US20200224669A1 - Fan blade structure - Google Patents

Fan blade structure Download PDF

Info

Publication number
US20200224669A1
US20200224669A1 US16/245,636 US201916245636A US2020224669A1 US 20200224669 A1 US20200224669 A1 US 20200224669A1 US 201916245636 A US201916245636 A US 201916245636A US 2020224669 A1 US2020224669 A1 US 2020224669A1
Authority
US
United States
Prior art keywords
flow
blades
hub
fan blade
blade structure
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US16/245,636
Inventor
Hsiu-Ching HUNG
Chih-Chien Hsu
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Dyna Rechi Co Ltd
Original Assignee
Dyna Rechi Co Ltd
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 Dyna Rechi Co Ltd filed Critical Dyna Rechi Co Ltd
Priority to US16/245,636 priority Critical patent/US20200224669A1/en
Assigned to DYNA RECHI CO., LTD. reassignment DYNA RECHI CO., LTD. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: HSU, CHIH-CHIEN, HUNG, HSIU-CHING
Publication of US20200224669A1 publication Critical patent/US20200224669A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00Axial-flow pumps
    • F04D19/002Axial flow fans
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/38Blades
    • F04D29/384Blades characterised by form
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/38Blades
    • F04D29/388Blades characterised by construction
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/325Rotors specially for elastic fluids for axial flow pumps for axial flow fans
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/20Rotors
    • F05B2240/30Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2250/00Geometry
    • F05B2250/20Geometry three-dimensional
    • F05B2250/24Geometry three-dimensional ellipsoidal
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/20Rotors
    • F05D2240/30Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05D2240/307Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the tip of a rotor blade

