Hereinafter, a cooling structure according to the present invention will be described in detail with reference to embodiments shown in the drawing.
A loss generated in the IGBT module 2 and the diode module 3 thermally conducts to the cooling fin 1. A cooling fin part of the fin 1 is configured so that wind is drawn out by the cooling fan 7 for the purpose of forced air cooling. As a result, heat generated in the IGBT module 2 and the diode module 3 is dissipated here, into ambient atmosphere air.
It is generally known that the cooling fin 1 has high efficiency at a back side of a base surface la and at a portion of a fin 1b close to the base surface 1a, and the efficiency decreases toward a tip of the fin 1b (on opposite side to the base surface 1a).
In addition, when considering the cooling fin 1 as one stream tube for example, the mass of fluid flowing though each cross-sectional area S of the stream tube per unit time is the same as that of the other if the stream tube does not have a portion where air gushes out or is sucked into. Thus, the following Numerical Expression 1 is generally known as a continuity equation.
ρvS=constant (Numerical Expression 1)
where v is a fluid velocity, and ρ is a fluid density.
Here, Numerical Expression 2 is derived from Numerical Expression 1 as follows.
v2=v1*(S1/S2) (Numerical Expression 2)
where v1 is a fluid velocity in cross-sectional area S1, and v2 is a fluid velocity in cross-sectional area S2.
Numerical Expression 2 shows that the fluid velocity v2 increases as the cross-sectional area S2 decreases.
According to this, by providing the limiting plate 4 for limiting wind toward the fin 7 on a tip side of the fin 1b to limit a flow passage area at an inlet in the fin tip part where the fin efficiency is low, the cross-sectional area corresponding to S2 in the above Numerical Expression 2 becomes decreased.
As a result, the wind velocity is increased in the base surface 1a and in the portion of the fin 1b close to the base surface 1a which are not limited by the limiting plate 4 and have high cooling fin efficiency, and by increasing the quantity of wind flowing through these portions per unit time, the cooling can be promoted as compared to the prior art.
In connection with the above descried embodiment,
In
In
First, with regard to the circle part A, the wind flow from right becomes fast in the part along the base surface 1a of the cooling fin 1. This is confirmed by the result that the arrows in the simulation in
It can be seen that, by the wind flow from right in the figure toward the fan on the left in the circle part A, the cooling efficiency in a portion along the base surface 1a of the cooling fin 1 can be improved as compared to the prior art.
Next, also in the circle part B, the wind flow from right becomes fast. This is confirmed by the fact that the arrows are longer than those in the simulation in the case of not providing the limiting plate 4, as is in the circle part A.
It can be seen that, by the wind flow from right in the figure toward the fan on the left in the circle part B, the cooling efficiency in a middle portion of the cooling fin 1 can be improved as compared to the prior art.
On the other hand, in the circle part C, the wind direction changes in an irregular manner, rather than the wind flow from right in the figure toward the fan on the left. Therefore, it seems that the cooling efficiency becomes lower than that in the circle parts A and B.
In fact, it has been found also in simulation that a contribution ratio of the circle part C is lower than that of the circle parts A and B in terms of cooling of the cooling fin 1, even if the limiting plate 4 is not provided. Therefore, it is deemed that influence by providing the limiting plate 4 is small. Then,
As can be seen from the result in
Then, it can be understood from
It is expected from the result in
Although a large cooling efficiency is obtained at 80% in
Again, as already described in connection with the circle part C in
In addition, it can be said that implementation in the order of 30% to 60% is preferable in consideration of the above described deposition and clogging of foreign matters to the cooling fin, etc. In such a range, generation and magnitude of wind sound when sucking air or atmosphere on the sucking side of the cooling fin 1 can be reduced to an insignificant level.
It was also confirmed with an actual prototype that good cooling effect can be obtained at about 35% as compared to the prior art, and wind sound when sucking is insignificant, etc.
Next,
In
Further,
In
Providing the limiting plate 8 aims to cause change in wind flow in order to improve the cooling efficiency of the fin near the base surface 1a of the cooling fin 1. Here, change in wind flow means turbulent flow which is said as flow in which small parts of fluid are irregularly mixed to include turbulence, irregular flow or the like.
The above described limiting plate 4 may be provided by bending a part of a housing which supports the cooling fin 1 and the like. In this way, another step of attaching the limiting plate 4 or the like may be eliminated and it is also possible to achieve reduction in the number of parts.
Embodiments of the present invention are not limited to the above described embodiments and those may be modified as appropriate. For example, instead of providing the limiting plate 4 in a bended manner as in
It should be further understood by those skilled in the art that although the foregoing description has been made on embodiments of the invention, the invention is not limited thereto and various changes and modifications may be made without departing from the spirit of the invention and the scope of the appended claims.
Number | Date | Country | Kind |
---|---|---|---|
2006-150874 | May 2006 | JP | national |