is provided with a accommodating cavity, an airflow inlet, an airflow outlet and a plurality of guide grooves, wherein the airflow inlet and the airflow outlet are respectively connected to the accommodating cavity; all the guide grooves are arranged at one end of the airflow inlet, and each of the guide grooves extends from the airflow inlet along the inner wall of the accommodating cavity toward the direction where the airflow outlet is located, and there is a gap between two adjacent guide grooves; the fan mechanism is accommodated in the accommodating cavity.
  2. 根据权利要求1所述的风机,其中,每个所述导流槽包括第一导流部和第二导流部,所述第一导流部呈弧形轨迹延伸并与所述第二导流部连接,所述第二导流部设于所述容纳腔的内壁面且所述第二导流部的延伸轨迹与所述扇叶的旋转中心轴平行。The fan according to claim 1, wherein each of the guide grooves includes a first guide part and a second guide part, and the first guide part extends in an arc-shaped trajectory and is connected with the second guide part. The flow parts are connected, the second flow guide part is provided on the inner wall surface of the accommodation cavity, and the extension trajectory of the second flow guide part is parallel to the rotation center axis of the fan blade.
  3. 根据权利要求2所述的风机,其中,所述壳体具有第一端面和第二端面,所述第一端面和所述第二端面相对设置,所述气流进口设于所述第一端面,所述气流出口设于所述第二端面;所述第一端面和所述容纳腔的壁面相互连接的部位形成倒角斜面,所述第一导流部自所述第一端面向所述倒角斜面延伸并与所述第二导流部连接。The fan according to claim 2, wherein the housing has a first end surface and a second end surface, the first end surface and the second end surface are arranged oppositely, and the airflow inlet is provided on the first end surface, The airflow outlet is provided on the second end face; the portion where the first end face and the wall of the accommodating cavity are connected to each other forms a chamfered slope, and the first flow guide portion faces the inverted surface from the first end face. The angular slope extends and is connected with the second flow guide part.
  4. 根据权利要求2所述的风机,其中,所述第一导流部以与所述扇叶之旋转中心轴和所述第二导流部之中心轴所形成的平面的距离逐渐减小的趋势向所述第二导流部延伸并与所述第二导流部连接,且所述第一导流部与所述第二导流部连接的一端位于所述扇叶旋转的前端,所述第一导流部远离所述第二导流部的一端位于所述扇叶旋转的末端。The fan according to claim 2, wherein the distance between the first air guide portion and the plane formed by the central axis of rotation of the fan blade and the central axis of the second air guide portion gradually decreases. Extends toward the second air guide part and is connected to the second air guide part, and one end of the first air guide part connected to the second air guide part is located at the front end of the rotation of the fan blade, the An end of the first air guide part away from the second air guide part is located at the end of rotation of the fan blade.
  5. 根据权利要求2所述的风机,其中,每个所述导流槽的宽度在1.0mm~5mm之间、深度在0.2mm~1.0mm之间;The fan according to claim 2, wherein the width of each guide groove is between 1.0mm and 5mm, and the depth is between 0.2mm and 1.0mm;
    和/或,相邻的两个所述导流槽之间的间距在1.0mm~10.0mm之间。And/or, the distance between two adjacent guide grooves is between 1.0 mm and 10.0 mm.
  6. 根据权利要求1至5任一项所述的风机,其中,所述壳体包括壳主体和环形凸台,所述环形凸台与所述壳主体的内壁面连接以形成所述气流进口;所述导流槽背对所述壳主体设于所述环形凸台,所述风扇机构设于所述环形凸台至所述气流出口之间的部位。The fan according to any one of claims 1 to 5, wherein the housing includes a housing body and an annular boss, and the annular boss is connected to an inner wall surface of the housing body to form the airflow inlet; The air guide groove is arranged on the annular boss opposite to the main body of the shell, and the fan mechanism is arranged between the annular boss and the air flow outlet.
  7. 根据权利要求6所述的风机,其中,所述扇叶至所述扇叶之旋转中心轴的最大距离与所述导流槽的槽底壁至所述扇叶之旋转中心轴的最小距离的差值在0~10mm之间。The fan according to claim 6, wherein the maximum distance from the fan blade to the rotation center axis of the fan blade is equal to the minimum distance from the groove bottom wall of the guide groove to the rotation center axis of the fan blade. The difference is between 0 and 10mm.
  8. 根据权利要求1至5任一项所述的风机,其中,所述扇叶具有第一扇面和第二扇面,所述第一扇面朝向所述气流进口,所述第二扇面背对所述气流进口,所述扇叶设有多个凹坑,所述凹坑自所述第一扇面向所述第二扇面凹陷;The fan according to any one of claims 1 to 5, wherein the fan blade has a first fan surface and a second fan surface, the first fan surface faces the airflow inlet, and the second fan surface faces away from the airflow. Inlet, the fan blade is provided with a plurality of pits, the pits are recessed from the first fan surface to the second fan surface;
    和/或,所述凹坑自所述第二扇面向所述第一扇面凹陷。And/or, the pit is recessed from the second sector to the first sector.
  9. 根据权利要求8所述的风机,其中,所述扇叶具有第一侧边缘,所述第一侧边缘为所述扇叶旋转时的前端,所述凹坑靠近所述第一侧边缘设置。The fan according to claim 8, wherein the fan blade has a first side edge, the first side edge is the front end of the fan blade when rotating, and the recess is provided close to the first side edge.
  10. 根据权利要求9所述的风机,其中,所述扇叶还具有第二侧边缘,所述第二侧边缘为所述扇叶旋转时的末端,所述第一扇面和/或所述第二扇面具有第一区域,且所述第一区域自所述第一侧边缘向所述第二侧边缘延伸且与所述第二侧边缘具有间距,所述第一区域占所述第一扇面或所述第二扇面面积的30%~40%,所述凹坑设于所述第一区域。The fan according to claim 9, wherein the fan blade further has a second side edge, and the second side edge is the end of the fan blade when rotating, and the first fan surface and/or the second The sector has a first area, and the first area extends from the first side edge to the second side edge and has a distance from the second side edge, and the first area occupies the first sector or The pits are provided in the first area of 30% to 40% of the second sector area.
  11. 一种通信设备,包括:A communications device including:
    权利要求1至10任一项所述的风机。 The fan according to any one of claims 1 to 10.
PCT/CN2023/112952 2022-09-22 2023-08-14 Fan, and communication device WO2024060878A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN202222518495.X 2022-09-22
CN202222518495.XU CN218644531U (en) 2022-09-22 2022-09-22 Fan and communication equipment

