In
However, because the blades of the impeller are arranged in the same height and have the same outer diameter, such designs will limit the air flowing way and their application.
According to one aspect of the present invention, the heat-dissipating device includes a housing having at least one opening, and a rotor disposed in the housing and having a base, a hub, a first set of blades disposed around the hub, and a second set of blades disposed on the base.
Preferably, the first set of blades extends downward from a periphery of the hub to a surface of the base. The first and second sets of blades are alternately arranged.
Alternatively, the first and second sets of blades are correspondingly partially connected with each other.
Preferably, the first and second sets of blades are shaped as curved or airfoil structures, respectively.
Preferably, the first and second sets of blades are correspondingly connected with each other and bent to different directions.
The base, the hub, the first and second sets of blades are integrally formed as a single unit. Alternatively, the hub and the first set of blades are integrally formed as a first unit, and the base and the second set of blades are integrally formed as a second unit to be assembled with the first unit.
In addition, the housing further includes a first frame for accommodating the rotor therein, and a second frame coupled to the first frame, provided with the opening and having a sidewall extending from a periphery of the opening inwardly to define an air-gathering chamber in the housing.
The second frame further includes a plurality of air-guiding members disposed along the sidewall for increasing a blast pressure of airflow passing through the heat-dissipating device. Preferably, the plurality of air-guiding members are shaped as strip, plate, curved, inclined or airfoil structures. Additionally, the second frame further includes a support mounted inside the opening and the plurality of air-guiding members are arranged between the sidewall and the support.
On the other hand, 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.
Preferably, the heat-dissipating device further includes an another set of air-guiding members disposed on an air outlet of the housing.
Additionally, 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.
Preferably, 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 cross-sectional area of the air-gathering chamber is substantially equal in size to that of an air outlet of the housing.
The second frame has an extending part formed on an inner surface thereof and extending toward a direction of the first frame to form an axially compressed airflow passage in the housing.
According to another aspect of the present invention, the heat-dissipating device includes a housing having an air inlet and an air outlet, and a rotor disposed in the housing, and having a first set of blades and a second set of blades, both of which have upper edges facing to the air inlet and positioned at different heights.
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.
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
In addition, the second frame 22 has an extending part 29 formed on an inner side thereof and axially extending toward the direction of the first frame 21 to form an axially compressed airflow passage in the housing as shown in
Certainly, the size, shape, and arrangement of the blade structure of the rotor include but not limited to those shown in
The above-described air-guiding members 225 can be disposed on the air inlet, but another similar air-guiding members 28 can also be mounted on the air outlet 212 as shown in
Finally, please refer to
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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93117623 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 a composite blade structure.
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Number | Date | Country | |
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Number | Date | Country | |
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Parent | 10848074 | May 2004 | US |
Child | 11150178 | US |