Turbo fan

Abstract

A turbo fan includes a plurality of blades positioned vertically in a radial direction between a main plate and a shroud. Each of the plurality of blades is formed with a slope at an outer periphery thereof to suppress generation of turbulence.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

These and/or other aspects and advantages of the present general inventive concept will become apparent and more readily appreciated from the following description of the embodiments, taken in conjunction with the accompanying drawings of which:

FIG. 1 is a cross-sectional view of an air conditioner having a conventional turbo fan;

FIG. 2 is a perspective view illustrating a structure of the conventional turbo fan of FIG. 1;

FIG. 3 is a perspective view illustrating a structure of a conventional turbo fan different from that illustrated in FIG. 2;

FIG. 4 illustrates a perspective view of a turbo fan according to an embodiment of the present general inventive concept; and

FIGS. 5A and 5B are partially cross-sectional views illustrating a blade included in the turbo fan of FIG. 4; and

FIG. 6A is a table illustrating experimental performance of the conventional turbo fan illustrated in FIG. 3, and FIG. 6B is a table illustrating experimental performance of the turbo fan according to an embodiment of the present general inventive concept.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

Reference will now be made in detail to the embodiments of the present general inventive concept, examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to the like elements throughout. The embodiments are described below in order to explain the present general inventive concept by referring to the figures.

FIG. 4 illustrates a perspective view of a turbo fan according to an embodiment of the present general inventive concept, and FIGS. 5A and 5B are partially cross-sectional views illustrating a blade included in the turbo fan of FIG. 4.

Referring to FIG. 4, a turbo fan 100 according to an embodiment of the present general inventive concept may include a main plate 30 having a hub 31 positioned at the center thereof and coupled to a rotational shaft of a fan motor (not illustrated), a plurality of blades 40 arranged radially at predetermined intervals on an outer periphery of the main plate 30 while being coupled perpendicularly to the main plate 30, and a shroud 50 coupled in a ring shape to upper surfaces of the respective blades 40 to prevent vibration and to guide air flow.

The main plate 30 may have a disc shape having a predetermined thickness, and may include the hub 31 positioned at the center thereof to connect with the fan motor (not illustrated), and a connection boss 32 formed at the center of the hub 31 to allow insertion of the rotational shaft of the fan motor (not illustrated) therein.

The hub 31 may protrude in a front direction from the main plate 30 to define a space at a rear side of the hub 31 such that the rotational shaft of the fan motor (not illustrated) can be inserted into the space, and the hub 31 may have holes 33 formed in a circumferential pattern outside the connection boss 32 to prevent overheating of the fan motor (not illustrated).

The blades 40 are disposed such that, when receiving a rotational force from the fan motor (not illustrated), the blades 40 rotate along with the rotational shaft of the fan motor (not illustrated) to generate a centrifugal force or a centripetal force to suck air axially with respect to the turbo fan 100 and to discharge air radially with respect to the turbo fan 100. To this end, the plurality of blades 40 are vertically installed to the main plate 30, and arranged at predetermined intervals on an outer periphery of the main plate 30 to define a curved pathway between the blades 40.

The plurality of blades 40 may be formed to have a constant thickness in order to reduce shrinkages or molding imperfections which can occur upon injection molding of streamline-shaped blades. In addition, a portion of each blade 40 may be located on the main plate 30, and a remaining portion of each blade 40 may extend away from the main plate 30. In other words, each blade 40 may have an inlet side 41 located on the main plate 30, and an outlet side provided as an extension 42 extending away from the main plate 30.

The shroud 50 is positioned in a ring shape on first ends of the blades 40 while connecting the respective blades 40. The shroud 50 is rounded in the axial direction such that a diameter of the shroud 50 gradually decreases towards a front side thereof extending away from the main plate 30.

The shroud 50 defines at a center thereof a suction port 101 through which air is sucked. In addition, discharge ports 102 are formed at a side of the turbo fan 100, that is, at an outside of pathways defined between the blades 40 and between the shroud 50 and the main plate 30. Accordingly, when the turbo fan 100 is rotated by a driving force of the fan motor (not illustrated), air is sucked into the turbo fan 100 through the suction port 101 defined inside the shroud 50 by the rotational force of the turbo fan 100, and is discharged towards the discharge ports 102 through the pathways between the blades 40.

In the turbo fan according to an embodiment of the present general inventive concept, each blade 40 may be formed with a slope 43 at an outer periphery thereof to suppress a generation of turbulence.

In other words, as the blades 40 are rotated, turbulence is generated along the end of the extension 42 of each blade 40, causing a noise of the turbo fan 100. Thus, in order to reduce the noise by reducing the generation of turbulence, the slope 43 can be formed at the end of the extension 42 of each blade 40.

While FIG. 4 illustrates the slope 43 as being formed at the lower end of the extension 42 of each blade 40, the present general inventive concept is not limited thereto, and the slope 43 may be formed at a lateral end along with the lower end of the extension 42 of each blade 40. The slope 43 may also be formed downwardly with respect to a rotational direction of the blades 40. In addition, the slope 43 may be formed with various slope surfaces including, for example, a straight line shape and a streamline shape as illustrated in FIGS. 5A and 5B. Additionally, the slope 43 may be formed at an angle of 45˜60 degrees downwardly with respect to the rotational direction of the blades 40, and the slope 43 at the extension 42 may be disposed such that an edge is not formed on the extension 42 of each blade 40.