Definitions

  • the present disclosure relates to a fan blade structure. More particularly, the present disclosure relates to a fan blade structure applied to various types of fans.
  • an electric fan and an air conditioner have been developed to reduce environmental discomfort. Due to high cost of the air conditioner, people generally choose the electric fan with lower prices and low power consumption.
  • the electric fans can be divided into box fans, vertical fans, ceiling fans, etc. The electric fan is the most common tool used for cooling because the electric fan can accelerate the convection by creating the airflow while rotating, thereby reducing the temperature.
  • a conventional fan blade structure 3 includes a hub 31 and a plurality of blades 32 , as shown in FIG. 1 .
  • the blades 32 are disposed around a surrounding side of the hub 31 .
  • Each of the blades 32 is obliquely disposed on the surrounding side of the hub 31 . Therefore, the conventional fan blade structure 3 may be cooperated with an actuating unit. When the actuating unit drives the conventional fan blade structure 3 to rotate, the blades 32 can be used for guiding airflow.
  • the conventional fan blade structure 3 cannot effectively increase the flow rate in actual use so as to cause a disadvantage that the flow rate is poor while being used and cannot meet the requirements of actual use.
  • a fan blade structure includes a hub, a plurality of blades and a plurality of flow-guiding units.
  • the hub has a shape of a hollow body.
  • the hub includes an end surface, a mounting surface and a surrounding side.
  • the hub has a shaft hole located in a center of the hub.
  • the blades are disposed around the surrounding side of the hub at intervals.
  • Each of the blades includes a windward surface, a front edge, a rear edge, an outer edge and a connecting section.
  • the windward surface is configured to generate airflow.
  • the front edge is first contacted with air when each of the blades is rotated.
  • the rear edge is disposed opposite to the front edge.
  • the outer edge is connected to the front edge and the rear edge, and the connecting section is connected to the surrounding side.
  • the flow-guiding units are formed on the outer edges of the blades, respectively.
  • Each of the flow-guiding units is composed of a plurality of three-dimensional protrusions.
  • FIG. 1 shows a schematic view of a conventional fan blade structure.
  • FIG. 2 shows one schematic view of a fan blade structure according to one embodiment of the present disclosure.
  • FIG. 3 shows another schematic view of the fan blade structure of FIG. 2 .
  • FIG. 4 shows a schematic front view of the fan blade structure of FIG. 2 .
  • FIG. 5 shows a partial enlarged view of the fan blade structure of FIG. 4 .
  • FIG. 6 shows a schematic view of the fan blade structure disposed on a fan according to another embodiment of the present disclosure.
  • FIG. 7 shows a schematic front view of the fan blade structure disposed on the fan of FIG. 6 .
  • FIG. 2 shows one schematic view of a fan blade structure 1 according to one embodiment of the present disclosure.
  • FIG. 3 shows another schematic view of the fan blade structure 1 of FIG. 2 .
  • FIG. 4 shows a schematic front view of the fan blade structure 1 of FIG. 2 .
  • FIG. 5 shows a partial enlarged view of the fan blade structure 1 of FIG. 4 .
  • the fan blade structure 1 includes a hub 11 , a plurality of blades 12 and a plurality of flow-guiding units 13 .
  • the hub 11 has a shape of a hollow body.
  • the hub 11 includes an end surface 111 , a mounting surface 112 and a surrounding side 113 .
  • the hub 11 has a shaft hole 110 located in a center of the hub 11 .
  • the shaft hole 110 penetrates through the end surface 111 and the mounting surface 112 .
  • a number of the blades 12 is five, but it is not limited thereto.
  • the blades 12 are disposed around the surrounding side 113 of the hub 11 at intervals.
  • Each of the blades 12 includes a windward surface 121 , a front edge 122 , a rear edge 123 , an outer edge 124 and a connecting section 125 .
  • the windward surface 121 is configured to generate airflow.
  • the front edge 122 is first contacted with air when each of the blades is rotated.
  • the rear edge 123 is disposed opposite to the front edge 122 .
  • the outer edge 124 is connected to the front edge 122 and the rear edge 123 .
  • the connecting section 125 is connected to the surrounding side 113 of the hub 11 .
  • the front edge 122 , the rear edge 123 and the outer edge 124 are formed in an arc shape or an irregular shape.
  • the flow-guiding units 13 are formed on the outer edges 124 of the blades 12 , respectively.
  • Each of the flow-guiding units 13 is composed of a plurality of three-dimensional protrusions 131 .
  • the fan blade structure 1 is explained in detail as follows:
  • Each of the three-dimensional protrusions 131 of each of the flow-guiding units 13 has a shape of a tubercle on whale flippers.
  • the three-dimensional protrusions 131 of each of the flow-guiding units 13 have a total length defined as L 2 .
  • the outer edge 124 of each of the blades 12 has a length defined as L 1 .
  • the total length L 2 and the length L 1 satisfy the following equation: L 2 ⁇ L 1 .
