COUNTER-ROTATING AXIAL AIR MOVING DEVICE

Abstract

A counter-rotating axial air moving device includes a front rotor and a rear rotor. The front rotor includes a front hub and a plurality of front blades, and the number of the front blades is equal to or greater than 7 and equal to or less than 11. The rear rotor is disposed on the downstream side of the front rotor. The rear rotor includes a rear hub and a plurality of rear blades, and the number of the rear blades is equal to or greater than 6 and equal to or less than 10. The front rotor and the rear rotor are stacked with each other with a total thickness and a diameter. The ratio of the total thickness to the diameter is equal to or more than 0.91 and equal to or less than 1.5.

Claims

1. A counter-rotating axial air moving device, comprising: a front rotor, comprising a front hub and a plurality of front blades arranged annularly on a periphery of the font hub spacedly, and an amount of the front blades being equal to or greater than seven and equal to or less than eleven; and a rear rotor, disposed on a downstream side of the front rotor, comprising a rear hub and a plurality of rear blades arranged annularly on a periphery of the rear hub spacedly, and an amount of the rear blades being equal to or greater than six and equal to or less than ten; wherein, the front rotor and the rear rotor are stacked with each other with a total thickness and a diameter, and a ratio of the total thickness to the diameter is equal to or greater than 0.91 and equal to or less than 1.5, and wherein the total thickness means a thickness of the front hub and the rear hub in an axial direction, and the total diameter means a diameter of an outermost end of the front rotor or the back rotor.

2. The counter-rotating axial air moving device according to claim 1, wherein the front rotor and the rear rotor rotate in opposite direction, and a diameter of the front rotor and a diameter of the rear rotor are the same.

3. The counter-rotating axial air moving device according to claim 1, wherein the front rotor comprises a front rotation speed, and the rear rotor comprises a rear rotation speed, and a ratio of the rear rotation speed to the front rotation speed is equal to or greater than 0.5 and equal to or less than 1.2.

4. The counter-rotating axial air moving device according to claim 1, further comprising: a stator component, located on a front or rear side of the front rotor, on a rear side of the rear rotor, or between the front rotor and the rear rotor.

5. The counter-rotating axial air moving device according to claim 4, wherein the stator component comprises a plurality of pillars or a plurality of stator blades, and the pillars or the stator blades are arranged radially.

6. The counter-rotating axial air moving device according to claim 1, wherein an average pitch angle of the front blades is greater than 55 degrees and less than 72 degrees.

7. The counter-rotating axial air moving device according to claim 6, wherein an average pitch angle of the rear blades is less than the average pitch angle of the front blades.

8. The counter-rotating axial air moving device according to claim 7, wherein the average pitch angle of the rear blades is greater than 50 degrees and less than 67 degrees.

Description

BRIEF DESCRIPTION OF DRAWINGS

[0008] The features of the disclosure believed to be novel are set forth with particularity in the appended claims. The disclosure itself, however, may be best understood by reference to the following detailed description of the disclosure, which describes a number of exemplary embodiments of the disclosure, taken in conjunction with the accompanying drawings, in which:

[0009] FIG. 1 is a perspective schematic view of the counter-rotating axial air moving device of this disclosure.

[0010] FIG. 2 is a side cross sectional view of the counter-rotating axial air moving device of this disclosure.

[0011] FIG. 3 is a top view of the front rotor and the rear rotor of this disclosure.

[0012] FIG. 4 is a schematic view of the pitch angle of the front rotor of this disclosure.

[0013] FIG. 5 is a schematic view of the pitch angle of the rear rotor of this disclosure.

[0014] FIG. 6 is a perspective schematic view of another embodiment of the counter-rotating axial air moving device of this disclosure.

[0015] FIG. 7 is a perspective schematic view of still another embodiment of the counter-rotating axial air moving device of this disclosure.

[0016] FIG. 8 is a perspective schematic view of another embodiment of the counter-rotating axial air moving device of this disclosure.