FIG. 6A is a table illustrating experimental performance of the conventional turbo fan illustrated in FIG. 3, and FIG. 6B is a table illustrating experimental performance of a turbo fan according to an embodiment of the present general inventive concept.

As illustrated in FIGS. 6A and 6B, according to results of experiments performed using the conventional turbo fan and the turbo fan according to an embodiment of the present general inventive concept in various conditions of an air volume, noise is reduced by about 0.7˜0.8 dBA in the turbo fan according to the present general inventive concept under a condition in which the air volume for both turbo fans is maintained at substantially the same level.

These results also illustrate that the turbo fan according to an embodiment of the present general inventive concept can generate a greater air volume than the conventional turbo fan under the same noise condition.

A turbo fan according to an embodiment of the present general inventive concept can be applied to a variety of applications, such as the air conditioner illustrated in FIG. 1.

In addition, according to an embodiment of the present general inventive concept, a main plate of a turbo fan may have an outer diameter less than or equal to an inner diameter of a shroud so that, when forming the turbo fan using a single mold, the turbo fan can be easily taken out from the mold. Accordingly, a turbo fan according to an embodiment of the present general inventive concept integrally comprising a main plate, a plurality of blades and a shroud can be produced without performing a post-machining process in which, after integrally molding the main plate and the plurality of blades, the shroud is separately molded and attached to the blades.

A turbo fan according to an embodiment of the present general inventive concept can also be integrally formed by injection molding, and reduce noise by a simple modification of an outer appearance to have a slope formed at each of the blades.

A turbo fan according to an embodiment of the present general inventive concept may have slopes formed at the outer periphery of a plurality of blades at an outlet side thereof to suppress a generation of turbulence, thereby reducing noise.

Although a few embodiments of the present general inventive concept have been shown and described, it will be appreciated by those skilled in the art that changes may be made in these embodiments without departing from the principles and spirit of the general inventive concept, the scope of which is defined in the appended claims and their equivalents.

Claims

1. A turbo fan, comprising: a plurality of blades positioned vertically in a radial direction from a center point and between a main plate and a shroud, wherein each of the blades is formed with a slope at an outer periphery thereof to suppress generation of turbulence.

2. The turbo fan according to claim 1, wherein the slope is formed at a lower end of each blade.

3. The turbo fan according to claim 2, wherein the slope is formed downwardly with respect to a rotational direction of the blade.

4. The turbo fan according to claim 1, wherein the slope is formed in a streamline shape.

5. The turbo fan according to claim 1, wherein the slope is formed in a straight line shape.

6. The turbo fan according to claim 3, wherein the main plate has an outer diameter less than or equal to an inner diameter of the shroud.

7. The turbo fan according to claim 6, wherein the main plate, the shroud, and the blade are integrally formed through inject molding.

8. A turbo fan, comprising: a plurality of blades positioned vertically in a radial direction from a point and between a main plate and a shroud, wherein the blades are formed to have a constant thickness, and are formed with a slope at an outer periphery thereof to suppress generation of turbulence.

9. The turbo fan according to claim 8, wherein each of the blades has an extension extending a predetermined length toward a discharge side with respect to the main plate, and the slope is formed at a lower surface of the extension.

10. The turbo fan according to claim 8, wherein the slope is formed downwardly with respect to a rotational direction of the blade.

11. A turbo fan, comprising: a main plate having a circular shape;a plurality of blades connected to the main plate at a first side thereof, the blades extending radially outward along the main plate at predetermined intervals and having a sloped portion on an outer part of the first side thereof; anda shroud connected to an inner part of a second side of the plurality of blades such that the shroud is parallel to the main plate.

12. The turbo fan of claim 11, wherein the plurality of blades each curve as they extend radially away from the center of the main plate.

13. The turbo fan of claim 11, wherein the plurality of blades are separated from each other at equal intervals.

14. The turbo fan of claim 11, wherein the shroud is formed in a ring shape.

15. The turbo fan of claim 11, wherein the sloped portion extends along the first side of the blade.

16. A turbo fan, comprising: a plurality of blades;a main plate coupled to a first side of each blade at a first portion of each of the plurality of blades such that the plurality of blades are arranged radially from a center point of the main plate at predetermined intervals and a second portion of the first side of each blade extends away from the main plate and has a slope; anda shroud coupled to each of the plurality of blades at a second side of each blade opposite to the first side of each blade coupled to the main plate.

17. The turbo fan of claim 16, wherein the shroud defines a suction port in the center thereof to guide an intake of air.

18. The turbo fan of claim 16, wherein the slope is formed on the second portion of the first side not coupled to the main plate.

19. The turbo fan of claim 16 wherein the slope is disposed at the first side in a position such that an edge is not formed at the periphery of the first side of each blade.