Diffuser for centrifugal compressor and method of producing the same
At least the throat of the suction surface of a conventionally-used diffuser blade having a two-dimensional shape is cut into a concave shape with a ball end mill. In the throat, the nearer to the bottom of the concave shape, the higher the gas pressure becomes, and therefore the gas flows from the concave bottom toward the hub end and the shroud end thereby to reduce the thickness of the boundary layer formed on the hub end and the shroud end.
The present invention relates to a diffuser for a centrifugal compressor and a fabricating method and, in particular, to a diffuser for a centrifugal compressor and a fabricating method capable of reducing both the incidence loss.
BACKGROUND ARTA centrifugal compressor is well known as a type of compressor for compressing and increasing the pressure of a gas.
A blade 14 is mounted on the impeller 12, and the gas flowing in along the direction of arrow 15 is accelerated by the impeller 12 and flows out along the radial direction 16 of the centrifugal compressor. The diffuser portion on the outer periphery of the impeller 12 includes a diffuser blade 17 for converting the dynamic pressure of the fluid flowing out along the radial direction 16 into a static pressure. Specifically, the diffuser blade 17 is mounted on an annular disk 18 fitted in the front inner wall of the diffuser portion of the casing 13, and the diffuser blade 17 extends toward the rear inner wall (along the height) of the diffuser portion in the casing.
The gas flowing out of the impeller 12 flows into the diffuser portion in the direction of arrow 20. The angle between the velocity vector of the gas and an axis tangent to the circumference of the annular disk 18 is referred to as flow angle α. The distribution of the flow angle α along the height of the diffuser blade has a parabolic shape wherein the angle is substantially zero at one side where the diffuser blade 17 is mounted to the annular disk 18 (shroud end S) and at the other side rear the inner wall of the casing (hub end H), while the flow angle α is positive in the intermediate area therebetween.
The difference (α−αksuc) between the flow angle α and the suction surface blade angle αksuc is defined as an incidence In. The incidence In becomes negative near the hub end H and the shroud end S (hatched portions in
The present invention has been achieved in view of the problems described above, and the object thereof is to provide a diffuser for the centrifugal compressor and a fabrication method capable of reducing the pressure loss by suppressing the generation of the boundary layer at the suction surface near the hub end and the shroud end of each diffuser blade.
According to a first aspect of the invention, there is provided a diffuser for a centrifugal compressor comprising a diffuser blade including a suction surface which is concave toward a pressure surface in a cross section, perpendicular to the flow direction.
According to a second aspect of the invention, there is provided a diffuser for a centrifugal compressor comprising a diffuser blade including a suction surface which defines an acute angle, in a cross section perpendicular to the flow direction, in relation to at least one of a shroud surface and a hub surface.
According to a third aspect of the invention, there is provided a diffuser for a centrifugal compressor comprising a diffuser blade including a suction surface which is concave toward a pressure surface in a cross section, perpendicular to the flow direction at least in a throat portion and a portion upstream thereof.
According to a fourth aspect of the invention, there is provided a diffuser for a centrifugal compressor comprising a suction surface which defines an acute angle, in a cross section perpendicular to the flow direction at least in a throat portion and a portion upstream thereof, in relation to at least one of a shroud surface and a hub surface.
According the first to fourth aspects of the invention, the suction surface is formed into a concave surface at least in the throat portion to suppress the generation of a boundary layer near the shroud surface and the hub surface.
According to a fifth aspect of the invention, there is provided a method of fabricating a diffuser for a centrifugal compressor, comprising the steps of fabricating a two-dimensional blade; and cutting one of the side surfaces of the blade, fabricated in the preceding step, into a concave shape with a ball end mill.
In the fifth aspect of the invention, the diffuser blade is fabricated by cutting one side surface of the diffuser blade having a two-dimensional shape with a ball end mill.
BRIEF DESCRIPTION OF THE DRAWINGS
In
This indicates that the boundary layer thickness of the suction surface near the hub end H and the shroud end S of the diffuser blade 4 is reduced thereby leading to a smaller incidence loss than the conventional diffuser blade.
In the area downstream of the throat area where the first diffuser blade 41 and the second diffuser blade 42 overlap each other, the constant-pressure curves assume a form perpendicular to the center line along the length of the first diffuser blade 41 and the second diffuser blade 42. Therefore, the gas is prevented from flowing from the suction surface of the first diffuser blade 41 toward the pressure surface of the second diffuser blade 42. Thus, it is especially important to form a throat and a concave suction surface at upstream of the throat, while the portion downstream of the throat is not required to be formed into a concave shape.
Next, the suction surface of the two-dimensional diffuser blade is cut with the ball end mill thereby to form a concave suction surface. After cutting the two-dimensional diffuser blade along one end thereof (
The cutting depth of the ball end mill being constant, the steps of fabricating the diffuser blade according to this invention are simplified.
Normally, a two-dimensional diffuser blade has the greatest thickness at the longitudinally central portion thereof, and therefor the cross section of the diffuser blade according to the invention is symmetric longitudinally about the central portion (III) thereof. Specifically, the cross section of the central portion (III) is shaped as shown in
The embodiment of the invention described above refers to an application of the diffuser according to the invention to a centrifugal compressor. It is apparent, however, that the diffuser according to this invention is also applicable to a centrifugal blower and a centrifugal pump with equal effect.
With the diffuser for a centrifugal compressor according to this invention, the boundary layer generated on the suction surface near the shroud end and the hub end of the diffuser blade is reduced, whereby the incidence loss is reduced.
In the method of fabricating the diffuser for the centrifugal compressor according to this invention, the diffuser blade can be easily fabricated by cutting a two-dimensional diffuser blade with a ball end mill.
Claims
1. A diffuser for a centrifugal compressor comprising a diffuser blade including a suction surface which is concave toward a pressure surface in a cross section, perpendicular to the flow direction.
2. A diffuser for a centrifugal compressor comprising a diffuser blade including a concave suction surface which defines an acute angle, in a cross section perpendicular to the flow direction, in relation to at least one of a shroud surface and a hub surface.
3. A diffuser for a centrifugal compressor comprising a diffuser blade including a suction surface which is concave toward a pressure surface in a cross section, perpendicular to the flow direction at least in a throat portion or a portion upstream thereof.
4. A diffuser for a centrifugal compressor comprising a concave suction surface which defines an acute angle, in a cross section perpendicular to the flow direction at least in a throat portion or a portion upstream thereof, in relation to at least one of a shroud surface and a hub surface.
5. A method of fabricating a diffuser for a centrifugal compressor comprising the steps of fabricating a two-dimensional blade, and cutting one of the side surfaces of the blade, fabricated in the preceding step, into a concave shape with a ball-end mill.
Type: Application
Filed: Dec 4, 2003
Publication Date: Jul 28, 2005
Inventor: Hirotaka Higashimori (Nagasaki-shi)
Application Number: 10/503,220