[0017] FIG. 9 is a comparison diagram of the curves of the static pressure versus air flowrate of the counter-rotating axial air moving device of this disclosure and the counter-rotating axial air moving device of the related art.

DETAILED DESCRIPTION

[0018] The technical contents of this disclosure will become apparent with the detailed description of embodiments accompanied with the illustration of related drawings as follows. It is intended that the embodiments and drawings disclosed herein are to be considered illustrative rather than restrictive.

[0019] Please refer to FIG. 1 and FIG. 2, which depict a perspective schematic view and a side cross sectional view of the counter-rotating axial air moving device of this disclosure. The counter-rotating axial air moving device 1 of this disclosure includes a front rotor 10 and a rear rotor 20. The rear rotor 20 is disposed on the downstream side of the front rotor 10 to configure the counter-rotating axial air moving device 1. Additionally, the rotation directions of the front rotor 10 and the rear rotor 20 are opposite, and the diameter of the front rotor 10 and the diameter of the rear rotor 20 are the same.

[0020] The front rotor 10 includes a front hub 11 and a plurality of front blades 12 arranged annularly on the periphery of the font hub 11 spacedly, and the number of the front blades 12 is equal to or greater than 7 and equal to or less than 11.

[0021] Similarly, the rear rotor 20 includes a rear hub 21 and a plurality of rear blades 22 arranged annularly on the periphery of the rear hub 21 spacedly, and the number of the rear blades 22 is equal to or greater than 6 and equal to or less than 10.

[0022] Moreover, the front rotor 10 and the rear rotor 20 are stacked with each other to have a total thickness T and a diameter D. The ratio of the total thickness T to the diameter D is equal to or greater than 0.91 and equal to or less than 1.5.

[0023] Specifically, in this embodiment, the ratio of the total thickness T to the diameter D is 1.4. Furthermore, the amount of the front blades 12 is 7, and the amount of the rear blades 22 is also 7.

[0024] In one embodiment of this disclosure, the counter-rotating axial air moving device 1 further includes a stator component 30 and a housing 40. The stator component 30 is connected to the housing 40 and is optionally located on the front or rear side of the front rotor 10, on the rear side of the rear rotor 20 or between the front rotor 10 and the rear rotor 20. In some embodiments of this disclosure, the stator component 30 includes a plurality of pillars or a plurality of stator blades with wing sections. The pillars or the stator blades are arranged radially corresponding to the type of the rotor. In this embodiment, the stator element 30 includes a plurality of stator blades, and the function of the stator blades is to recover the rotational kinetic energy of the airflow.

[0025] It should be noted that the front rotor 10 has a front rotation speed, and the rear rotor 20 has a rear rotation speed. In some embodiments, the ratio of the rear rotation speed to the front rotation speed is equal to or greater than about 0.5 and equal to or less than about 1.2 (is not greater than 1.2).

[0026] Please further refer to FIG. 3 to FIG. 5, which depict a top view of the front rotor and the rear rotor of this disclosure, a schematic view of the pitch angle of the front rotor blade of this disclosure, and a schematic view of the pitch angle of the rear rotor blade of this disclosure. In the FIG. 3, the cross-sectional view is made along the line 4-4 of the front blades 12 to form a wing section BA. The angle formed by the nose-tail line LA of the wing section BA and the rotation direction U of the front rotor 10 is defined as the pitch angle θ.sub.A.

[0027] Moreover, the cross-sectional view is made along the line 5-5 of the rear blades 22 to form another wing section BB. The angle formed by the nose-tail line LB of the wing section BB and the rotation direction U of the rear rotor 20 is defined as the pitch angle θ.sub.B.