  • the three-dimensional protrusions 131 of each of the flow-guiding units 13 may be arranged in a regular shape or an irregular shape. In FIGS. 2-4 , the three-dimensional protrusions 131 of each of the flow-guiding units 13 are arranged in the regular shape, but it is not limited thereto.
  • Shapes of the three-dimensional protrusions 131 of each of the flow-guiding units 13 may be the same, partially different or totally different, and sizes of the three-dimensional protrusions 131 of each of the flow-guiding units 13 may be the same, partially different or totally different.
  • the shapes of the three-dimensional protrusions 131 of each of the flow-guiding units 13 are the same, and the sizes of the three-dimensional protrusions 131 of each of the flow-guiding units 13 are the same, but it is not limited thereto.
  • the three-dimensional protrusions 131 of each of the flow-guiding units 13 may be formed in an arc shape or a geometric shape different from the arc shape. In FIGS. 2-4 , the three-dimensional protrusions 131 of each of the flow-guiding units 13 are formed in the arc shape, but it is not limited thereto.
  • the hub 11 , the blades 12 and the flow-guiding units 13 are integrally connected to each other.
  • Each of the blades 12 is obliquely disposed on the surrounding side 113 of the hub 11 . Accordingly, the fan blade structure 1 of the present disclosure can be completely formed.
  • FIG. 6 shows a schematic view of the fan blade structure 1 disposed on a fan 2 according to another embodiment of the present disclosure.
  • FIG. 7 shows a schematic front view of the fan blade structure 1 disposed on the fan 2 of FIG. 6 .
  • the fan 2 is formed in a folded configuration, but it is not limited thereto.
  • the fan blade structure 1 includes a hub 11 , a plurality of blades 12 and a plurality of flow-guiding units 13 .
  • the detail of the hub 11 , the blades 12 and the flow-guiding units 13 is the same as the embodiments of FIGS. 2-5 , and will not be described again herein.
  • the shaft hole 110 of the hub 11 may be assembled with a motor shaft 21 of the fan 2 .
  • the fan 2 of the present disclosure may be used for dissipating heat.
  • the airflow passes through each of the windward surfaces 121 of the blades 12 so as to allow the airflow to flow through the outer edge 124 of the blades 12 .
  • the blades 12 combined with the flow-guiding units 13 have the shape of the tubercle on whale flippers.
  • the flow-guiding units 13 are formed on the outer edges 124 of the blades 12 , respectively.
  • Each of the flow-guiding units 13 is composed of the three-dimensional protrusions 131 . Accordingly, the outer edges 124 of the blades 12 and a flow path of the fan 2 cause different types of disturbances via the three-dimensional protrusions 131 of the flow-guiding units 13 so as to prevent leakage of the airflow and effectively maintain the airflow in a pressure zone between the blades 12 .
  • the airflow may be concentrated at an outlet of the fan 2 , so that a maximum flow rate of the fan 2 can be effectively increased to reduce the input performance of the motor to a load. In other words, the fan 2 with high-performance capability can be achieved under the same input performance.
  • Table 1 lists actual experimental results of the fan blade structure 1 of the present disclosure and a conventional fan blade structure.
  • An experimental group represents the actual experimental results of the fan blade structure 1 of the present disclosure.
  • the flow-guiding units 13 are formed on the outer edges 124 of the blades 12 , respectively, and each of the flow-guiding units 13 is composed of the three-dimensional protrusions 131 .
  • a control group represents the actual experimental results of the conventional fan blade structure.
  • the conventional fan blade structure includes the blades 12 without the flow-guiding units 13 .
  • Table 1 it is obvious that when the motor of the experiment group is the same as that of the control group, the fan blade structure 1 of the experimental group can reduce a rotational speed with the same flow rate in a wind tunnel test, thereby saving more power.
  • the three-dimensional protrusions 131 of the flow-guiding units 13 respectively formed on the outer edges 124 of the blades 12 can really allow the maximum flow rate of the fan 2 to be effectively increased so as to reduce the input performance of the motor to the load.
  • the fan 2 with high-performance capability can be achieved under the same input performance, thereby saving more power.
  • the fan blade structure 1 of the present disclosure utilizes the three-dimensional protrusions 131 of the flow-guiding units 13 formed on the outer edges 124 of the blades 12 , respectively, to allow the blades 12 and the flow path to cause different types of disturbances so as to prevent leakage of the airflow and effectively maintain the airflow in the pressure zone between the blades 12 .
  • the airflow may be concentrated at an outlet of the fan 2 , so that the maximum flow rate of the fan 2 can be effectively increased to reduce the input performance of the motor to the load.
  • the fan 2 with high-performance capability can be achieved under the same input performance, thereby saving more power.
  • the fan blade structure 1 of the present disclosure utilizes each of the blades 12 cooperated with each of the flow-guiding units 13 to concentrate the airflow, thus increasing the maximum flow rate in actual use.