Publications (1)

Publication Number Publication Date
WO2024060878A1 true WO2024060878A1 (en) 2024-03-28

Family

ID=85493355

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2023/112952 WO2024060878A1 (en) 2022-09-22 2023-08-14 Fan, and communication device

Country Status (2)

Country Link
CN (1) CN218644531U (en)
WO (1) WO2024060878A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN218644531U (en) * 2022-09-22 2023-03-17 中兴通讯股份有限公司 Fan and communication equipment

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3164940U (en) * 2010-10-12 2010-12-24 南實企業有限公司 Fan structure
CN203067353U (en) * 2013-01-06 2013-07-17 苏州三星电子有限公司 Fan and air flow regulating device
CN208900387U (en) * 2018-08-14 2019-05-24 顿力集团有限公司 Low noise blade and blower with low noise blade
CN114017392A (en) * 2021-11-12 2022-02-08 杭州老板电器股份有限公司 Flow guiding air inlet ring and centrifugal fan
CN216241400U (en) * 2021-11-12 2022-04-08 杭州老板电器股份有限公司 Air inlet guiding device and centrifugal fan
CN114876828A (en) * 2021-02-05 2022-08-09 全亿大科技(佛山)有限公司 Fan with cooling device
CN218644531U (en) * 2022-09-22 2023-03-17 中兴通讯股份有限公司 Fan and communication equipment

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3164940U (en) * 2010-10-12 2010-12-24 南實企業有限公司 Fan structure
CN203067353U (en) * 2013-01-06 2013-07-17 苏州三星电子有限公司 Fan and air flow regulating device
CN208900387U (en) * 2018-08-14 2019-05-24 顿力集团有限公司 Low noise blade and blower with low noise blade
CN114876828A (en) * 2021-02-05 2022-08-09 全亿大科技(佛山)有限公司 Fan with cooling device
CN114017392A (en) * 2021-11-12 2022-02-08 杭州老板电器股份有限公司 Flow guiding air inlet ring and centrifugal fan
CN216241400U (en) * 2021-11-12 2022-04-08 杭州老板电器股份有限公司 Air inlet guiding device and centrifugal fan
CN218644531U (en) * 2022-09-22 2023-03-17 中兴通讯股份有限公司 Fan and communication equipment

Also Published As

Publication number Publication date
CN218644531U (en) 2023-03-17

Similar Documents

Publication Publication Date Title
WO2024060878A1 (en) Fan, and communication device
KR100405981B1 (en) Structure of turbo fan for cassette type air conditioner
TWI487475B (en) Heat dissipation module
KR101313420B1 (en) Crossflow fan and air conditioner provided with same
JPH11201084A (en) Blowing device
US7760506B1 (en) Electronic components, systems and apparatus with air flow devices
KR20060051506A (en) Airfoil with large fillet and micro-circuit cooling
JP2009516386A (en) Cooler
TWI439609B (en) Centrifugal fan module, heat sink device having the same and electric device having the heat sink device
TW201031880A (en) Spiral heat exchanger
US20140352937A1 (en) Injection plate for microstructure water cooling units for an electrical or electronic component
JP2009299635A (en) Electric blower and vacuum cleaner equipped with the same
TWI809381B (en) Fluid heat exchanger with pump
WO2022001620A1 (en) Color wheel heat dissipation device and projection apparatus using same
TWI655894B (en) Electronic device, computer device and casing thereof
TW202237993A (en) Fan
JP4742965B2 (en) Heat transfer device and liquid cooling system using it
CN210799491U (en) Axial flow cooling fan assembly structure
JP2007138824A (en) Blade unit for centrifugal fan
TW201339808A (en) Electronic device
TW202137865A (en) Liquid cooling module and its liquid cooling head
TWM529763U (en) Flow rate enhanced composite blade structure of axial fan
TWI422747B (en) Cooling fan and impeller thereof
CN217063469U (en) Disc type motor with cooling structure
CN108447510B (en) Electronic equipment, SSD and shell thereof

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 23867172

Country of ref document: EP

Kind code of ref document: A1