Rotary machine, blade wheel used in rotary machine, and blade wheel manufacturing method

Abstract

A compressor of the present invention includes an impeller that is rotatably provided inside an accommodation portion of a compressor casing, the impeller includes a blade that extends toward an inner peripheral surface of the accommodation portion, and an outer edge of the blade facing the inner peripheral surface of the accommodation portion is provided with a shroud portion that is formed from a resin layer. With such a configuration, the wear damage of the casing and the blade of the blade wheel may be prevented, and the effort and the time in the manufacturing process may be reduced.

Claims

1. A rotary machine, comprising: a casing; and a blade wheel that is rotatably provided inside the casing such that the blade wheel is able to rotate relative to the casing, wherein the blade wheel includes: a blade that extends toward an inner peripheral surface of the casing and terminates at an edge that faces the inner peripheral surface of the casing and that is able to rotate relative to the inner peripheral surface of the casing; and a shroud portion provided in at least a part of the edge of the blade facing the inner peripheral surface of the casing, wherein a resin layer is provided only at the shroud portion and only at a portion of the outer edge of the blade facing the inner peripheral surface of the casing with a gap of a constant size, wherein the portion of the edge of the blade having the resin layer provided thereon has a shape following the inner peripheral surface of the casing.

2. The rotary machine according to claim 1, wherein the shroud portion is provided at the entire edge of the blade.

3. The rotary machine according to claim 1, wherein at least a part of the shroud portion contacts the inner peripheral surface of the casing.

4. The rotary machine according to claim 1, wherein the edge of the blade includes a radial facing portion that faces the inner peripheral surface of the casing in the radial direction of the blade wheel, and the radial facing portion is provided with the shroud portion.

5. The rotary machine according to claim 1, wherein the edge of the blade includes an axial facing portion that faces the inner peripheral surface of the casing in the axial direction of the blade wheel, and the axial facing portion is provided with the shroud portion.

6. A blade wheel that is used in the rotary machine according to claim 1.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a partially cross-sectional view illustrating a compressor according to an embodiment of the present invention.

(2) FIG. 2 is a partially enlarged view illustrating the vicinity of a compressor casing and a blade of an impeller of the compressor illustrated in FIG. 1.

(3) FIG. 3 is a perspective view illustrating the impeller used in the compressor according to the embodiment of the present invention.

(4) FIG. 4 is a flowchart illustrating an impeller processing procedure.

(5) FIG. 5 is a perspective view illustrating a base material that is used to manufacture the impeller.

(6) FIG. 6 is a perspective view illustrating a base material subjected to rough processing.

DESCRIPTION OF THE PREFERRED EMBODIMENTS

(7) Hereinafter, an embodiment of the present invention will be described with reference to the drawings.

(8) FIG. 1 is a partially cross-sectional view illustrating a compressor according to this embodiment. The compressor according to this embodiment is an example of the rotary machine of the present invention, and includes a drive mechanism 2, a compressor casing 4, a casing cover 6, an impeller 8, and a seal member 10.

(9) The drive mechanism 2 is used to rotate the impeller 8, and includes a low-speed shaft 12, bearings 14a and 14b, a motor (not illustrated), a gear casing 16, a low-speed gear 18, a high-speed shaft 20, bearings 22a and 22b, and a high-speed gear 23.

(10) The low-speed shaft 12 is rotatably supported by the gear casing 16 through the bearings 14a and 14b. A drive shaft of the motor (not illustrated) is connected to one end of the low-speed shaft 12.

(11) The low-speed gear 18 is fitted to the outside of the low-speed shaft 12 at the position between the bearings 14a and 14b, and is disposed inside the gear casing 16.

(12) The high-speed shaft 20 is disposed in parallel to the low-speed shaft 12 inside the gear casing 16. The high-speed shaft 20 is rotatably supported by the bearings 22a and 22b. The left end of the high-speed shaft 20 in FIG. 1 protrudes outward from the gear casing 16.

(13) The high-speed gear 23 is provided at the position between the bearings 22a and 22b in the high-speed shaft 20, and engages with the low-speed gear 18.

(14) The compressor casing 4 is attached to the left side portion of the gear casing 16 in FIG. 1 through the casing cover 6. In this embodiment, the compressor casing 4 corresponds to the casing of the present invention. The compressor casing 4 includes an accommodation portion 24 that accommodates the impeller 8 and a peripheral portion 26 that is disposed at the outer periphery of the accommodation portion 24 and is integrally formed with the accommodation portion 24.