Abstract

A fan blade structure includes a hub, a plurality of blades and a plurality of flow-guiding units. The hub includes an end surface, a mounting surface and a surrounding side. The hub has a shaft hole located in a center of the hub. The blades are disposed around the surrounding side of the hub at intervals. Each of the blades includes a windward surface, a front edge, a rear edge, an outer edge and a connecting section. The windward surface is configured to generate airflow. The rear edge is disposed opposite to the front edge. The outer edge is connected to the front edge and the rear edge, and the connecting section is connected to the surrounding side. The flow-guiding units are formed on the outer edges of the blades, respectively. Each of the flow-guiding units is composed of a plurality of three-dimensional protrusions.

Description

    BACKGROUND Technical Field
  • The present disclosure relates to a fan blade structure. More particularly, the present disclosure relates to a fan blade structure applied to various types of fans.
  • Description of Related Art
  • In a high temperature environment, if there is no air circulation or airflow disturbance, it will often make people feel more stuffy, even sweaty and uncomfortable. In order to improve such problems, an electric fan and an air conditioner have been developed to reduce environmental discomfort. Due to high cost of the air conditioner, people generally choose the electric fan with lower prices and low power consumption. In general, the electric fans can be divided into box fans, vertical fans, ceiling fans, etc. The electric fan is the most common tool used for cooling because the electric fan can accelerate the convection by creating the airflow while rotating, thereby reducing the temperature.
  • A conventional fan blade structure 3 includes a hub 31 and a plurality of blades 32, as shown in FIG. 1. The blades 32 are disposed around a surrounding side of the hub 31. Each of the blades 32 is obliquely disposed on the surrounding side of the hub 31. Therefore, the conventional fan blade structure 3 may be cooperated with an actuating unit. When the actuating unit drives the conventional fan blade structure 3 to rotate, the blades 32 can be used for guiding airflow.
  • However, in the conventional fan blade structure 3, the airflow is only guided by the blades 32, and there are no flow-guiding units that can be cooperated. Accordingly, the conventional fan blade structure 3 cannot effectively increase the flow rate in actual use so as to cause a disadvantage that the flow rate is poor while being used and cannot meet the requirements of actual use.
  • Therefore, a fan blade structure having the features of solving problems of the conventional fan blade structure is commercially desirable.
  • SUMMARY
  • According to one aspect of the present disclosure, a fan blade structure includes a hub, a plurality of blades and a plurality of flow-guiding units. The hub has a shape of a hollow body. The hub includes an end surface, a mounting surface and a surrounding side. The hub has a shaft hole located in a center of the hub. The blades are disposed around the surrounding side of the hub at intervals. Each of the blades includes a windward surface, a front edge, a rear edge, an outer edge and a connecting section. The windward surface is configured to generate airflow. The front edge is first contacted with air when each of the blades is rotated. The rear edge is disposed opposite to the front edge. The outer edge is connected to the front edge and the rear edge, and the connecting section is connected to the surrounding side. The flow-guiding units are formed on the outer edges of the blades, respectively. Each of the flow-guiding units is composed of a plurality of three-dimensional protrusions.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • The present disclosure can be more fully understood by reading the following detailed description of the embodiment, with reference made to the accompanying drawings as follows:
  • FIG. 1 shows a schematic view of a conventional fan blade structure.
  • FIG. 2 shows one schematic view of a fan blade structure according to one embodiment of the present disclosure.
  • FIG. 3 shows another schematic view of the fan blade structure of FIG. 2.
  • FIG. 4 shows a schematic front view of the fan blade structure of FIG. 2.
  • FIG. 5 shows a partial enlarged view of the fan blade structure of FIG. 4.
  • FIG. 6 shows a schematic view of the fan blade structure disposed on a fan according to another embodiment of the present disclosure.
  • FIG. 7 shows a schematic front view of the fan blade structure disposed on the fan of FIG. 6.
  • DETAILED DESCRIPTION
  • The embodiment will be described with the drawings. For clarity, some practical details will be described below. However, it should be noted that the present disclosure should not be limited by the practical details, that is, in some embodiment, the practical details is unnecessary. In addition, for simplifying the drawings, some conventional structures and elements will be simply illustrated, and repeated elements may be represented by the same labels.
  • FIG. 2 shows one schematic view of a fan blade structure 1 according to one embodiment of the present disclosure. FIG. 3 shows another schematic view of the fan blade structure 1 of FIG. 2. FIG. 4 shows a schematic front view of the fan blade structure 1 of FIG. 2. FIG. 5 shows a partial enlarged view of the fan blade structure 1 of FIG. 4. The fan blade structure 1 includes a hub 11, a plurality of blades 12 and a plurality of flow-guiding units 13.
  • The hub 11 has a shape of a hollow body. The hub 11 includes an end surface 111, a mounting surface 112 and a surrounding side 113. The hub 11 has a shaft hole 110 located in a center of the hub 11. The shaft hole 110 penetrates through the end surface 111 and the mounting surface 112.
  • A number of the blades 12 is five, but it is not limited thereto. The blades 12 are disposed around the surrounding side 113 of the hub 11 at intervals. Each of the blades 12 includes a windward surface 121, a front edge 122, a rear edge 123, an outer edge 124 and a connecting section 125. The windward surface 121 is configured to generate airflow. The front edge 122 is first contacted with air when each of the blades is rotated. The rear edge 123 is disposed opposite to the front edge 122. The outer edge 124 is connected to the front edge 122 and the rear edge 123. The connecting section 125 is connected to the surrounding side 113 of the hub 11. The front edge 122, the rear edge 123 and the outer edge 124 are formed in an arc shape or an irregular shape.
  • The flow-guiding units 13 are formed on the outer edges 124 of the blades 12, respectively. Each of the flow-guiding units 13 is composed of a plurality of three-dimensional protrusions 131.
  • The fan blade structure 1 is explained in detail as follows:
