In
However, this conventional blower adopts a design of radially compressed air passage as shown in
An object of the present invention is to provide a heat-dissipating device with an axially compressed air passage.
Another object of the present invention is to provide a heat-dissipating device utilizing an axially compressed air passage for enabling the airflow to smoothly flow in the air passage inside the frame thereof so as to enhance its performance.
According to the present invention, the heat-dissipating device includes a housing having at least one air inlet and at least one air outlet, and a rotor disposed in the housing, wherein the housing has a first extending part extending along an axial direction of the heat-dissipating device to form an axially compressed air passage inside the housing.
Preferably, an axially extending depth of the first extending part is gradually increased from the air outlet to a position far away from the air outlet.
The housing further includes a second extending part axially extending corresponding to the first extending part to form a two-side axially compressed air passage inside the housing. An axially extending depth of the second extending part is gradually increased from the air outlet to a position far away from the air outlet. Preferably, an axially extending depth of the first or second extending part is gradually decreased to almost become zero near the air outlet.
Alternatively, the first and second extending parts are formed in a mirror image configuration in the axial direction. Preferably, the housing further comprises a radially compressed air passage inside the housing.
On the other hand, the rotor comprises a base, a hub, a first set of blades and a second set of blades. The first set of blades extends from a periphery of the hub to a surface of the base and the second set of blades is disposed on the base. The base, the hub, the first and second sets of blades can be integrally formed as a single unit.
Additionally, the housing further includes a first frame for accommodating the rotor therein, and a second frame coupled to the first frame, provided with the air inlet, and having a sidewall extending from a periphery of the air inlet to define an air-gathering chamber in the housing. The sidewall has a flange radially extending from one end thereof to define an entrance of the air-gathering chamber, and each of the blades has an end extending toward the entrance of the air-gathering chamber for guiding the airflow into the air-gathering chamber. The air-gathering chamber partially or completely overlaps an air passage through the rotor in height along an axis of the heat-dissipating device.
The second frame further comprises a plurality of air-guiding members disposed along the sidewall for increasing a blast pressure of airflow passing through the heat-dissipating device. In addition, the second frame has a support mounted inside the air inlet and the plurality of air-guiding members are arranged between the sidewall and the support. The plurality of air-guiding members can be shaped as strip, plate, curved, inclined or airfoil structures.
Additionally, the first frame has a bearing tube for allowing a first bearing to be disposed therein and the support of the second frame receives a second bearing so as to jointly support a shaft of the rotor with the first bearing.
The present invention is more fully understood by reading the subsequent detailed description and examples with references made to the accompanying drawings, wherein:
Please refer to
The first frame 21 includes a bearing tube 211 for receiving and supporting the driving device 23 and the bearing 231 is mounted inside the bearing tube 211 for supporting a rotating shaft 27 of the rotor 25. The second frame 22 includes an air inlet 221 and a sidewall 222 extending downward from an inner margin of the air inlet 221. When the first frame 21 and the second frame 22 are assembled together, a space will be formed inside the heat-dissipating device and can be divided to an air-gathering chamber 26 and a partition for disposing the rotor 25 therein by the sidewall 222. An air outlet 212 is also formed simultaneously as shown in
The rotor 25 includes a hub 251, a base 252 radially extending from the bottom end of the hub 251, a first set of blades 253 and a second set of blades 254, and is driven by the driving device 23 coupled inside the hub 251. The first and second sets of blades 253, 254 are curved blades disposed on the base 252, respectively, and each blade has one end extending toward the entrance 261 of the air-gathering chamber 26, wherein the first set of blades is extended downward from the outer periphery of the hub 251 to the surface of the base 252. The first and second sets of blades are alternately arranged as shown in
The second frame 22 further has a support 224 mounted inside the air inlet and a plurality of air-guiding members 225 are disposed between the support 224 and the sidewall 222 for increasing the blast pressure of the heat-dissipating device. The number, shape and arrangement of the air-guiding members can be modified or selected according to the actual application. The plurality of air-guiding members can be shaped as strip, plate, curved, inclined or airfoil structures. In addition, if the aspect of the present invention is applied to an upside-down blower, a two-suction blower or an axial-flow fan, the air-guiding members can be disposed on one of the air inlets or both.