[0028] It is worth of noticing that the pitch angles of the wing sections on different radius positions may be different. The θ.sub.A mentioned afterward refers to the average pitch angle of the front blades, and the θ.sub.B mentioned afterward refers to the average pitch angle of the rear blades. The average pitch angle θ.sub.A of the front blades 12 of the counter-rotating axial air moving device 1 of this disclosure is greater than about 55 degrees and less than about 72 degrees. Additionally, the average pitch angle θ.sub.B of the rear blades 22 is greater than about 50 degrees and less than about 67 degrees. The average pitch angle θ.sub.B of the rear blades 22 is smaller than the average pitch angle θ.sub.A of the front blades 12. In this embodiment, the average pitch angle θ.sub.A of the front blades 12 is about 60.8 degrees. Moreover, the average pitch angle θ.sub.B of the rear blades 22 is about 54 degrees.

[0029] Please further refer to FIG. 6 to FIG. 8, which depict the other three embodiments of the counter-rotating axial air moving device of this disclosure. The differences between these three embodiments and the previous embodiment are the number of the front blades and the number of the rear blades, and the average pitch angle of the front blades and the average pitch angle of the rear blades.

[0030] As shown in the FIG. 6, in this embodiment, the counter-rotating axial air moving device 1a includes a front rotor 10a and a rear rotor 20a. The front rotor 10a includes a front hub 11a and a plurality of front blades 12a, and the number of the front blades 12a is 9. Additionally, the rear rotor 20a includes a rear hub 21a and a plurality of rear blades 22a, and the number of rear blades 12a is 8.

[0031] Furthermore, in this embodiment, the average pitch angle θ.sub.A of the front blades 12a is about 61 degrees. Moreover, the average pitch angle θ.sub.B of the rear blades 22a is about 54.5 degrees.

[0032] Please refer to FIG. 7, in this embodiment, the counter-rotating axial air moving device 1b includes a front rotor 10b and a rear rotor 20b. The front rotor 10b includes a front hub 11b and a plurality of front blades 12b, and the number of the front blades 12b is 10. Additionally, the rear rotor 20b includes a rear hub 21b and a plurality of rear blades 22b, and the number of the rear blades 12b is also 10.

[0033] Moreover, in this embodiment, the average pitch angle θ.sub.A of the front blades 12b is about 68.5 degrees. The average pitch angle θ.sub.B of the rear blades 22b is about 65 degrees.

[0034] Please further refer to FIG. 8, in this embodiment, the counter-rotating axial air moving device 1c includes a front rotor 10c and a rear rotor 20c. The front rotor 10c includes a front hub 11c and a plurality of front blades 12c, and the number of the front blades 12c is 11. Additionally, the rear rotor 20c includes a rear hub 21c and a plurality of rear blades 22c, and the number of rear blades 22c is 10.

[0035] Moreover, in this embodiment, the average pitch angle θ.sub.A of the front blades 12c is about 67.7 degrees. The average pitch angle θ.sub.B of the rear blades 22c is about 58.1 degrees.

[0036] Please refer to FIG. 9, which depicts a comparison diagram of the curves of the static pressure-air flowrate of the counter-rotating axial air moving device of this disclosure and the counter-rotating axial air moving device of the related art under the same size and the same rotation speed. It is shown in the figures, under the same air pressure, the curve of the characteristic of the counter-rotating axial air moving device of this disclosure (represented in the thin line) is in a higher air flowrate region comparing with the counter-rotating axial air moving device of the related art (represented in the thick line). In other words, in the environment of the same flow resistance, the counter-rotating axial air moving device of this disclosure provides the higher air flowrate. Accordingly, at the same rotating speed, the counter-rotating axial air moving device of this disclosure provides the better characteristics and performance than the counter-rotating axial air moving device of the related art. Therefore, the deterioration of vibration and noise caused by increasing the rotation speed may be avoided, and the energy consumption may be reduced.

[0037] While this disclosure has been described by means of specific embodiments, numerous modifications and variations could be made thereto by those skilled in the art without departing from the scope and spirit of this disclosure set forth in the claims.