  • Each of the three-dimensional protrusions 131 of each of the flow-guiding units 13 has a shape of a tubercle on whale flippers. The three-dimensional protrusions 131 of each of the flow-guiding units 13 have a total length defined as L2. The outer edge 124 of each of the blades 12 has a length defined as L1. The total length L2 and the length L1 satisfy the following equation: L2<L1.
  • The three-dimensional protrusions 131 of each of the flow-guiding units 13 may be arranged in a regular shape or an irregular shape. In FIGS. 2-4, the three-dimensional protrusions 131 of each of the flow-guiding units 13 are arranged in the regular shape, but it is not limited thereto.
  • Shapes of the three-dimensional protrusions 131 of each of the flow-guiding units 13 may be the same, partially different or totally different, and sizes of the three-dimensional protrusions 131 of each of the flow-guiding units 13 may be the same, partially different or totally different. In FIGS. 2-4, the shapes of the three-dimensional protrusions 131 of each of the flow-guiding units 13 are the same, and the sizes of the three-dimensional protrusions 131 of each of the flow-guiding units 13 are the same, but it is not limited thereto.
  • The three-dimensional protrusions 131 of each of the flow-guiding units 13 may be formed in an arc shape or a geometric shape different from the arc shape. In FIGS. 2-4, the three-dimensional protrusions 131 of each of the flow-guiding units 13 are formed in the arc shape, but it is not limited thereto.
  • The hub 11, the blades 12 and the flow-guiding units 13 are integrally connected to each other.
  • Each of the blades 12 is obliquely disposed on the surrounding side 113 of the hub 11. Accordingly, the fan blade structure 1 of the present disclosure can be completely formed.
  • FIG. 6 shows a schematic view of the fan blade structure 1 disposed on a fan 2 according to another embodiment of the present disclosure. FIG. 7 shows a schematic front view of the fan blade structure 1 disposed on the fan 2 of FIG. 6. In the embodiment, the fan 2 is formed in a folded configuration, but it is not limited thereto. The fan blade structure 1 includes a hub 11, a plurality of blades 12 and a plurality of flow-guiding units 13. In FIGS. 6 and 7, the detail of the hub 11, the blades 12 and the flow-guiding units 13 is the same as the embodiments of FIGS. 2-5, and will not be described again herein.
  • In FIGS. 6 and 7, the shaft hole 110 of the hub 11 may be assembled with a motor shaft 21 of the fan 2. When a user feels hot in the summer, the fan 2 of the present disclosure may be used for dissipating heat. When the user drives a motor to rotate the fan blade structure 1 of the present disclosure, the airflow passes through each of the windward surfaces 121 of the blades 12 so as to allow the airflow to flow through the outer edge 124 of the blades 12. In addition, the blades 12 combined with the flow-guiding units 13 have the shape of the tubercle on whale flippers. The flow-guiding units 13 are formed on the outer edges 124 of the blades 12, respectively. Each of the flow-guiding units 13 is composed of the three-dimensional protrusions 131. Accordingly, the outer edges 124 of the blades 12 and a flow path of the fan 2 cause different types of disturbances via the three-dimensional protrusions 131 of the flow-guiding units 13 so as to prevent leakage of the airflow and effectively maintain the airflow in a pressure zone between the blades 12. The airflow may be concentrated at an outlet of the fan 2, so that a maximum flow rate of the fan 2 can be effectively increased to reduce the input performance of the motor to a load. In other words, the fan 2 with high-performance capability can be achieved under the same input performance.
  • Table 1 lists actual experimental results of the fan blade structure 1 of the present disclosure and a conventional fan blade structure. An experimental group represents the actual experimental results of the fan blade structure 1 of the present disclosure. The flow-guiding units 13 are formed on the outer edges 124 of the blades 12, respectively, and each of the flow-guiding units 13 is composed of the three-dimensional protrusions 131. A control group represents the actual experimental results of the conventional fan blade structure. The conventional fan blade structure includes the blades 12 without the flow-guiding units 13. In Table 1, it is obvious that when the motor of the experiment group is the same as that of the control group, the fan blade structure 1 of the experimental group can reduce a rotational speed with the same flow rate in a wind tunnel test, thereby saving more power. Therefore, the three-dimensional protrusions 131 of the flow-guiding units 13 respectively formed on the outer edges 124 of the blades 12 can really allow the maximum flow rate of the fan 2 to be effectively increased so as to reduce the input performance of the motor to the load. In other words, the fan 2 with high-performance capability can be achieved under the same input performance, thereby saving more power.
  • TABLE 1
    Rotational
    Flow Rate Voltage Power Speed
    Item CFM V W rpm Qmax/W
    Control 509.24 110 9.01 931 56.5194
    group
    Experimental 509.52 110 8 885 63.69
    group
  • According to the aforementioned embodiments and examples, the fan blade structure 1 of the present disclosure utilizes the three-dimensional protrusions 131 of the flow-guiding units 13 formed on the outer edges 124 of the blades 12, respectively, to allow the blades 12 and the flow path to cause different types of disturbances so as to prevent leakage of the airflow and effectively maintain the airflow in the pressure zone between the blades 12. The airflow may be concentrated at an outlet of the fan 2, so that the maximum flow rate of the fan 2 can be effectively increased to reduce the input performance of the motor to the load. In other words, the fan 2 with high-performance capability can be achieved under the same input performance, thereby saving more power. Hence, the fan blade structure 1 of the present disclosure utilizes each of the blades 12 cooperated with each of the flow-guiding units 13 to concentrate the airflow, thus increasing the maximum flow rate in actual use.
  • Although the present disclosure has been described in considerable detail with reference to certain embodiments thereof, other embodiments are possible. Therefore, the spirit and scope of the appended claims should not be limited to the description of the embodiments contained herein.
  • It will be apparent to those skilled in the art that various modifications and variations can be made to the structure of the present disclosure without departing from the scope or spirit of the disclosure. In view of the foregoing, it is intended that the present disclosure cover modifications and variations of this disclosure provided they fall within the scope of the following claims.