(15) An inner space 24a in which the impeller 8 is disposed is provided inside the accommodation portion 24. Both ends of the inner space 24a of the high-speed shaft 20 in the axial direction are opened. Hereinafter, the axial direction simply indicates the axial direction of the high-speed shaft 20. Further, the radial direction about the high-speed shaft 20 simply indicates the radial direction. The casing cover 6 is fastened to the end of the compressor casing 4 near the gear casing 16, and covers the end of the inner space 24a near the gear casing 16. A through-hole 6a is formed at the center of the casing cover 6, and an end 200 of the high-speed shaft 20 is disposed inside the through-hole 6a. The seal member 10 which prevents the leakage of a gas from the inner space 24a is provided between the outer peripheral surface of the end 200 of the high-speed shaft 20 and the inner peripheral surface of the through-hole 6a. A gas introduction port 24b is formed by the end of the inner space 24a opposite to the casing cover 6.

(16) FIG. 2 is a partially enlarged view illustrating the vicinity of the compressor casing 4 and blades 30 of the impeller 8 of the compressor. As illustrated in FIG. 2, an inner peripheral surface 24c of the accommodation portion 24 forming the inner space 24a includes an inlet-side tapered surface 24d, an intermediate surface 24e, and an outlet-side tapered surface 24f.

(17) The inlet-side tapered surface 24d, the intermediate surface 24e, and the outlet-side tapered surface 24f are sequentially disposed from the introduction port 24b toward the casing cover 6. The inlet-side tapered surface 24d is formed in a tapered shape which decreases in diameter as it goes from the introduction port 24b toward the casing cover 6. The intermediate surface 24e is formed in a cylindrical shape that extends in the axial direction. The outlet-side tapered surface 24f is formed in a tapered shape which increases in diameter so as to perpendicularly approach the axial direction as it goes from the intermediate surface 24e toward the casing cover 6.

(18) The peripheral portion 26 includes an end surface 26a that extends from the outer edge of the outlet-side tapered surface 24f (the edge near the casing cover 6) outward in the radial direction. The end surface 26a is perpendicular to the axial direction, and is disposed with a gap between the end surface and the casing cover 6. A communication path 26b is formed by the gap between the end surface 26a and the casing cover 6. Further, the peripheral portion 26 is provided with a discharge port 26c which is connected to the communication path 26b and into which the compressed gas is discharged.

(19) As illustrated in FIG. 1, the impeller 8 is rotatably provided while being accommodated in the inner space 24a of the accommodation portion 24. The impeller 8 is an example of the blade wheel of the present invention. FIG. 3 is a perspective view of the impeller 8. The impeller 8 includes a hub 28 and the plurality of blades 30.

(20) As illustrated in FIG. 1, the hub 28 is coupled to the end 200 of the high-speed shaft 20 while being disposed so as to be coaxial with the high-speed shaft 20. The hub 28 includes an outer peripheral surface 28a (see FIG. 2) that is widened outward in the radial direction as it goes from an apex 280 toward the casing cover 6.

(21) As illustrated in FIG. 3, the plurality of blades 30 protrude from the outer peripheral surface 28a of the hub 28 toward the inner peripheral surface 24c of the accommodation portion 24, and are disposed with a gap therebetween in the circumferential direction of the hub 28 (the circumferential direction of the impeller 8). The plurality of blades 30 and the hub 28 are integrally formed with one another by a metal material. As illustrated in FIG. 2, the blade 30 is provided in an area facing the vicinity of the outlet-side tapered surface 24f of the intermediate surface 24e and the outlet-side tapered surface 24f. Each blade 30 includes a leading edge 30a that is located near the introduction port 24b and extends in a direction perpendicular to the axial direction, a trailing edge 30b that is located near the discharge port 26c and extends in a direction parallel to the axial direction, and an outer edge 30c that faces the inner peripheral surface 24c of the accommodation portion 24 and is formed in a shape following the inner peripheral surface 24c. In the outer edge 30c, a portion near the leading edge 30a faces the intermediate surface 24e of the accommodation portion 24 in the radial direction. Hereinafter, the portion near the leading edge 30a is referred to as a radial facing portion 30d. In the outer edge 30c, a portion near the trailing edge 30b faces the outlet-side tapered surface 24f of the accommodation portion 24 in the axial direction. Hereinafter, the portion near the trailing edge 30b is referred to as an axial facing portion 30e.

(22) A shroud portion 31b that is formed from a resin layer 31a is formed throughout the outer edge 30c. The resin layer 31a has a thickness of 1 mm to 10 mm. As the material of the resin layer 31a, for example, a resin such as PEEK (polyethelethelketon) which has wear resistance and is softer than the metal material forming the blade 30 and the compressor casing 4 is used. In a state where the impeller 8 is stopped, the resin layer 31a (shroud portion 31b) entirely contacts the inner peripheral surface 24c of the accommodation portion 24.

(23) In the compressor with the above-described configuration, in a case where a gas is compressed by the compressor, the low-speed shaft 12 (see FIG. 1) is rotated by the power generated from the motor (not illustrated), and the rotation of the low-speed shaft 12 is transmitted to the high-speed shaft 20 through the low-speed gear 18 and the high-speed gear 23. The high-speed shaft 20 and the impeller 8 rotate together, and the gas that is suctioned from the introduction port 24b to the inner space 24a of the accommodation portion 24 is compressed by the impeller 8. The compressed gas is discharged through the communication path 26b and the discharge port 26c.

(24) Next, a process of manufacturing the impeller 8 according to this embodiment will be described based on the flowchart illustrated in FIG. 4.

(25) First, a metallic columnar base material 50 (see FIG. 5) is subjected to rough processing (cutting), thereby forming a base material 50a having a circular truncated cone shape as illustrated in FIG. 6 (step S1).

(26) Next, a physical and chemical pre-treatment is performed to clean the base material 50a (step S2).

(27) Subsequently, a surface preparation is performed on the surface of the base material 50a using a surface preparation agent, thereby changing the state of the surface of the base material 50a so that a resin may easily adhere to the surface (step S3).

(28) Next, a resin is spray-coated on the tapered outer peripheral surface 50b (see FIG. 6) of the base material 50a (step S4). Subsequently, the base material 50a is baked at a high temperature in a kiln, thereby baking the resin layer (step S5). After the baking, the base material 50a is cooled (step S6). The process of step S4 to step S6 is an example of the resin layer formation process of the present invention.

(29) Next, it is checked whether the resin layer has a thickness in accordance with the specification (step S7). When the resin layer has a thickness in accordance with the specification, shaving processing is performed which shaves the impeller 8 (see FIG. 3) from the base material 50a (step S8). Meanwhile, when the resin layer does not have a thickness in accordance with the specification, the process after the spray-coating (step S4) is performed again. In the shaving processing, the plurality of blades 30 and the hub 28 are shaved by cutting a portion corresponding to the gap between the blades 30 in the base material 50a so that the resin layer formed on the outer peripheral surface 50b of the base material 50a forms the resin layer 31a of the shroud portion 31b. By the above-described processings, the impeller 8 is formed.

(30) In this embodiment, it is possible to prevent the contact of the blade 30 with respect to the inner peripheral surface 24c of the accommodation portion 24 even when the resin layer 31a of the shroud portion 31b contacts the inner peripheral surface 24c of the accommodation portion 24 during the rotation of the impeller 8. As a result, it is possible to prevent the wear damage of the blade 30. Further, since the resin layer 31a is softer than the metal material of the compressor casing 4, the wear damage of the accommodation portion 24 contacting the resin layer 31a may be also prevented. Further, since the resin layer 31a may be formed on the blade 30 of the impeller 8 that is smaller than the compressor casing 4 and is easily handled, the effort and the time in the manufacturing process may be reduced.

(31) Further, in this embodiment, since the shroud portion 31b contacts the inner peripheral surface 24c of the accommodation portion 24, the gas compression efficiency of the compressor may be improved.

(32) Since the resin layer 31a is formed in the radial facing portion 30d and the axial facing portion 30e of the outer edge 30c of the blade 30, the wear damage of the blade 30 and the accommodation portion 24 may be prevented even when the impeller 8 rotates while being deviated in position in any one of the radial direction and the axial direction.

(33) Since a so-called resin lining is performed in which a thick resin layer is formed on the entire outer peripheral surface 50b of the base material 50a, the resin layer 31a of the shroud portion 31b may be easily formed compared to the case where the resin layer is formed on the outer edge of the blade after the blade is formed.

(34) Furthermore, the embodiment disclosed herein is merely an example in every respect, and it should be considered that the embodiment does not limit the present invention. The scope of the present invention is illustrated in not the above-described embodiment but claims, and includes meanings equivalent to claims and all modifications within the scope.

(35) In the above-described embodiment, the compressor has been described as an example of the rotary machine of the present invention, but the present invention may be applied to another rotary machine other than the compressor. For example, the present invention may be applied to a turbine. In this case, a turbine runner that rotates by a steam pressure corresponds to the blade wheel of the present invention.

(36) The resin layer of the shroud portion does not need to be formed on the entire outer edge of the blade. For example, the resin layer may be formed on only the radial facing portion of the outer edge, only the axial facing portion, or only the radial facing portion and the axial facing portion.

(37) The resin layer of the shroud portion may be formed so that at least a part thereof contacts the inner peripheral surface of the accommodation portion, and the entire thereof does not need to essentially contact the inner peripheral surface of the accommodation portion. Further, the shroud portion may be separated from the inner peripheral surface of the accommodation portion during the rotation of the impeller. The blade 30 may be formed as a member separated from the hub 28.