As the rotor 25 rotates, the airflow is intaked into the air inlet 221, passes through the air-guiding members 225 and the blades 253, 254, and is guided into the air-gathering chamber 26 via the entrance 261. In the air-gathering chamber 26, the airflow is gradually collected and discharged therefrom to the exterior at a high pressure via the air outlet 212, which can prevent the sudden change of the airflow pressure. Thus, the airflow sequentially passes through the air inlet 221, the air-guiding members 225, the blades 253, 254 and the entrance 261 of the air-gathering chamber 26.
Because the sidewall 222 extends downward from the inner margin of the air inlet 221 and separates the air-gathering chamber 26 from the rotor 25 and the size of the air outlet 212 is reduced, time of airflow pressurization by the rotor 25 is increased such that the variation in airflow pressure are stabilized. Further, because the height of the air-gathering chamber 26 partially or completely overlaps that of the flow passage through the rotor 25 and the air-guiding members 225 in the axial direction, the occupied space of the centrifugal fan can be minimized. The cross-sectional area of the air-gathering chamber 26 is substantially equal in size to that of the air outlet 212 such that airflow can constantly and stably flow within the air-gathering chamber 26 and the air outlet 212 to prevent work loss.
On the other hand, the present invention adopts a two-side motor fixed design, as shown in
As shown in
In addition to the above-described one-side axially compressed airflow passage, another two-side axially compressed airflow passage can also be adopted. As shown in
In conclusion, the present invention provides a heat-dissipating device utilizing an one-side or two-side axially compressed air passage for enabling the airflow to smoothly flow in the air passage inside the frame thereof so as to enhance its performance.
While the invention has been described in connection with what is presently considered to be the most practical and preferred embodiment, it is to be understood that the invention is not limited to the disclosed embodiments, but, on the contrary, is intended to accommodate various modifications and equivalent arrangements included within the spirit and scope of the appended claims.
Number | Date | Country | Kind |
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93117624 A | Jun 2004 | TW | national |
The present invention is a continuation-in-part application of the parent application bearing Ser. No. 10/848,074 and filed on May 19, 2004 now U.S. Pat. No. 7,241,110. The present invention relates to a heat-dissipating device, and in particular to a high-pressure centrifugal fan with an axially compressed air passage.
Number | Name | Date | Kind |
---|---|---|---|
3407995 | Kinsworthy | Oct 1968 | A |
5188508 | Scott et al. | Feb 1993 | A |
5257904 | Sullivan | Nov 1993 | A |
5982064 | Umeda et al. | Nov 1999 | A |
5997246 | Humbad | Dec 1999 | A |
6179561 | Horng | Jan 2001 | B1 |
6802699 | Mikami et al. | Oct 2004 | B2 |
Number | Date | Country |
---|---|---|
1369671 | Sep 2002 | CN |
2533304 | Jan 2003 | CN |
2 223 066 | Nov 1973 | DE |
2 223 066 | Oct 2003 | DE |
203 09 621 | Oct 2003 | DE |
0 846 868 | Jun 1998 | EP |
1 178 215 | Feb 2002 | EP |
39-10991 | Jun 1964 | JP |
53-10402 | Jul 1976 | JP |
60-130114 | Jul 1985 | JP |
61-078776 | May 1986 | JP |
3038538 | Jun 1997 | JP |
2001-182691 | Jul 2001 | JP |
2002-257085 | Sep 2002 | JP |
2003-206891 | Jul 2003 | JP |
2004-01635 | Jan 2004 | JP |
Number | Date | Country | |
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20050260073 A1 | Nov 2005 | US |
Number | Date | Country | |
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Parent | 10848074 | May 2004 | US |
Child | 11150236 | US |