Claims (8)

What is claimed is:
1. A fan blade structure, comprising:
a hub having a shape of a hollow body, wherein the hub comprises an end surface, a mounting surface and a surrounding side, and the hub has a shaft hole located in a center of the hub;
a plurality of blades disposed around the surrounding side of the hub at intervals, wherein each of the blades comprises a windward surface, a front edge, a rear edge, an outer edge and a connecting section, the windward surface is configured to generate airflow, the front edge is first contacted with air when each of the blades is rotated, the rear edge is disposed opposite to the front edge, the outer edge is connected to the front edge and the rear edge, and the connecting section is connected to the surrounding side of the hub; and
a plurality of flow-guiding units formed on the outer edges of the blades, respectively, wherein each of the flow-guiding units is composed of a plurality of three-dimensional protrusions.
2. The fan blade structure of claim 1, wherein each of the three-dimensional protrusions of each of the flow-guiding units has a shape of a tubercle on whale flippers.
3. The fan blade structure of claim 2, wherein the three-dimensional protrusions of each of the flow-guiding units have a total length defined as L2, the outer edge of each of the blades has a length defined as L1, and the total length L2 and the length L1 satisfy the following equation:

L2<L1.
4. The fan blade structure of claim 3, wherein the three-dimensional protrusions of each of the flow-guiding units are arranged in a regular shape or an irregular shape.
5. The fan blade structure of claim 4, wherein shapes of the three-dimensional protrusions of each of the flow-guiding units are the same, partially different or totally different, and sizes of the three-dimensional protrusions of each of the flow-guiding units are the same, partially different or totally different.
6. The fan blade structure of claim 5, wherein the three-dimensional protrusions of each of the flow-guiding units are formed in an arc shape or a geometric shape different from the arc shape.
7. The fan blade structure of claim 1, wherein the hub, the blades and the flow-guiding units are integrally connected to each other.
8. The fan blade structure of claim 1, wherein each of the blades is obliquely disposed on the surrounding side of the hub.
US16/245,636 2019-01-11 2019-01-11 Fan blade structure Abandoned US20200224669A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US16/245,636 US20200224669A1 (en) 2019-01-11 2019-01-11 Fan blade structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US16/245,636 US20200224669A1 (en) 2019-01-11 2019-01-11 Fan blade structure

