US20200200184A1 - Centrifugal rotating machine - Google Patents
Centrifugal rotating machine Download PDFInfo
- Publication number
- US20200200184A1 US20200200184A1 US16/717,134 US201916717134A US2020200184A1 US 20200200184 A1 US20200200184 A1 US 20200200184A1 US 201916717134 A US201916717134 A US 201916717134A US 2020200184 A1 US2020200184 A1 US 2020200184A1
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- flow path
- peripheral surface
- impeller
- protrusion portion
- casing
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- 230000002093 peripheral effect Effects 0.000 claims abstract description 103
- 239000012530 fluid Substances 0.000 claims abstract description 69
- 238000011144 upstream manufacturing Methods 0.000 claims abstract description 18
- 230000007423 decrease Effects 0.000 claims description 6
- 230000005284 excitation Effects 0.000 description 14
- 230000004048 modification Effects 0.000 description 6
- 238000012986 modification Methods 0.000 description 6
- 238000006073 displacement reaction Methods 0.000 description 3
- 230000001595 contractor effect Effects 0.000 description 2
- 238000007792 addition Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
- F04D29/284—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
- F04D17/08—Centrifugal pumps
- F04D17/10—Centrifugal pumps for compressing or evacuating
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
- F04D17/08—Centrifugal pumps
- F04D17/10—Centrifugal pumps for compressing or evacuating
- F04D17/12—Multi-stage pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
- F04D17/08—Centrifugal pumps
- F04D17/10—Centrifugal pumps for compressing or evacuating
- F04D17/12—Multi-stage pumps
- F04D17/122—Multi-stage pumps the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/05—Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps
- F04D29/053—Shafts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/08—Sealings
- F04D29/16—Sealings between pressure and suction sides
- F04D29/161—Sealings between pressure and suction sides especially adapted for elastic fluid pumps
- F04D29/162—Sealings between pressure and suction sides especially adapted for elastic fluid pumps of a centrifugal flow wheel
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/44—Fluid-guiding means, e.g. diffusers
- F04D29/441—Fluid-guiding means, e.g. diffusers especially adapted for elastic fluid pumps
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
- F04D29/667—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps by influencing the flow pattern, e.g. suppression of turbulence
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
- F04D29/668—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps damping or preventing mechanical vibrations
Definitions
- the present invention relates to a centrifugal rotating machine.
- a centrifugal compressor has a rotating shaft which extends along an axis, an impeller which is provided on the rotating shaft, and a casing which covers the impeller from an outside.
- an impeller referred to as a closed impeller.
- the closed impeller has a disk-shaped disk centered on an axis, a plurality of blades which are provided on one surface of the disk, and a conical cover which covers the plurality of blades from one side.
- a clearance (outer flow path) is provided between an outer peripheral surface of the cover and an inner peripheral surface of the casing.
- a fluid flows through a flow path defined by the blades.
- the fluid is compressed and brought into a high pressure state while flowing through the flow path from an inlet side toward an outlet side of the flow path.
- the fluid having a pressure higher than that of the inlet side flows through the outlet side of the flow path, and thus, the fluid flows into the above-described outer flow path. Accordingly, in a case where lot of fluid flows into the outer flow path, compression efficiency of the centrifugal compressor decreases. Therefore, a technology is known in which a seal portion for preventing the flow of the fluid is provided on the inner peripheral surface of the casing.
- WO 2016/043090 discloses a configuration in which a seal fin is provided on the inlet side of the impeller in the inner peripheral surface of the casing as a specific example of the seal portion. By providing the seal fin, the fluid which flows into the outer flow path is reduced.
- the present invention is made to solve the above-described problems, and an object thereof is to provide a centrifugal rotating machine in which a vibration is further reduced.
- a centrifugal rotating machine including: a rotating shaft which extends along an axis; an impeller which is configured to pump a fluid flowing in from one side in an axial direction to an outside in a radial direction, the impeller including a disk fixed to the rotating shaft and a cover covering a blade provided on the disk; and a casing which accommodates the impeller, in which an impeller flow path through which the fluid is pumped is formed by an upstream surface of the disk in the axial direction and an inner peripheral surface of the cover, an outer flow path is formed by an outer peripheral surface of the cover and an inner peripheral surface of the casing facing the outer peripheral surface of the cover, the outer flow path is connected to the impeller flow path at an outlet of the impeller flow path, and a protrusion portion protruding from the inner peripheral surface of the casing is provided in the outer flow path.
- the fluid which has flowed into the outer flow path is guided by the protrusion portion provided on the inner peripheral surface of the casing. Therefore, even in a case where the fluid includes a swirl component (swirling flow component), the fluid is guided by the protrusion portion, and thus, the swirl component can be reduced.
- an excitation force (seal excitation force) in a direction orthogonal to a displacement direction acts on the impeller. This seal excitation force is continuously added, and thus, a swing-rotation vibration is generated in the rotating shaft and the impeller.
- the possibility of the above-described problems can be reduced.
- a plurality of the protrusion portions may be formed at intervals in a circumferential direction.
- the plurality of protrusion portions are formed at intervals in the circumferential direction. Therefore, the swirl component can be uniformly reduced over the entire area of the outer flow path in the circumferential direction. Thereby, the pressure distribution of the fluid in the outer flow path becomes uniform, and thus, vibrations generated in the impeller can be further effectively suppressed.
- the protrusion portion may be provided at a predetermined region on the inner peripheral surface of the casing.
- the protrusion portion may be provided at a position overlapping the outlet of the impeller flow path in a radial direction with respect to the axis.
- the protrusion portion is provided at the position overlapping the outlet of the impeller flow path in the radial direction. Therefore, the swirl component included in the fluid which has flowed into the outer flow path can be reduced immediately after the inflow.
- the present inventors performed a CFD analysis on the excitation force by the swirl component. As a result, it was found that the excitation force generated in the impeller cover was large. The excitation force generated in this cover is caused by the fluid flowing into the outer flow path. Accordingly, as described in the configuration, the protrusion portion is provided at the position overlapping the inlet of the outer flow path, that is, the outlet of the impeller flow path. Therefore, the swirl component is reduced, and the excitation force generated in the cover can be more positively reduced.
- the swirl component increases as it gets closer to the outlet of the impeller flow path. Therefore, the swirl component can be more effectively reduced. As a result, it is possible to further reduce a possibility of the impeller being displaced or excited due the influence of the swirl component. Further, as compared to a configuration in which the protrusion portion extends over the entire area of the outer flow path, only a necessary and sufficient amount of the swirl component is removed. Accordingly, it is also possible to avoid an increase in a frictional resistance between the cover outer peripheral surface of the impeller and the fluid due to an excessive reduction of the swirl component.
- the centrifugal rotating machine may further include a step which is provided on the outer peripheral surface of the cover and is an annual step centered on the axis in the outer flow path, in which the step may be provided radially outside the protrusion portion.
- the step is provided on the outer peripheral surface of the cover. Therefore, the fluid flowing out from the outlet of the impeller passes through a radially outer portion of the outer flow path. That is, more fluid flows along the inner peripheral surface of the casing where the protrusion portion is provided. As a result, more fluid is guided toward the protrusion portion provided on the inner peripheral surface of the casing. Thereby, the swirl component of the fluid which flows into the outer flow path can be more positively reduced.
- the protrusion portion may be provided over the entire area of the casing inner peripheral surface in the outer flow path.
- the protrusion portion is provided over the entire area of the outer flow path, the swirl component of the fluid which has flowed into the outer flow path can be further reduced.
- the protrusion portion is curved from one side toward the other side in a circumferential direction with respect to the axis as the protrusion portion goes outward in the radial direction.
- the swirl component which turns from the other side toward the one side in the circumferential direction (that is, toward front side in rotation direction of the impeller) is added to the fluid flowing into the outer flow path.
- the protrusion portion is curved from the one side toward the other side in the circumferential direction as the protrusion goes radially outward from the inlet side. That is, the protrusion portion is curved in a direction opposite to a turning direction of the swirl component. Therefore, the swirl component can be rectified in the opposite direction by the protrusion portion. As a result, it is possible to further reduce the possibility of the rotating shaft and the impeller being excited due to the influence of the swirl component.
- the protrusion portion may be twisted from one side toward the other side in a circumferential direction with respect to the axis with reference to the inner peripheral surface of the casing as the protrusion portion goes from the outlet side toward the inlet side.
- the protrusion portion since the twist of the protrusion portion is small on the outlet side, the protrusion portion has a large angle with respect to the inner peripheral surface of the casing. Therefore, the flow of the fluid including the swirl component which has flowed into the outer flow path from the outlet side (that is, upstream side of outer flow path of the impeller can be captured more efficiently. Thereby, the swirl component can be further reduced.
- the centrifugal rotating machine may further include a seal portion which is provided on a radially inner end portion of the outer flow path and seals leakage of the fluid between the inner peripheral surface of the casing and the outer peripheral surface of the cover.
- the protrusion portion since the twist of the protrusion portion is large on the inlet side (that is, downstream side of outer flow path) of the impeller, the protrusion portion has a small angle with respect to the inner peripheral surface of the casing. Therefore, the fluid guided by the protrusion portion flows around the inner peripheral surface of the casing. As a result, for example, in a case where the seal portion is provided on the upstream side of the casing inner peripheral surface, the fluid can flow more positively toward the seal portion itself rather than toward the clearance between the seal portion and the cover outer peripheral surface of the impeller.
- the flow into the seal portion on the inlet side of the impeller becomes a radially inward flow state (down flow) from the casing inner peripheral surface to the cover outer peripheral surface, and thus, a contraction effect in the seal portion increases. Thereby, a leak flow which passes through the seal portion can be further reduced.
- the protrusion portion may be twisted from a front side toward a rear side in a rotation direction of the impeller with reference to the inner peripheral surface of the casing as the protrusion portion goes inward in the radial direction.
- the protrusion portion is twisted toward a rear side (that is, side opposite to turning direction of swirl component included in flow in outer flow path) in a rotation direction of the impeller. Accordingly, it is possible to more effectively capture and reduce the swirl component.
- a circumferential dimension of the protrusion portion with respect to the axis gradually decreases as the protrusion portion is separated from the inner peripheral surface of the casing.
- the protrusion portion has a tapered shape such that a dimension thereof in a circumferential direction gradually decreases. Accordingly, for example, even in a case where the outer peripheral surface of the impeller comes into contact with the protrusion portion, a contact area between the protrusion portion and the outer peripheral surface can be suppressed to be small. As a result, it is possible to prevent the impeller from being damaged or from being vibrated.
- a centrifugal rotating machine including: a rotating shaft which extends along an axis; an impeller which is configured to pump a fluid flowing in from one side in an axial direction to an outside in a radial direction, the impeller including a disk fixed to the rotating shaft and a cover covering a blade provided on the disk; and a casing which accommodates the impeller, in which an impeller flow path through which the fluid is pumped is formed by an upstream surface of the disk in the axial direction and an inner peripheral surface of the cover, an outer flow path is formed by an outer peripheral surface of the cover and an inner peripheral surface of the casing facing the outer peripheral surface of the cover, the outer flow path is connected to the impeller flow path at an outlet of the impeller flow path, and a step which is an annual step centered on the axis is provided on the outer peripheral surface of the cover in the outer flow path.
- the step is provided on the outer peripheral surface of the cover, the gap between the outer peripheral surface of the cover and the inner peripheral surface of the casing can be reduced. That is, the amount of fluid flowing into the outer flow path can be limited. As a result, it is possible to reduce the excitation force to the impeller generated when a large amount of fluid flows into the outer flow path.
- the centrifugal rotating machine that is capable of further reducing vibrations.
- FIG. 1 is a cross-sectional view of a centrifugal compressor according to a first embodiment of the present invention.
- FIG. 2 is an enlarged cross-sectional view of a main portion of the centrifugal compressor according to the first embodiment of the present invention.
- FIG. 3 is an enlarged cross-sectional view of a main portion of a centrifugal compressor according to a second embodiment of the present invention.
- FIG. 4 is a perspective view of an impeller according to the second embodiment of the present invention.
- FIG. 5 is an enlarged cross-sectional view of a main portion of a centrifugal compressor according to a third embodiment of the present invention.
- FIG. 6 is a view when an impeller according to a third embodiment of the present invention is viewed in an axial direction.
- FIG. 7 is an enlarged sectional view of a main portion of a centrifugal compressor according to a fourth embodiment of the present invention.
- FIG. 8 is a view when an impeller according to a fourth embodiment of the present invention is viewed in the axial direction.
- FIG. 9 is an explanatory view showing a flow of a fluid in a seal portion according to the fourth embodiment of the present invention.
- FIG. 10 is a cross-sectional view showing a modified example of a protrusion portion according to each embodiment of the present invention.
- centrifugal compressor 100 (centrifugal rotating machine) according to a first embodiment of the present invention will be described with reference to the drawings.
- the centrifugal compressor 100 includes a rotating shaft 1 which rotates around an axis O, a casing 3 which covers a periphery of the rotating shaft 1 to form a flow path 2 , a plurality of stages of impeller 4 which are provided on the rotating shaft 1 , and protrusion portions 9 which are provided in the casing 3 .
- the casing 3 is formed in a cylindrical shape extending along the axis O.
- the rotating shaft 1 extends to penetrate an inside of the casing 3 along the axis O.
- a journal bearing 5 and a thrust bearing 6 are respectively provided on both end portions of the casing 3 in a direction of the axis O.
- the rotating shaft 1 is rotatably supported around the axis O by the journal bearing 5 and the thrust bearing 6 .
- An intake port 7 through which air serving as a working fluid G is taken in from the outside is provided on a first side (one side) of the rotating shaft 1 of the casing 3 in the direction of the axis O.
- an exhaust port 8 through the working fluid G compressed inside the casing 3 is exhausted is provided on a second side (other side) of the rotating shaft 1 of the casing 3 in the direction of the axis O.
- An internal space which communicates with the intake port 7 and the exhaust port 8 is formed inside the casing 3 .
- An inner diameter of the internal space repeatedly increases and decreases.
- the internal spaces accommodate a plurality of impellers 4 and form a portion of the flow path 2 .
- a side on which the intake port 7 is located in the flow path 2 is referred to as an upstream side
- a side on which the exhaust port 8 is located is referred to as a downstream side.
- a return vane 50 is provided on the downstream side of each impeller 4 on the flow path 2 .
- each impeller 4 includes a disk-shaped disk 41 centered on the axis O, a plurality of blades 42 which are provided on an upstream surface of the disk 41 , and a cover 43 which covers the plurality of blades 42 from the upstream side.
- an outer dimension of the disk in the radial direction is formed so as to gradually expand from the first side to the second side in the direction of the axis O, and thus, the disk 41 is formed in an approximately conical shape.
- a plurality of blades 42 are radially arranged radially outward about the axis O on a surface (disk upstream surface 41 A) facing the upstream side of both surfaces of the disk 41 in the direction of the axis O. More specifically, each blade is formed by a thin plate erected from the disk upstream surface 41 A toward the upstream side.
- the plurality of blades 42 is curved to be directed from one side from the other side in a circumferential direction with respect to the axis O.
- the disk back surface 41 B and the casing 3 (casing facing surface 3 B) are disposed with a gap in the direction of the axis O. This gap is formed along a direction perpendicular to the direction of the axis O.
- An upstream end edge of the blade 42 is covered with the cover 43 .
- the plurality of blades 42 are interposed between the cover 43 and the disk 41 in the direction of the axis O. Accordingly, a space is formed by the cover 43 , the disk 41 , and a pair of blades 42 adjacent to each other. This space forms an impeller flow path 21 which is a portion of the above-described flow path 2 .
- a radially inner end portion of the impeller flow path 21 is referred to as an inlet 21 A, and a radially outer end portion thereof is referred to as an outlet 21 B.
- An outer peripheral surface (cover outer peripheral surface 43 A) of the cover 43 extends radially outward toward the second side in the direction of the axis O, and thus, is formed in an approximately conical shape.
- the cover outer peripheral surface 43 A faces an inner peripheral surface (casing inner peripheral surface 3 A) of the casing 3 with a gap.
- the casing inner peripheral surface 3 A extends radially outward from the first side toward the second side in the direction of the axis O, following a shape of the cover outer peripheral surface 43 A.
- An outer flow path F is defined between the casing inner peripheral surface 3 A and the cover outer peripheral surface 43 A.
- An annular space centered on the axis O is formed radially inside the casing inner peripheral surface 3 A. This space is referred to as a cavity C.
- a seal portion S is provided on a first side (upstream side) of the cavity C in the direction of the axis O.
- the seal portion S is provided to seal leakage of a fluid between the casing 3 and the cover outer peripheral surface 43 A.
- the seal portion S has a plurality of seal fins S 1 and a base portion S 2 which supports the seal fins S 1 .
- a plurality of protrusion portions 9 for guiding the fluid flowing into the outer flow path F are provided in the outer flow path F.
- Each protrusion portion 9 protrudes from the casing inner peripheral surface 3 A toward the second side in the direction of the axis O and extends from the outlet side toward the inlet side.
- the plurality of protrusion portions 9 are arranged at intervals in a circumferential direction with respect to the axis O in the outer flow path F.
- Each protrusion portion 9 is formed in a plate shape which extends from the outlet side toward the inlet side.
- the protrusion portion 9 is provided at a position overlapping the outlet 21 B of the impeller 4 in the radial direction with respect to the axis O.
- the protrusion portion 9 when viewed in the direction of the axis O, the protrusion portion 9 is provided at a position overlapping the outlet 21 B of the impeller 4 . Moreover, in a cross-sectional view including the axis O, the protrusion portion 9 is formed in a rectangular shape.
- the centrifugal compressor 100 When the centrifugal compressor 100 is operated, first, the rotating shaft 1 is rotationally driven by a drive source such as an electric motor. As the rotating shaft 1 rotates, the impellers 4 rotate, and the working fluid G is introduced from the intake port 7 into the flow path 2 . The working fluid G introduced into the flow path 2 is sequentially compressed while passing through the impeller flow path 21 in each impeller 4 . The working fluid G that has been compressed and brought into a high pressure state is pumped to the outside via the exhaust port 8 .
- a drive source such as an electric motor
- the high pressure working fluid G may flow in from the outlet 21 B side of the impeller flow path 21 .
- a swirl component (swirling flow component) accompanying rotation of the impeller 4 is added to the fluid flowing through the outer flow path F.
- the swirl component turns in the same direction as a rotation direction of the impeller 4 . Due to an influence of this swirl component, an excitation force directed in a direction orthogonal to a displacement direction acts on impeller 4 .
- a swing-rotation vibration may occur in the rotating shaft 1 and the impeller 4 by continuously adding this excitation force.
- the working fluid G which has flowed into the outer flow path F is guided by the protrusion portion 9 provided on the inner peripheral surface (casing inner peripheral surface 3 A) of the casing 3 .
- the protrusion portion 9 extends from the outlet 21 B side of the impeller 4 toward the inlet 21 A side thereof in the outer flow path F. Therefore, even in a case where the working fluid G includes the swirl component, the working fluid G is guided by the protrusion portion 9 , and thus, the swirl component can be reduced. As a result, the possibility of the swing-rotation vibration occurring in the rotating shaft 1 and the impeller 4 can be reduced.
- the protrusion portion 9 is provided at the position overlapping the outlet 21 B of the impeller 4 in the radial direction. Accordingly, the swirl component included in the working fluid G which has flowed into the outer flow path F can be reduced immediately after the inflow. In particular, in the outer flow path F, the closer the outlet 21 B of the impeller flow path 21 is, the more the swirl component is. Therefore, the swirl component can be more effectively reduced by the above configuration. As a result, it is possible to further reduce the possibility of the impeller 4 being displaced or excited due to the influence of the swirl component.
- the plurality of protrusion portions 9 are formed at intervals in the circumferential direction. Accordingly, the swirl component can be uniformly reduced over the entire area of the outer flow path F in the circumferential direction. Thereby, a pressure distribution of the fluid in the outer flow path F becomes uniform, and thus, vibrations generated in the rotating shaft 1 and the impeller 4 can be further effectively suppressed.
- FIGS. 3 and 4 a second embodiment of the present invention will be described with reference to FIGS. 3 and 4 .
- the same reference numerals are assigned to the same configurations as those of the first embodiment, and detail descriptions thereof are omitted.
- a position of a protrusion portion 9 B is different from that in the first embodiment, and a step 10 is provided on the cover outer peripheral surface 43 A closer to the outlet 21 B side than the protrusion portion 9 B.
- FIG. 4 is a view showing a state where only the impeller 4 is extracted.
- a casing 3 is attached so as to cover an outside of the impeller 4 , and the outer flow path F is formed between the impeller 4 and the casing 3 .
- the rotating shaft 1 is attached to the impeller 4 so as to penetrate a center hole of the impeller 4 , and the impeller 4 rotates together with the rotating shaft 1 .
- the casing 3 is a case which covers the whole and is a member that does not rotate (stationary member). It is naturally necessary to form a gap between the casing 3 and the impeller 4 , and thus, the outer flow path F is necessarily formed.
- the step 10 protrudes from the cover outer peripheral surface 43 A toward the first side in the direction of the axis O.
- the step 10 has an annular shape centered on the axis O.
- the step 10 is arranged closer to the outlet 21 B side than the protrusion portion 9 B when viewed in a cross section perpendicular to the axis O.
- the protrusion portion 9 B and the step 10 are arranged with an interval. More specifically, when viewed from the direction in which the outer flow path F extends, the protrusion portion 9 B and step 10 overlap each other.
- a cross section of step 10 is rectangular.
- a cross-sectional shape of step 10 may be a triangle or a trapezoid in addition to a rectangle.
- the step 10 is provided on the cover outer peripheral surface 43 A of the impeller 4 . Therefore, the working fluid G (broken line in FIG. 3 ) flowing out from the outlet 21 B of the impeller flow path 21 is obstructed by the step 10 , and thus, the working fluid G passes through a radially outer portion of the outer flow path F. That is, more fluid flows along the casing inner peripheral surface 3 A where the protrusion portion 9 B is provided. As a result, more fluid is guided toward the protrusion portion 9 B. Thereby, the swirl component of the working fluid G which flows into the outer flow path F can be more positively reduced. Therefore, the possibility of vibrations occurring in the rotating shaft 1 and the impeller 4 can be further reduced.
- the second embodiment of the present invention is described.
- various changes and modifications can be made to the configuration without departing from the gist of the present invention.
- the configuration in which the protrusion portion 9 B and the step 10 are provided is described.
- the protrusion portion 9 B may not necessarily be provided, and a configuration in which only the step 10 is provided on the cover outer peripheral surface 43 A of the impeller 4 may be adopted.
- the gap between the cover outer peripheral surface 43 A and the casing inner peripheral surface 3 A can be reduced. That is, the amount of working fluid G flowing into the outer flow path F can be limited. As a result, it is possible to reduce the excitation force to the impeller 4 generated when a large amount of working fluid G flows into the outer flow path F.
- a shape of a protrusion portion 9 C is different from those of the embodiments.
- the protrusion portion 9 C extends over the entire area from the outlet 21 B to the inlet 21 A of the impeller flow path 21 in the outer flow path F. More specifically, the protrusion portion 9 C extends from the outlet 21 B of the impeller flow path 21 to an end portion on the second side of the cavity C in the direction of the axis O.
- the protrusion height (protrusion dimension from the casing inner peripheral surface 3 A) of the protrusion portion 9 C is constant over the entire area in the extension direction of the protrusion portion 9 C. Furthermore, as shown in FIG. 6 , the protrusion portion 9 C is curved from a first side toward a second side in a circumferential direction with respect to the axis O as the protrusion portion 9 C goes from the inlet 21 A side toward the outlet 21 B side. In other words, the protrusion portion 9 C is curved in a curved shape which is convex toward a front side in the rotation direction of the impeller 4 . Further, the protrusion portion 9 C extends in a direction intersecting a radial direction with respect to the axis O (broken line in FIG. 6 ).
- the protrusion portion 9 C is provided over the entire area of the outer flow path F, the swirl component of the working fluid G which has flowed into the outer flow path F can be further reduced. As a result, the possibility that vibrations occur in the rotating shaft 1 and the impeller 4 can be further reduced.
- a swirl component which turns from the second side toward the first side in the circumferential direction (that is, toward front side in rotation direction of the impeller) is added to the fluid flowing into the outer flow path F.
- the protrusion portion 9 C is curved from the first side toward the second side in the circumferential direction as the protrusion portion 9 C goes from the inlet side toward the outlet 21 B. That is, the protrusion portion 9 C is curved in a direction opposite to a turning direction of the swirl component. Therefore, the swirl component can be rectified in the opposite direction by the protrusion portion 9 C. As a result, it is possible to further reduce the possibility of the impeller 4 being displaced or excited due to the influence of the swirl component.
- a shape of a protrusion portion 9 D is different from that of each of the embodiments.
- the protrusion portion 9 D is twisted from a first side toward a second side in a circumferential direction with respect to axis O with reference to an end edge 91 on the casing inner peripheral surface 3 A side as the protrusion portion 9 D goes from the outlet 21 B side to the inlet 21 A side.
- an end edge 92 on a side opposite to the end edge 91 is curved from the first side toward the second side along an arc centered on the end edge 91 as the end edge 92 goes from the outlet 21 B side toward the inlet 21 A side.
- the end edge 92 is twisted from a front side toward a rear side (that is, side opposite to turning direction of swirl component included in flow in outer flow path) in a rotation direction R of the impeller 4 as the end edge 92 goes from the outlet 21 B side toward the inlet 21 A side. Therefore, the angle formed between the protrusion portion 9 D and the casing inner peripheral surface 3 A is larger as the angle is closer to the outlet 21 B side, and is smaller as the angle is closer to the inlet 21 A side.
- the protrusion portion 9 D since the twist of the protrusion portion 9 D is small on the outlet 21 B side, the protrusion portion 9 D has a large angle with respect to the casing inner peripheral surface 3 A. Therefore, the flow of the working fluid G including the swirl component which has flowed into the outer flow path F from the outlet 21 B side (that is, upstream side of outer flow path F) can be captured more efficiently. Thereby, the swirl component can be further reduced. Further, since the twist of the protrusion portion 9 D is large on the inlet 21 A side (that is, downstream side of outer flow path F), the protrusion portion 9 D has a small angle with respect to the casing inner peripheral surface 3 A.
- the fluid guided by the protrusion portion 9 D flows in a region biased in the vicinity of the casing inner peripheral surface 3 A.
- the flow into the seal fin S 1 on the inlet 21 A side of the impeller 4 becomes a radially inward flow state (down flow) from the casing inner peripheral surface 3 A to the cover outer peripheral surface 43 A, and thus, a contraction effect in the seal fin S 1 increases. Therefore, the working fluid G can flow more positively toward the seal fin S 1 itself rather than toward a clearance V 1 between the seal fin S 1 provided on the upstream side of the casing inner peripheral surface 3 A and the impeller 4 (cover outer peripheral surface 43 A) (refer to FIG. 9 ).
- an apparent clearance V 2 of the seal fin S 1 can be made smaller than the actual clearance V 1 . Thereby, a leak flow which passes through the seal fin S 1 can be further reduced.
- the fourth embodiment of the present invention is described.
- various changes and modifications can be made to the configuration without departing from the gist of the present invention.
- a configuration as shown in FIG. 10 can be adopted.
- the protrusion portion 9 ( 9 B, 9 C, 9 D) has a tapered shape such that a dimension thereof in a circumferential direction gradually decreases as the protrusion portion is separated radially inward from the casing inner peripheral surface 3 A.
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Abstract
Description
- The present invention relates to a centrifugal rotating machine.
- Priority is claimed on Japanese Patent Application No. 2018-241697, filed on Dec. 25, 2018, the content of which is incorporated herein by reference.
- In general, a centrifugal compressor has a rotating shaft which extends along an axis, an impeller which is provided on the rotating shaft, and a casing which covers the impeller from an outside. Among these, in the impeller, there is an impeller referred to as a closed impeller. The closed impeller has a disk-shaped disk centered on an axis, a plurality of blades which are provided on one surface of the disk, and a conical cover which covers the plurality of blades from one side. A clearance (outer flow path) is provided between an outer peripheral surface of the cover and an inner peripheral surface of the casing.
- If the centrifugal compressor is operated, a fluid flows through a flow path defined by the blades. The fluid is compressed and brought into a high pressure state while flowing through the flow path from an inlet side toward an outlet side of the flow path. Here, the fluid having a pressure higher than that of the inlet side flows through the outlet side of the flow path, and thus, the fluid flows into the above-described outer flow path. Accordingly, in a case where lot of fluid flows into the outer flow path, compression efficiency of the centrifugal compressor decreases. Therefore, a technology is known in which a seal portion for preventing the flow of the fluid is provided on the inner peripheral surface of the casing. For example, PCT International Publication No. WO 2016/043090 discloses a configuration in which a seal fin is provided on the inlet side of the impeller in the inner peripheral surface of the casing as a specific example of the seal portion. By providing the seal fin, the fluid which flows into the outer flow path is reduced.
- In the centrifugal compressor having the above configuration, if a rotor including the impeller is displaced in a radial direction in a state where the fluid leaks between the seal fin and the outer peripheral surface of the cover, a circumferential pressure distribution is generated on a rotor surface. Here, a swirl component (swirling flow component) according to the rotation of the impeller is added to the fluid flowing through the outer flow path. Due to influences of this swirl component, an excitation force (seal excitation force) in a direction orthogonal to the displacement direction acts on the impeller. This seal excitation force is continuously applied, and thus, a swing-rotation vibration is generated in the rotor. That is, the centrifugal compressor described in PCT International Publication No. WO 2016/043090 still has a room for improvement.
- The present invention is made to solve the above-described problems, and an object thereof is to provide a centrifugal rotating machine in which a vibration is further reduced.
- According to an aspect of the present invention, there is provided a centrifugal rotating machine including: a rotating shaft which extends along an axis; an impeller which is configured to pump a fluid flowing in from one side in an axial direction to an outside in a radial direction, the impeller including a disk fixed to the rotating shaft and a cover covering a blade provided on the disk; and a casing which accommodates the impeller, in which an impeller flow path through which the fluid is pumped is formed by an upstream surface of the disk in the axial direction and an inner peripheral surface of the cover, an outer flow path is formed by an outer peripheral surface of the cover and an inner peripheral surface of the casing facing the outer peripheral surface of the cover, the outer flow path is connected to the impeller flow path at an outlet of the impeller flow path, and a protrusion portion protruding from the inner peripheral surface of the casing is provided in the outer flow path.
- According to the configuration, the fluid which has flowed into the outer flow path is guided by the protrusion portion provided on the inner peripheral surface of the casing. Therefore, even in a case where the fluid includes a swirl component (swirling flow component), the fluid is guided by the protrusion portion, and thus, the swirl component can be reduced. Here, in a case where the fluid including the swirl component flows into the outer flow path, an excitation force (seal excitation force) in a direction orthogonal to a displacement direction acts on the impeller. This seal excitation force is continuously added, and thus, a swing-rotation vibration is generated in the rotating shaft and the impeller. However, according to the configuration, the possibility of the above-described problems can be reduced.
- In the centrifugal rotating machine, a plurality of the protrusion portions may be formed at intervals in a circumferential direction.
- According to the above configuration, the plurality of protrusion portions are formed at intervals in the circumferential direction. Therefore, the swirl component can be uniformly reduced over the entire area of the outer flow path in the circumferential direction. Thereby, the pressure distribution of the fluid in the outer flow path becomes uniform, and thus, vibrations generated in the impeller can be further effectively suppressed.
- In the centrifugal rotating machine, the protrusion portion may be provided at a predetermined region on the inner peripheral surface of the casing.
- In the centrifugal rotating machine, the protrusion portion may be provided at a position overlapping the outlet of the impeller flow path in a radial direction with respect to the axis.
- According to the configuration, the protrusion portion is provided at the position overlapping the outlet of the impeller flow path in the radial direction. Therefore, the swirl component included in the fluid which has flowed into the outer flow path can be reduced immediately after the inflow. Here, the present inventors performed a CFD analysis on the excitation force by the swirl component. As a result, it was found that the excitation force generated in the impeller cover was large. The excitation force generated in this cover is caused by the fluid flowing into the outer flow path. Accordingly, as described in the configuration, the protrusion portion is provided at the position overlapping the inlet of the outer flow path, that is, the outlet of the impeller flow path. Therefore, the swirl component is reduced, and the excitation force generated in the cover can be more positively reduced. In addition, the swirl component increases as it gets closer to the outlet of the impeller flow path. Therefore, the swirl component can be more effectively reduced. As a result, it is possible to further reduce a possibility of the impeller being displaced or excited due the influence of the swirl component. Further, as compared to a configuration in which the protrusion portion extends over the entire area of the outer flow path, only a necessary and sufficient amount of the swirl component is removed. Accordingly, it is also possible to avoid an increase in a frictional resistance between the cover outer peripheral surface of the impeller and the fluid due to an excessive reduction of the swirl component.
- The centrifugal rotating machine may further include a step which is provided on the outer peripheral surface of the cover and is an annual step centered on the axis in the outer flow path, in which the step may be provided radially outside the protrusion portion.
- According to the above configuration, the step is provided on the outer peripheral surface of the cover. Therefore, the fluid flowing out from the outlet of the impeller passes through a radially outer portion of the outer flow path. That is, more fluid flows along the inner peripheral surface of the casing where the protrusion portion is provided. As a result, more fluid is guided toward the protrusion portion provided on the inner peripheral surface of the casing. Thereby, the swirl component of the fluid which flows into the outer flow path can be more positively reduced.
- In the centrifugal rotating machine, the protrusion portion may be provided over the entire area of the casing inner peripheral surface in the outer flow path.
- According to the configuration, since the protrusion portion is provided over the entire area of the outer flow path, the swirl component of the fluid which has flowed into the outer flow path can be further reduced.
- In the centrifugal rotating machine, the protrusion portion is curved from one side toward the other side in a circumferential direction with respect to the axis as the protrusion portion goes outward in the radial direction.
- Here, the swirl component which turns from the other side toward the one side in the circumferential direction (that is, toward front side in rotation direction of the impeller) is added to the fluid flowing into the outer flow path. According to the above configuration, the protrusion portion is curved from the one side toward the other side in the circumferential direction as the protrusion goes radially outward from the inlet side. That is, the protrusion portion is curved in a direction opposite to a turning direction of the swirl component. Therefore, the swirl component can be rectified in the opposite direction by the protrusion portion. As a result, it is possible to further reduce the possibility of the rotating shaft and the impeller being excited due to the influence of the swirl component.
- In the centrifugal rotating machine, the protrusion portion may be twisted from one side toward the other side in a circumferential direction with respect to the axis with reference to the inner peripheral surface of the casing as the protrusion portion goes from the outlet side toward the inlet side.
- According to the above configuration, since the twist of the protrusion portion is small on the outlet side, the protrusion portion has a large angle with respect to the inner peripheral surface of the casing. Therefore, the flow of the fluid including the swirl component which has flowed into the outer flow path from the outlet side (that is, upstream side of outer flow path of the impeller can be captured more efficiently. Thereby, the swirl component can be further reduced.
- The centrifugal rotating machine may further include a seal portion which is provided on a radially inner end portion of the outer flow path and seals leakage of the fluid between the inner peripheral surface of the casing and the outer peripheral surface of the cover.
- According to the above configuration, since the twist of the protrusion portion is large on the inlet side (that is, downstream side of outer flow path) of the impeller, the protrusion portion has a small angle with respect to the inner peripheral surface of the casing. Therefore, the fluid guided by the protrusion portion flows around the inner peripheral surface of the casing. As a result, for example, in a case where the seal portion is provided on the upstream side of the casing inner peripheral surface, the fluid can flow more positively toward the seal portion itself rather than toward the clearance between the seal portion and the cover outer peripheral surface of the impeller. That is, the flow into the seal portion on the inlet side of the impeller becomes a radially inward flow state (down flow) from the casing inner peripheral surface to the cover outer peripheral surface, and thus, a contraction effect in the seal portion increases. Thereby, a leak flow which passes through the seal portion can be further reduced.
- In the centrifugal rotating machine, the protrusion portion may be twisted from a front side toward a rear side in a rotation direction of the impeller with reference to the inner peripheral surface of the casing as the protrusion portion goes inward in the radial direction.
- According to the above configuration, the protrusion portion is twisted toward a rear side (that is, side opposite to turning direction of swirl component included in flow in outer flow path) in a rotation direction of the impeller. Accordingly, it is possible to more effectively capture and reduce the swirl component.
- In the centrifugal rotating machine, a circumferential dimension of the protrusion portion with respect to the axis gradually decreases as the protrusion portion is separated from the inner peripheral surface of the casing.
- According to the above configuration, the protrusion portion has a tapered shape such that a dimension thereof in a circumferential direction gradually decreases. Accordingly, for example, even in a case where the outer peripheral surface of the impeller comes into contact with the protrusion portion, a contact area between the protrusion portion and the outer peripheral surface can be suppressed to be small. As a result, it is possible to prevent the impeller from being damaged or from being vibrated.
- According to another aspect of the present invention, there is provided a centrifugal rotating machine including: a rotating shaft which extends along an axis; an impeller which is configured to pump a fluid flowing in from one side in an axial direction to an outside in a radial direction, the impeller including a disk fixed to the rotating shaft and a cover covering a blade provided on the disk; and a casing which accommodates the impeller, in which an impeller flow path through which the fluid is pumped is formed by an upstream surface of the disk in the axial direction and an inner peripheral surface of the cover, an outer flow path is formed by an outer peripheral surface of the cover and an inner peripheral surface of the casing facing the outer peripheral surface of the cover, the outer flow path is connected to the impeller flow path at an outlet of the impeller flow path, and a step which is an annual step centered on the axis is provided on the outer peripheral surface of the cover in the outer flow path.
- According to the above configuration, since the step is provided on the outer peripheral surface of the cover, the gap between the outer peripheral surface of the cover and the inner peripheral surface of the casing can be reduced. That is, the amount of fluid flowing into the outer flow path can be limited. As a result, it is possible to reduce the excitation force to the impeller generated when a large amount of fluid flows into the outer flow path.
- According to the present invention, it is possible to provide the centrifugal rotating machine that is capable of further reducing vibrations.
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FIG. 1 is a cross-sectional view of a centrifugal compressor according to a first embodiment of the present invention. -
FIG. 2 is an enlarged cross-sectional view of a main portion of the centrifugal compressor according to the first embodiment of the present invention. -
FIG. 3 is an enlarged cross-sectional view of a main portion of a centrifugal compressor according to a second embodiment of the present invention. -
FIG. 4 is a perspective view of an impeller according to the second embodiment of the present invention. -
FIG. 5 is an enlarged cross-sectional view of a main portion of a centrifugal compressor according to a third embodiment of the present invention. -
FIG. 6 is a view when an impeller according to a third embodiment of the present invention is viewed in an axial direction. -
FIG. 7 is an enlarged sectional view of a main portion of a centrifugal compressor according to a fourth embodiment of the present invention. -
FIG. 8 is a view when an impeller according to a fourth embodiment of the present invention is viewed in the axial direction. -
FIG. 9 is an explanatory view showing a flow of a fluid in a seal portion according to the fourth embodiment of the present invention. -
FIG. 10 is a cross-sectional view showing a modified example of a protrusion portion according to each embodiment of the present invention. - A centrifugal compressor 100 (centrifugal rotating machine) according to a first embodiment of the present invention will be described with reference to the drawings. As shown in
FIG. 1 , thecentrifugal compressor 100 includes arotating shaft 1 which rotates around an axis O, acasing 3 which covers a periphery of therotating shaft 1 to form aflow path 2, a plurality of stages ofimpeller 4 which are provided on therotating shaft 1, andprotrusion portions 9 which are provided in thecasing 3. - The
casing 3 is formed in a cylindrical shape extending along the axis O. Therotating shaft 1 extends to penetrate an inside of thecasing 3 along the axis O. Ajournal bearing 5 and athrust bearing 6 are respectively provided on both end portions of thecasing 3 in a direction of the axis O. Therotating shaft 1 is rotatably supported around the axis O by thejournal bearing 5 and thethrust bearing 6. - An
intake port 7 through which air serving as a working fluid G is taken in from the outside is provided on a first side (one side) of therotating shaft 1 of thecasing 3 in the direction of the axis O. In addition, anexhaust port 8 through the working fluid G compressed inside thecasing 3 is exhausted is provided on a second side (other side) of therotating shaft 1 of thecasing 3 in the direction of the axis O. - An internal space which communicates with the
intake port 7 and theexhaust port 8 is formed inside thecasing 3. An inner diameter of the internal space repeatedly increases and decreases. The internal spaces accommodate a plurality ofimpellers 4 and form a portion of theflow path 2. Moreover, in following descriptions, a side on which theintake port 7 is located in theflow path 2 is referred to as an upstream side, and a side on which theexhaust port 8 is located is referred to as a downstream side. Areturn vane 50 is provided on the downstream side of eachimpeller 4 on theflow path 2. - In the
rotating shaft 1, the plurality of (six) impellers are provided on an outer peripheral surface of therotating shaft 1 at intervals in the direction of the axis O. As shown inFIG. 2 , eachimpeller 4 includes a disk-shapeddisk 41 centered on the axis O, a plurality ofblades 42 which are provided on an upstream surface of thedisk 41, and acover 43 which covers the plurality ofblades 42 from the upstream side. - When viewed in a direction intersecting the axis O, an outer dimension of the disk in the radial direction is formed so as to gradually expand from the first side to the second side in the direction of the axis O, and thus, the
disk 41 is formed in an approximately conical shape. A plurality ofblades 42 are radially arranged radially outward about the axis O on a surface (diskupstream surface 41A) facing the upstream side of both surfaces of thedisk 41 in the direction of the axis O. More specifically, each blade is formed by a thin plate erected from the diskupstream surface 41A toward the upstream side. When viewed in the direction of the axis O, the plurality ofblades 42 is curved to be directed from one side from the other side in a circumferential direction with respect to the axis O. - A surface (disk back
surface 41B) facing the downstream side of both surfaces of thedisk 41 in the direction of the axis O expands radially outward with respect to the axis O from therotating shaft 1. The disk backsurface 41B and the casing 3 (casing facing surface 3B) are disposed with a gap in the direction of the axis O. This gap is formed along a direction perpendicular to the direction of the axis O. - An upstream end edge of the
blade 42 is covered with thecover 43. In other words, the plurality ofblades 42 are interposed between thecover 43 and thedisk 41 in the direction of the axis O. Accordingly, a space is formed by thecover 43, thedisk 41, and a pair ofblades 42 adjacent to each other. This space forms animpeller flow path 21 which is a portion of the above-describedflow path 2. Moreover, in the following descriptions, a radially inner end portion of theimpeller flow path 21 is referred to as aninlet 21A, and a radially outer end portion thereof is referred to as anoutlet 21B. An outer peripheral surface (cover outerperipheral surface 43A) of thecover 43 extends radially outward toward the second side in the direction of the axis O, and thus, is formed in an approximately conical shape. - The cover outer
peripheral surface 43A faces an inner peripheral surface (casing innerperipheral surface 3A) of thecasing 3 with a gap. The casing innerperipheral surface 3A extends radially outward from the first side toward the second side in the direction of the axis O, following a shape of the cover outerperipheral surface 43A. An outer flow path F is defined between the casing innerperipheral surface 3A and the cover outerperipheral surface 43A. In the following descriptions, an end portion side corresponding to a side of theoutlet 21B of the above-describedimpeller flow path 21 in an extension direction of the outer flow path F is simply referred to as an “outlet side”, and an end portion side corresponding to a side of theinlet 21A is simply referred to as an “inlet side”. - An annular space centered on the axis O is formed radially inside the casing inner
peripheral surface 3A. This space is referred to as a cavity C. A seal portion S is provided on a first side (upstream side) of the cavity C in the direction of the axis O. The seal portion S is provided to seal leakage of a fluid between thecasing 3 and the cover outerperipheral surface 43A. The seal portion S has a plurality of seal fins S1 and a base portion S2 which supports the seal fins S1. - A plurality of
protrusion portions 9 for guiding the fluid flowing into the outer flow path F are provided in the outer flow path F. Eachprotrusion portion 9 protrudes from the casing innerperipheral surface 3A toward the second side in the direction of the axis O and extends from the outlet side toward the inlet side. The plurality ofprotrusion portions 9 are arranged at intervals in a circumferential direction with respect to the axis O in the outer flow path F. Eachprotrusion portion 9 is formed in a plate shape which extends from the outlet side toward the inlet side. Moreover, in the present embodiment, theprotrusion portion 9 is provided at a position overlapping theoutlet 21B of theimpeller 4 in the radial direction with respect to the axis O. In other words, when viewed in the direction of the axis O, theprotrusion portion 9 is provided at a position overlapping theoutlet 21B of theimpeller 4. Moreover, in a cross-sectional view including the axis O, theprotrusion portion 9 is formed in a rectangular shape. - Next, an operation of the
centrifugal compressor 100 according to the present embodiment will be described. When thecentrifugal compressor 100 is operated, first, therotating shaft 1 is rotationally driven by a drive source such as an electric motor. As therotating shaft 1 rotates, theimpellers 4 rotate, and the working fluid G is introduced from theintake port 7 into theflow path 2. The working fluid G introduced into theflow path 2 is sequentially compressed while passing through theimpeller flow path 21 in eachimpeller 4. The working fluid G that has been compressed and brought into a high pressure state is pumped to the outside via theexhaust port 8. - Meanwhile, as indicated by a broken line arrow in
FIG. 2 , in the outer flow path F, the high pressure working fluid G may flow in from theoutlet 21B side of theimpeller flow path 21. A swirl component (swirling flow component) accompanying rotation of theimpeller 4 is added to the fluid flowing through the outer flow path F. The swirl component turns in the same direction as a rotation direction of theimpeller 4. Due to an influence of this swirl component, an excitation force directed in a direction orthogonal to a displacement direction acts onimpeller 4. A swing-rotation vibration may occur in therotating shaft 1 and theimpeller 4 by continuously adding this excitation force. - However, according to the above configuration, the working fluid G which has flowed into the outer flow path F is guided by the
protrusion portion 9 provided on the inner peripheral surface (casing innerperipheral surface 3A) of thecasing 3. Theprotrusion portion 9 extends from theoutlet 21B side of theimpeller 4 toward theinlet 21A side thereof in the outer flow path F. Therefore, even in a case where the working fluid G includes the swirl component, the working fluid G is guided by theprotrusion portion 9, and thus, the swirl component can be reduced. As a result, the possibility of the swing-rotation vibration occurring in therotating shaft 1 and theimpeller 4 can be reduced. - Furthermore, according to the above configuration, the
protrusion portion 9 is provided at the position overlapping theoutlet 21B of theimpeller 4 in the radial direction. Accordingly, the swirl component included in the working fluid G which has flowed into the outer flow path F can be reduced immediately after the inflow. In particular, in the outer flow path F, the closer theoutlet 21B of theimpeller flow path 21 is, the more the swirl component is. Therefore, the swirl component can be more effectively reduced by the above configuration. As a result, it is possible to further reduce the possibility of theimpeller 4 being displaced or excited due to the influence of the swirl component. - Further, as compared to a configuration in which the
protrusion portion 9 extends over the entire area of the outer flow path F, by providing theprotrusion portion 9 in a portion of the outer flow path F, only a necessary and sufficient amount of the swirl component is removed. Accordingly, it is also possible to avoid an increase in a frictional resistance between the cover outerperipheral surface 43A of theimpeller 4 and the working fluid G due to an excessive reduction of the swirl component. If the swirl component is excessively reduced, a flow velocity of the working fluid G flowing in the outer flow path F becomes too small. Therefore, the frictional resistance due to the working fluid G increases between the cover outerperipheral surface 43A of theimpeller 4 and the casing innerperipheral surface 3A, and a smooth rotation of theimpeller 4 may be hindered. According to the configuration, the possibility can be reduced. - Moreover, according to the configuration, the plurality of
protrusion portions 9 are formed at intervals in the circumferential direction. Accordingly, the swirl component can be uniformly reduced over the entire area of the outer flow path F in the circumferential direction. Thereby, a pressure distribution of the fluid in the outer flow path F becomes uniform, and thus, vibrations generated in therotating shaft 1 and theimpeller 4 can be further effectively suppressed. - Hereinbefore, the first embodiment of the present invention is described. In addition, various changes and modifications can be made to the configuration without departing from the gist of the present invention.
- Next, a second embodiment of the present invention will be described with reference to
FIGS. 3 and 4 . In addition, the same reference numerals are assigned to the same configurations as those of the first embodiment, and detail descriptions thereof are omitted. As shown inFIGS. 3 and 4 , in the present embodiment, a position of aprotrusion portion 9B is different from that in the first embodiment, and astep 10 is provided on the cover outerperipheral surface 43A closer to theoutlet 21B side than theprotrusion portion 9B.FIG. 4 is a view showing a state where only theimpeller 4 is extracted. In a centrifugal compressor according to the present embodiment, acasing 3 is attached so as to cover an outside of theimpeller 4, and the outer flow path F is formed between theimpeller 4 and thecasing 3. Therotating shaft 1 is attached to theimpeller 4 so as to penetrate a center hole of theimpeller 4, and theimpeller 4 rotates together with therotating shaft 1. Thecasing 3 is a case which covers the whole and is a member that does not rotate (stationary member). It is naturally necessary to form a gap between thecasing 3 and theimpeller 4, and thus, the outer flow path F is necessarily formed. - The
step 10 protrudes from the cover outerperipheral surface 43A toward the first side in the direction of the axis O. Thestep 10 has an annular shape centered on the axis O. In addition, thestep 10 is arranged closer to theoutlet 21B side than theprotrusion portion 9B when viewed in a cross section perpendicular to the axis O. Moreover, theprotrusion portion 9B and thestep 10 are arranged with an interval. More specifically, when viewed from the direction in which the outer flow path F extends, theprotrusion portion 9B and step 10 overlap each other. Further, a cross section ofstep 10 is rectangular. A cross-sectional shape ofstep 10 may be a triangle or a trapezoid in addition to a rectangle. - According to the configuration, the
step 10 is provided on the cover outerperipheral surface 43A of theimpeller 4. Therefore, the working fluid G (broken line inFIG. 3 ) flowing out from theoutlet 21B of theimpeller flow path 21 is obstructed by thestep 10, and thus, the working fluid G passes through a radially outer portion of the outer flow path F. That is, more fluid flows along the casing innerperipheral surface 3A where theprotrusion portion 9B is provided. As a result, more fluid is guided toward theprotrusion portion 9B. Thereby, the swirl component of the working fluid G which flows into the outer flow path F can be more positively reduced. Therefore, the possibility of vibrations occurring in therotating shaft 1 and theimpeller 4 can be further reduced. - Hereinbefore, the second embodiment of the present invention is described. In addition, various changes and modifications can be made to the configuration without departing from the gist of the present invention. For example, in the second embodiment, the configuration in which the
protrusion portion 9B and thestep 10 are provided is described. However, theprotrusion portion 9B may not necessarily be provided, and a configuration in which only thestep 10 is provided on the cover outerperipheral surface 43A of theimpeller 4 may be adopted. According to this configuration, since thestep 10 is provided on the cover outerperipheral surface 43A of theimpeller 4, the gap between the cover outerperipheral surface 43A and the casing innerperipheral surface 3A can be reduced. That is, the amount of working fluid G flowing into the outer flow path F can be limited. As a result, it is possible to reduce the excitation force to theimpeller 4 generated when a large amount of working fluid G flows into the outer flow path F. - Next, a third embodiment of the present invention will be described with reference to
FIGS. 5 and 6 . In addition, the same reference numerals are assigned to the same configurations as those of each of the embodiments, and detail descriptions thereof are omitted. As shown inFIG. 5 orFIG. 6 , in the present embodiment, a shape of aprotrusion portion 9C is different from those of the embodiments. Theprotrusion portion 9C extends over the entire area from theoutlet 21B to theinlet 21A of theimpeller flow path 21 in the outer flow path F. More specifically, theprotrusion portion 9C extends from theoutlet 21B of theimpeller flow path 21 to an end portion on the second side of the cavity C in the direction of the axis O. The protrusion height (protrusion dimension from the casing innerperipheral surface 3A) of theprotrusion portion 9C is constant over the entire area in the extension direction of theprotrusion portion 9C. Furthermore, as shown inFIG. 6 , theprotrusion portion 9C is curved from a first side toward a second side in a circumferential direction with respect to the axis O as theprotrusion portion 9C goes from theinlet 21A side toward theoutlet 21B side. In other words, theprotrusion portion 9C is curved in a curved shape which is convex toward a front side in the rotation direction of theimpeller 4. Further, theprotrusion portion 9C extends in a direction intersecting a radial direction with respect to the axis O (broken line inFIG. 6 ). - According to the above configuration, since the
protrusion portion 9C is provided over the entire area of the outer flow path F, the swirl component of the working fluid G which has flowed into the outer flow path F can be further reduced. As a result, the possibility that vibrations occur in therotating shaft 1 and theimpeller 4 can be further reduced. - Here, a swirl component which turns from the second side toward the first side in the circumferential direction (that is, toward front side in rotation direction of the impeller) is added to the fluid flowing into the outer flow path F. According to the configuration, the
protrusion portion 9C is curved from the first side toward the second side in the circumferential direction as theprotrusion portion 9C goes from the inlet side toward theoutlet 21B. That is, theprotrusion portion 9C is curved in a direction opposite to a turning direction of the swirl component. Therefore, the swirl component can be rectified in the opposite direction by theprotrusion portion 9C. As a result, it is possible to further reduce the possibility of theimpeller 4 being displaced or excited due to the influence of the swirl component. - Hereinbefore, the third embodiment of the present invention is described. In addition, various changes and modifications can be made to the configuration without departing from the gist of the present invention.
- Next, a fourth embodiment of the present invention will be described with reference to
FIGS. 7 to 9 . In addition, the same reference numerals are assigned to the same configurations as those of each of the embodiments, and detail descriptions thereof are omitted. As shown inFIGS. 7 and 8 , in the present embodiment, a shape of aprotrusion portion 9D is different from that of each of the embodiments. Theprotrusion portion 9D is twisted from a first side toward a second side in a circumferential direction with respect to axis O with reference to anend edge 91 on the casing innerperipheral surface 3A side as theprotrusion portion 9D goes from theoutlet 21B side to theinlet 21A side. More specifically, while theend edge 91 extends linearly along the casing innerperipheral surface 3A, anend edge 92 on a side opposite to theend edge 91 is curved from the first side toward the second side along an arc centered on theend edge 91 as theend edge 92 goes from theoutlet 21B side toward theinlet 21A side. In other words, as shown inFIG. 8 , theend edge 92 is twisted from a front side toward a rear side (that is, side opposite to turning direction of swirl component included in flow in outer flow path) in a rotation direction R of theimpeller 4 as theend edge 92 goes from theoutlet 21B side toward theinlet 21A side. Therefore, the angle formed between theprotrusion portion 9D and the casing innerperipheral surface 3A is larger as the angle is closer to theoutlet 21B side, and is smaller as the angle is closer to theinlet 21A side. - According to the configuration, since the twist of the
protrusion portion 9D is small on theoutlet 21B side, theprotrusion portion 9D has a large angle with respect to the casing innerperipheral surface 3A. Therefore, the flow of the working fluid G including the swirl component which has flowed into the outer flow path F from theoutlet 21B side (that is, upstream side of outer flow path F) can be captured more efficiently. Thereby, the swirl component can be further reduced. Further, since the twist of theprotrusion portion 9D is large on theinlet 21A side (that is, downstream side of outer flow path F), theprotrusion portion 9D has a small angle with respect to the casing innerperipheral surface 3A. Therefore, the fluid guided by theprotrusion portion 9D flows in a region biased in the vicinity of the casing innerperipheral surface 3A. As a result, the flow into the seal fin S1 on theinlet 21A side of theimpeller 4 becomes a radially inward flow state (down flow) from the casing innerperipheral surface 3A to the cover outerperipheral surface 43A, and thus, a contraction effect in the seal fin S1 increases. Therefore, the working fluid G can flow more positively toward the seal fin S1 itself rather than toward a clearance V1 between the seal fin S1 provided on the upstream side of the casing innerperipheral surface 3A and the impeller 4 (cover outerperipheral surface 43A) (refer toFIG. 9 ). In other words, an apparent clearance V2 of the seal fin S1 can be made smaller than the actual clearance V1. Thereby, a leak flow which passes through the seal fin S1 can be further reduced. - Hereinbefore, the fourth embodiment of the present invention is described. In addition, various changes and modifications can be made to the configuration without departing from the gist of the present invention. For example, as a modification common to the embodiments, a configuration as shown in
FIG. 10 can be adopted. In the example ofFIG. 10 , the protrusion portion 9 (9B, 9C, 9D) has a tapered shape such that a dimension thereof in a circumferential direction gradually decreases as the protrusion portion is separated radially inward from the casing innerperipheral surface 3A. According to this configuration, for example, even in a case where the outer peripheral surface of the impeller 4 (cover 43) comes into contact with the protrusion portion 9 (9B, 9C, 9D), a contact area between the protrusion portion 9 (9B, 9C, 9D) and the outer peripheral surface can be suppressed to be small. As a result, it is possible to prevent theimpeller 4 from being damaged or from being vibrated. - While preferred embodiments of the invention have been described and illustrated above, it should be understood that these are exemplary of the invention and are not to be considered as limiting. Additions, omissions, substitutions, and other modifications can be made without departing from the spirit or scope of the present invention. Accordingly, the invention is not to be considered as being limited by the foregoing description, and is only limited by the scope of the appended claims.
Claims (12)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2018-241697 | 2018-12-25 | ||
| JP2018241697A JP7168441B2 (en) | 2018-12-25 | 2018-12-25 | centrifugal rotating machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20200200184A1 true US20200200184A1 (en) | 2020-06-25 |
Family
ID=71097394
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US16/717,134 Abandoned US20200200184A1 (en) | 2018-12-25 | 2019-12-17 | Centrifugal rotating machine |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US20200200184A1 (en) |
| JP (1) | JP7168441B2 (en) |
| CN (1) | CN111379744B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111946662A (en) * | 2020-08-25 | 2020-11-17 | 绍兴市上虞区兴荣风机有限公司 | Centrifugal impeller and fan |
| US20210330146A1 (en) * | 2020-04-27 | 2021-10-28 | Samsung Electronics Co., Ltd. | Motor assembly and a cleaner comprising the same |
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| US2471174A (en) * | 1947-04-24 | 1949-05-24 | Clark Bros Co Inc | Centrifugal compressor stability means |
| US5228832A (en) * | 1990-03-14 | 1993-07-20 | Hitachi, Ltd. | Mixed flow compressor |
| JPH04159497A (en) * | 1990-10-19 | 1992-06-02 | Hitachi Ltd | Fluid machine |
| JPH064398U (en) * | 1992-06-19 | 1994-01-21 | 三菱重工業株式会社 | Centrifugal compressor |
| TW431562U (en) * | 2000-02-02 | 2001-04-21 | Ind Tech Res Inst | Floating type vane wheel structure for multi-stage type pressing pump |
| JP2006057487A (en) | 2004-08-18 | 2006-03-02 | Mitsubishi Heavy Ind Ltd | Centrifugal compressor |
| US7731476B2 (en) | 2007-01-30 | 2010-06-08 | Technology Commercialization Corp. | Method and device for reducing axial thrust and radial oscillations and rotary machines using same |
| JP2010025000A (en) | 2008-07-22 | 2010-02-04 | Hitachi Plant Technologies Ltd | Centrifugal fluid machine |
| JP2012007592A (en) | 2010-06-28 | 2012-01-12 | Mitsubishi Heavy Ind Ltd | Seal device, and fluid machine provided with the same |
| JP5769978B2 (en) | 2011-01-27 | 2015-08-26 | ミネベア株式会社 | Centrifugal fan |
| WO2014077058A1 (en) | 2012-11-13 | 2014-05-22 | 三菱重工コンプレッサ株式会社 | Rotary machine |
| ITFI20130204A1 (en) * | 2013-09-03 | 2015-03-04 | Nuovo Pignone Srl | "FAN-COOLED ELECTRICAL MACHINE WITH AXIAL THRUST COMPENSATION" |
| JP6260481B2 (en) | 2013-10-21 | 2018-01-17 | 株式会社デンソー | Centrifugal blower |
| US10634157B2 (en) * | 2014-01-07 | 2020-04-28 | Nuovo Pignone Srl | Centrifugal compressor impeller with non-linear leading edge and associated design method |
| CN203783951U (en) * | 2014-01-08 | 2014-08-20 | 陈亚波 | Port ring sealing mechanism for centrifugal pump |
| JP2016148308A (en) * | 2015-02-13 | 2016-08-18 | 三菱重工業株式会社 | Centrifugal compressor and geared centrifugal compressor |
| CN105545810A (en) * | 2015-12-18 | 2016-05-04 | 清华大学 | Case of centrifugal compressor |
| CN105570186B (en) * | 2016-03-04 | 2019-01-08 | 浙江工业大学 | A kind of centrifugal pump of single stage type being able to achieve axial force self-balancing |
-
2018
- 2018-12-25 JP JP2018241697A patent/JP7168441B2/en active Active
-
2019
- 2019-12-17 US US16/717,134 patent/US20200200184A1/en not_active Abandoned
- 2019-12-20 CN CN201911326761.5A patent/CN111379744B/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20210330146A1 (en) * | 2020-04-27 | 2021-10-28 | Samsung Electronics Co., Ltd. | Motor assembly and a cleaner comprising the same |
| US12279739B2 (en) * | 2020-04-27 | 2025-04-22 | Samsung Electronics Co., Ltd. | Motor assembly and a cleaner comprising the same |
| CN111946662A (en) * | 2020-08-25 | 2020-11-17 | 绍兴市上虞区兴荣风机有限公司 | Centrifugal impeller and fan |
Also Published As
| Publication number | Publication date |
|---|---|
| JP7168441B2 (en) | 2022-11-09 |
| CN111379744A (en) | 2020-07-07 |
| JP2020101169A (en) | 2020-07-02 |
| CN111379744B (en) | 2022-03-29 |
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