Publications (1)

Publication Number Publication Date
US20200224669A1 true US20200224669A1 (en) 2020-07-16

Family

ID=71516338

Family Applications (1)

Application Number Title Priority Date Filing Date
US16/245,636 Abandoned US20200224669A1 (en) 2019-01-11 2019-01-11 Fan blade structure

Country Status (1)

Country Link
US (1) US20200224669A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20230184259A1 (en) * 2021-12-14 2023-06-15 Giga-Byte Technology Co., Ltd. Fan device

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6428277B1 (en) * 2001-05-17 2002-08-06 Siemens Vdo Automotive Inc. High speed, low torque axial flow fan
US20100284817A1 (en) * 2007-10-19 2010-11-11 Joachim Bamberg Method for producing a blisk or a bling, component produced therewith and turbine blade
US20130149108A1 (en) * 2010-08-23 2013-06-13 Rolls-Royce Plc Blade
US8512004B2 (en) * 2007-07-11 2013-08-20 Daikin Industries, Ltd. Propeller fan
US20180057141A1 (en) * 2016-08-31 2018-03-01 David E. Shormann Biomimetic airfoil bodies and methods of designing and making same

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6428277B1 (en) * 2001-05-17 2002-08-06 Siemens Vdo Automotive Inc. High speed, low torque axial flow fan
US8512004B2 (en) * 2007-07-11 2013-08-20 Daikin Industries, Ltd. Propeller fan
US20100284817A1 (en) * 2007-10-19 2010-11-11 Joachim Bamberg Method for producing a blisk or a bling, component produced therewith and turbine blade
US20130149108A1 (en) * 2010-08-23 2013-06-13 Rolls-Royce Plc Blade
US20180057141A1 (en) * 2016-08-31 2018-03-01 David E. Shormann Biomimetic airfoil bodies and methods of designing and making same

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20230184259A1 (en) * 2021-12-14 2023-06-15 Giga-Byte Technology Co., Ltd. Fan device

Similar Documents

Publication Publication Date Title
US8919300B2 (en) Vehicle with fan unit producing an amplified air flow to a heat exchanger
US10052931B2 (en) Outdoor cooling unit in vehicle air-conditioning apparatus
US10606325B2 (en) Thermal management components for electronic devices
US20070284955A1 (en) Heat dissipating fan
TW201440625A (en) Heat dissipation module
US20200224669A1 (en) Fan blade structure
US20220252081A1 (en) Fan
US7959413B2 (en) Fan and impeller thereof
US20030123988A1 (en) Fan blades
US7018175B2 (en) Airflow guiding structure for a heat dissipation fan
CN102768894A (en) Heat dissipating device for transformer
JP6398086B2 (en) Blower and air conditioner using the same
CN207010011U (en) A kind of heat radiating type power distribution cabinet
US20220159880A1 (en) Inverter and heat radiation structure thereof
TWM581150U (en) Fan blade structure
US11668318B2 (en) Blade structure with multiple blade angles and heat dissipation device
JP2013160137A (en) Electric fan
CN209781287U (en) Fan blade structure
US9890795B2 (en) Cooling fan structure
CN206975592U (en) A kind of computer radiator with dust reduction capability
CN105404371A (en) Server fan regulating method considering duct synergistic effect
WO2018205310A1 (en) Multi-hole fan rear cover and front cover, fan cover consisting of same and fan consisting of same
CN204961059U (en) Radiator unit , engine cooling system and vehicle
JP2000205180A (en) Cross flow fan and fluid feeding device using it
CN210533140U (en) Air conditioning equipment and heat radiation structure

Legal Events

Date Code Title Description
AS Assignment

Owner name: DYNA RECHI CO., LTD., TAIWAN

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:HUNG, HSIU-CHING;HSU, CHIH-CHIEN;REEL/FRAME:047968/0773

Effective date: 20190111

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION