WO2015132896A1 - 回転流体要素及び回転流体要素のアンバラス修正方法 - Google Patents
回転流体要素及び回転流体要素のアンバラス修正方法 Download PDFInfo
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- WO2015132896A1 WO2015132896A1 PCT/JP2014/055583 JP2014055583W WO2015132896A1 WO 2015132896 A1 WO2015132896 A1 WO 2015132896A1 JP 2014055583 W JP2014055583 W JP 2014055583W WO 2015132896 A1 WO2015132896 A1 WO 2015132896A1
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- Prior art keywords
- cutting
- fluid element
- region
- rotating fluid
- unbalance
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- 239000012530 fluid Substances 0.000 title claims abstract description 111
- 238000000034 method Methods 0.000 title claims abstract description 39
- 238000012937 correction Methods 0.000 claims abstract description 69
- 238000005520 cutting process Methods 0.000 claims description 274
- 230000002093 peripheral effect Effects 0.000 claims description 28
- 238000012217 deletion Methods 0.000 claims description 2
- 230000037430 deletion Effects 0.000 claims description 2
- 239000013598 vector Substances 0.000 description 16
- 238000010586 diagram Methods 0.000 description 3
- 238000005259 measurement Methods 0.000 description 3
- 238000003672 processing method Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 238000012951 Remeasurement Methods 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 239000010936 titanium Substances 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
- F04D29/66—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
- F04D29/662—Balancing of rotors
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/027—Arrangements for balancing
-
- 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
-
- 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
- F04D29/666—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps by means of rotor construction or layout, e.g. unequal distribution of blades or vanes
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/40—Application in turbochargers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/10—Manufacture by removing material
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/10—Manufacture by removing material
- F05D2230/14—Micromachining
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/32—Correcting- or balancing-weights or equivalent means for balancing rotating bodies, e.g. vehicle wheels
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M1/00—Testing static or dynamic balance of machines or structures
- G01M1/30—Compensating imbalance
- G01M1/34—Compensating imbalance by removing material from the body to be tested, e.g. from the tread of tyres
Definitions
- the present disclosure relates to a rotating fluid element including a plurality of blades extending in the centrifugal direction on the outer peripheral surface of the boss portion and disposed at intervals in the circumferential direction, and an unbalance correcting method for the rotating fluid element.
- Patent Document 1 proposes an unbalance correction processing method using a rotating fluid element (turbine wheel, compressor wheel) of a supercharger as an example of a rotating fluid element.
- a rotating fluid element turbine wheel, compressor wheel
- a plurality of cutting removal portions having a certain angle in the circumferential direction are set between blades that are removal target portions of a rotating fluid element (turbine wheel, compressor wheel), and the rotating fluid element is unloaded.
- An unbalance vector indicating the amount and direction of balance is measured and divided into divided vectors in a pair of cutting removal units located on both sides of the direction of the unbalance vector, and the unbalance amount corresponding to each divided vector corresponds to If the removal unit exceeds the maximum amount that can be removed by cutting, the division vector is subdivided into division vectors in a pair of cut removal units located on both sides of the orientation, and the subdivision is divided into an unbalance amount corresponding to each division vector. The corresponding cut-off portion is repeatedly removed until the corresponding cut-off portion is less than or equal to the maximum amount that can be cut off.
- the unbalance correction processing method described in this Patent Document 1 is based on the measured unbalance vector, at one location on the radially outer side of the cutting removal portion of the rotating body corresponding to the unbalance vector, or a divided vector. One portion (a plurality of locations as a whole) is processed on each radially outer side of a plurality of cutting removal portions having different corresponding rotating bodies.
- the correction of unbalance is generally cut and removed at the radially outer peripheral edge of the rotating fluid element.
- the first corrected position may be corrected again.
- a desired correction amount may not be obtained, and the correction accuracy is lowered.
- the re-correction is excessive, there is a risk that the strength of the blade provided adjacent to the cutting removal portion (between the blades) of the rotating body is lowered.
- At least some embodiments of the present invention provide a rotation in which the imbalance correction accuracy is high and the blade strength is not reduced even if the rotation fluid element is subjected to unbalance correction a plurality of times. It is an object of the present invention to provide a method for correcting imbalance of a fluid element and a rotating fluid element.
- the rotating fluid element A plurality of blades extending in the centrifugal direction on the outer peripheral surface of the boss portion and arranged at intervals in the circumferential direction, and a cutting removal portion for reducing unbalance between the blades adjacent in the circumferential direction.
- the cutting and removing part is A first cut and removed portion cut and removed at a radially outer peripheral portion between the blades; And one or more additional cutting removal portions cut and removed in a radially inner portion than the first cutting removal portion (74c1).
- the cutting removal portion of the rotating fluid element includes a first cutting removal portion cut and removed at a radially outer peripheral portion between the blades, and an additional cutting cut and removed at a radially inner portion than the first cutting portion. Since the removal portion is included, the parts to be cut and removed to correct the imbalance are at different positions. For this reason, even if the imbalance correction is performed on the rotating fluid element a plurality of times, the imbalance correction accuracy can be increased and a rotating fluid element in which the blade strength is not reduced can be realized.
- the first cutting removal part is provided in an annular region located on the outermost radial direction among a plurality of annular regions having different radii that are concentric with the rotation center of the rotating fluid element,
- the additional cutting removal portion is provided in an annular region other than the annular region located on the outermost radial direction, Further, when there are a plurality of the additional cutting removal portions, each is configured to be provided in a different annular region.
- the first cutting removal unit is provided in an annular region located on the outermost radial direction among a plurality of annular regions having different radii that are concentric with the rotation center of the rotating fluid element, and the additional cutting removal unit is Since it is provided in an annular region other than the annular region located on the outermost radial direction, the first cutting removal part and the additional cutting removal part are in different positions. For this reason, even if the imbalance correction is performed on the rotating fluid element a plurality of times, the imbalance correction accuracy can be increased and a rotating fluid element in which the blade strength is not reduced can be realized.
- the first cutting and removing portion is provided in any one of a pair of phase regions located on one side in the radial direction and the other side in the radial direction with respect to the rotation center of the rotating fluid element and in mutually opposite phases,
- the additional cutting removal unit is configured to be provided in a phase region opposite to the phase region in which the first cutting removal unit is provided.
- the first cutting removal unit is provided in one of the pair of phase regions, and the additional cutting removal unit is provided in a phase region opposite to the phase region in which the first cutting removal unit is provided. Therefore, the first cutting removal part and the additional cutting removal part are in different positions. For this reason, even if the imbalance correction is performed on the rotating fluid element a plurality of times, the imbalance correction accuracy can be increased and a rotating fluid element in which the blade strength is not reduced can be realized.
- the additional cutting / removing portion is configured to continuously extend radially inward from the first cutting / removing portion between the blades provided with the first cutting / removing portion.
- the additional cutting removal portion is provided continuously extending radially inward from the first cutting removal portion between the blades provided with the first cutting removal portion, the unbalance amount is relatively small. If it is large, a large amount of unbalance can be removed at once by the second cutting operation. For this reason, the workability of the unbalance correction work can be improved.
- the additional cutting / removing portion is configured to extend from the first cutting / removing portion in a direction orthogonal to the centripetal direction of the rotating fluid element in the blades where the first cutting / removing portion is provided. Is done.
- the additional cutting removal portion is provided extending from the first cutting removal portion in a direction orthogonal to the centripetal direction of the rotating fluid element in the space between the blades provided with the first cutting removal portion,
- the balance amount is relatively large, a large unbalance amount can be removed at a stretch by the second cutting operation. For this reason, the workability of the unbalance correction work can be improved.
- a cutting removal section that includes a plurality of blades extending in the centrifugal direction on the outer peripheral surface of the boss portion and arranged at intervals in the circumferential direction, and reducing unbalance between the blades adjacent in the circumferential direction.
- An unbalance correction method for a rotating fluid element of A first step of setting a region including a radially outer peripheral portion between the reciprocal blades adjacent in the circumferential direction of the rotating fluid element, and a reciprocal region including a region located radially inward of the region; , A second step of determining the amount and position of the unbalance of the rotating fluid element; Based on the amount and position of the unbalance of the rotating fluid element obtained in the second step, a region including the radially outer peripheral portion is selected from the plurality of regions, and the cutting position of the selected region is A third step for determining the cutting amount; Based on the cutting position and the cutting amount obtained in the third step, a first cutting removal portion is provided by performing the first cutting removal at the cutting position with the cutting amount obtained in the third step.
- the fourth step A fifth step of determining the amount and position of the unbalance of the rotating fluid element that has undergone the first cutting removal; Based on the amount and position of the unbalance obtained in the fifth step, a region other than the selected region is selected from among the plurality of regions, and a cutting position and a cutting amount of the selected region are obtained. Based on the cutting position and cutting amount obtained in step 6 and step 6, a second cutting removal is performed at the cutting position with the cutting amount obtained in step 6 to provide an additional cutting removal unit. 7 steps.
- the unbalance correcting method for the rotating fluid element when the unbalance remains in the rotating fluid element that has been removed by the first cutting, the amount and position of the second unbalance are obtained. Then, based on the determined amount and position of the second unbalance, any region other than the region selected in the first time is selected, and the cutting position and amount of the selected region are determined. Then, the second cutting removal is performed based on the obtained cutting position and cutting amount. For this reason, since the position where the first cutting removal is performed is different from the position where the second cutting removal is performed, a desired cutting amount is obtained at the time of correcting the unbalance remaining after the first cutting removal. It can be modified. Therefore, it is possible to improve the imbalance correction accuracy of the rotating fluid element that can increase the accuracy of the unbalance correction and does not reduce the strength of the blade.
- From the fifth step to the seventh step It is configured to repeat until a predetermined unbalance amount is reached.
- the accuracy of unbalance correction can be further increased by repeating the fifth step to the seventh step until a predetermined unbalance amount is reached.
- the plurality of regions set in the first step are set as a plurality of annular regions having different radii that are concentric with the rotation center of the rotating fluid element
- the region selected in the third step is an annular region located on the outermost radial direction among the plurality of annular regions
- an annular region other than the annular region located on the outermost radial direction is selected based on the amount and position of the imbalance obtained in the fifth step. Configured.
- the plurality of regions set in the first step are set as a plurality of annular regions having different radii that are concentric with the rotation center of the rotating fluid element
- the region selected in the third step is a plurality of annular regions.
- the region selected in the sixth step is the annular region located on the outermost radial direction, and the region selected in the sixth step has the largest diameter based on the amount and position of the second unbalance obtained in the fifth step.
- An annular region other than the annular region located outside in the direction is selected. For this reason, since the second cutting removal is performed on the inner side in the radial direction of the rotating fluid element from the position where the first cutting removal is performed, both of the cutting removal positions can be different positions. For this reason, it is possible to process with a desired cutting amount at the time of correction processing of the unbalance remaining after the first cutting removal, and it is possible to improve the accuracy of the unbalance correction.
- an allowable cutting amount that can be removed by cutting is set,
- the region selected in the sixth step is configured to be any region that does not exceed the allowable cutting amount.
- an allowable cutting amount that can be cut and removed is set for each of the plurality of regions, and the region selected in the sixth step is any region that does not exceed the allowable cutting amount. It can be determined whether or not the obtained cutting amount exceeds the allowable cutting amount. For this reason, it is possible to easily determine the region selection.
- the cutting position obtained in the sixth step is configured to be a position on an imaginary line connecting the cutting position obtained in the third step and the rotation center of the rotating fluid element in the selected region.
- the cutting position obtained in the sixth step is a position on the imaginary line connecting the cutting position obtained in the third step and the rotation center of the rotating fluid element in the selected region. Therefore, when the rotating fluid element rotates, the vector of the centrifugal force corresponding to the unbalanced mass remaining after the first cutting removal and the vector of the centrifugal force at the second cutting position are aligned. Can do. Therefore, unbalance can be effectively reduced, and the accuracy of unbalance correction can be increased.
- a map in which a cutting amount with respect to an unbalance amount of the rotating fluid element is set for each of the plurality of regions is provided in advance,
- the cutting amount obtained in the sixth step is configured to be obtained based on the map in accordance with the unbalance amount obtained in the fifth step.
- a map in which the cutting amount with respect to the unbalance amount of the rotating fluid element is set for each of a plurality of regions is provided in advance, and the cutting amount obtained in the sixth step is equal to the unbalance amount obtained in the fifth step. Accordingly, since it is obtained based on the map, the cutting amount obtained in the sixth step is easily obtained via the map. For this reason, when calculating
- the plurality of regions set in the first step are set as a pair of phase regions arranged on the one side in the radial direction and the other side in the radial direction with respect to the center of rotation of the rotating fluid element and in mutually opposite phase positions.
- the region selected in the third step is any one of the phase regions including the radially outer peripheral portion of the pair of phase regions,
- the region selected in the sixth step is configured to be a phase region opposite to the phase region selected in the third step.
- one of the pair of phase regions including the radially outer peripheral portion is selected, and the region selected in the sixth step is Since the phase region is opposite to the phase region selected in the third step, the cutting position where the first cutting is removed and the position where the second cutting is removed are different positions. For this reason, it is possible to perform cutting with fine adjustment during the second correction process of the unbalance remaining at the first time, and the imbalance correction accuracy can be increased.
- the cutting amount determined in the third step is determined in the second step so that an unbalance amount smaller than the unbalance amount determined in the second step is generated in the opposite phase region.
- the amount of cutting is larger than the amount In the fourth step, based on the cutting amount obtained in the third step, the selected phase region is cut and removed, In the sixth step, the opposite phase region is cut and removed based on the amount and position of the unbalance obtained in the fifth step.
- the selected phase region is cut and removed based on the large cutting amount
- the phase on the opposite side is determined based on the unbalance amount and position obtained in the fifth step. Since the region is removed by cutting, it is possible to perform coarse correction in the first unbalance correction and perform high-precision correction in the second unbalance correction. For example, even when the cutting amount is less than or exceeds the desired cutting amount during the first correction processing, fine adjustment can be performed by the second correction. For this reason, the imbalance correction can be facilitated and the accuracy of the imbalance correction can be increased.
- An element imbalance correction method can be provided.
- FIG. 4A is a plan view of a rotating fluid element whose unbalance is corrected
- FIG. 4B is a cross-sectional view corresponding to the arrow II in FIG.
- FIG. 4A is a cross-sectional explanatory view of a turbocharger to which an unbalance correction method is applied
- FIG. 4B is a compressor in which a plurality of unbalance corrections are made in the radial direction of the compressor wheel of the turbocharger. It is a side view of a wheel.
- It is a block diagram of the imbalance correction apparatus of a rotating fluid element. It is a flowchart of the imbalance correction method of a rotating fluid element. It is a detailed flowchart of step 105 in the flowchart.
- (A) is a cross-sectional explanatory view of a turbocharger to which another unbalance correction method is applied, and (b) is a diagram illustrating a plurality of other unbalance corrections in the radial direction of the compressor wheel of the turbocharger. It is a side view of the compressor wheel to which is applied.
- (A) is a cross-sectional explanatory view of a turbocharger to which another unbalance correction method is applied, and (b) is a diagram illustrating a plurality of other unbalance corrections in the radial direction of the compressor wheel of the turbocharger.
- FIGS. 1 to 10 a compressor wheel of a turbocharger will be described as an example of a rotating fluid element.
- the rotating fluid element is not limited to the compressor wheel of the turbocharger, but may be a turbine wheel of the turbocharger provided on the opposite side of the compressor wheel. It should be noted that the materials, shapes, relative arrangements, and the like of the components described in this embodiment are not intended to limit the scope of the present invention, but are merely illustrative examples.
- the turbocharger 70 to which the rotating fluid element is applied will be outlined. As shown in FIG. 2A (cross-sectional explanatory view), the turbocharger 70 rotates the turbine wheel 71 that is rotated by exhaust gas of the engine, and rotates integrally with the turbine wheel 71 to generate compressed air. And a rotating shaft 78 having one end coupled to the turbine wheel 71 and the other end coupled to the compressor wheel 72.
- the turbocharger 70 is provided with a turbine housing (not shown) surrounding the turbine wheel 71, a compressor housing (not shown) surrounding the compressor wheel 72, and a bearing housing 79 that rotatably supports the rotating shaft 78. It has been.
- the compressor wheel 72 is formed by being cast from, for example, aluminum or titanium and cut by a lathe or the like.
- the compressor wheel 72 includes a disc-shaped back plate 73, a truncated cone-shaped boss portion 74 that protrudes in a direction orthogonal to one surface of the back plate 73, and is provided integrally with the back plate 73, and a boss portion 74 and a plurality of blades 75 provided integrally from the outer peripheral surface 74 a to the back plate 73.
- the plurality of blades 75 extend to the outer peripheral surface 74a of the boss portion 74 of the compressor wheel 72 so as to be inclined in the centrifugal direction.
- the outer peripheral surface 74a of the boss portion 74 is exposed between the blades 75 adjacent to each other in the circumferential direction of the compressor wheel 72 (hereinafter referred to as “blade space 76”).
- the cross-sectional shape of the boss portion 74 between the blades 76 gradually widens as the radial dimension gradually widens from the top portion of the boss portion 74 opposite to the back plate 73 toward the bottom portion on the back plate 73 side. , It is formed so as to be connected to the back plate 73 at the widest portion.
- the axial thickness of the boss portion 74 of the compressor wheel 72 is the thinnest at the radially outer end, gradually increases from the radially outer end to the radially inner side, and further increases in radial thickness. It is formed so as to become thinner as it progresses radially inward.
- the axial direction and radial thickness of the boss part 74 are related to the cutting and removing part 74 where the boss part 74 between the blades 76 is removed in order to correct an unbalance of the compressor wheel 72 described later.
- a through hole 74b penetrating from the top to the bottom of the boss 74.
- a rotary shaft 78 is inserted through the through hole 74 b, a nut 80 is screwed into the rotary shaft 78 extending from the tip of the boss portion 74, and the compressor wheel 72 is integrally coupled to the rotary shaft 78.
- the unbalance correction device 1 includes an area setting unit 3, an unbalance measurement unit 5, a cutting condition setting unit 7, a map 9, and a cutting work unit 11.
- the region setting unit 3 has a function of setting the inter-blade 76 that is a removal target portion of the compressor wheel 72 (rotating fluid element) to a plurality of different regions.
- FIG. 2B three annular regions A1, A2, and A3 having different radii that are concentric with the rotation center O of the compressor wheel 72 are set.
- the region A1 has a radius r1 smaller than the radius r0 of the compressor wheel 72.
- the width of the region A1 that is, the difference between the radius r0 and the radius r1
- the widths of the region A2 and the region A3 have the same width as the width of the region A1. For this reason, when the hole is cut into the areas A1, A2, and A3 with the drill 12, the holes are less likely to enter the adjacent areas A1, A2, and A3.
- an end mill is used instead of the drill 12 for the cutting work unit 11.
- the unbalance measuring unit 5 has a function of obtaining the unbalance amount and position of the compressor wheel 72.
- the unbalance measuring unit 5 detects the mark with an optical sensor (not shown) while rotating the compressor wheel 72 that is rotatably held and processed with the mark. Based on a detection signal from a detector (not shown), the amount and position of the unbalance of the compressor wheel 72 are measured. As a result, it is measured how many weights are unbalanced at the number of angles with the mark as the zero reference.
- the cutting condition setting unit 7 selects one of the three regions A1, A2, and A3 set by the region setting unit 3 based on the unbalance amount and position of the compressor wheel 72 obtained by the unbalance measuring unit 5. It has a function of selecting a region and obtaining a cutting position and a cutting amount in the selected region.
- the cutting condition setting unit 7 selects a region located on the outermost side of the compressor wheel 72, that is, the region A1. Based on the measured unbalance amount and position, the cutting amount and the cutting position are set in the region A1.
- the cutting position P1 sets the intersection of the center line S in the width direction of the region A1 and the virtual line K passing through the rotation center O of the compressor wheel 72 and the measured unbalance position.
- the cutting amount is set based on the distance from the rotation center O of the compressor wheel 72 to the cutting position P1 and the specific gravity of the material so that the measured unbalance amount can be cut off.
- the cutting condition setting unit 7 is based on the unbalance amount and position obtained again by the unbalance measurement unit 5 when the unbalance amount and position of the compressor wheel 72 that has been cut and removed are remeasured. Then, one of the three regions A1, A2, A3 other than the selected region (A1) (A2, A3) is selected, and the cutting position and the cutting amount of the selected region are obtained.
- the cutting condition setting unit 7 does not exceed the allowable cutting amount based on the map 9 in which the allowable cutting amount (see FIG. 6, Cn, Dn) that can be cut and removed is set in each of the plurality of regions when reselecting the region. Select one of the areas. For this reason, the possibility that the strength of the compressor wheel is lowered when the cutting amount is excessive is prevented.
- the cutting condition setting unit 7 obtains the cutting position for correcting the unbalance after the amount and position of the unbalanced compressor wheel 72 that has been cut and removed are re-measured, the cutting condition setting unit 7 The intersection of the center line in the width direction and the virtual line passing through the rotation center O of the compressor wheel 72 and the measured unbalance position is set. However, when the intersection point is on the wing or near the wing to some extent in terms of strength, a point on the center line that can be cut off closest to the intersection is set.
- the cutting condition setting unit 7 determines the unbalance amount of the compressor wheel 72 when the cutting amount for correcting the unbalance after the remeasurement of the unbalance amount and the position of the compressor wheel 72 that has been cut and removed is obtained.
- the cutting amount relative to the balance amount is obtained based on the map 9 set for each of a plurality of regions. As shown in FIG. 6, the map 9 is provided for each of the areas A1, A2, and A3. In the map 9, for example, in the case of the area A1, when the measured unbalance amounts are U1, U2, and U3, the cutting amounts are set as C1, C2, and C3, and the maximum allowable cutting amount (Allowable cutting amount Cn (max)) is also set. If the measured unbalance amount does not exist in the map 9, the cutting condition setting unit 7 sets the two unbalance amounts on the map 9 defined before and after the measured unbalance amount. It calculates based on two corresponding cutting amounts.
- the map 9 is set to have cutting amounts of D1, D2, and D3, and the maximum allowable amount.
- a cutting amount (allowable cutting amount Dn (max)) is also set. It should be noted that D1> C1, D2> C2, D3> C3, and Dn> Cn.
- the cutting work unit 11 is configured to machine a boss portion 74 between the blades 76 of the compressor wheel 72 into a circular shape using the drill 12.
- a recess 74c having a drill tip shape is formed on the outer peripheral surface 74a of the boss portion 74 processed by the drill 12.
- the region setting unit 3 sets the inter-blade 76 as a removal target portion of the compressor wheel 72 to a plurality of different regions A1, A2, and A3. (Step 100).
- three annular regions A1, A2, and A3 having different radii that are concentric with the rotation center O of the compressor wheel 72 are set (see FIG. 2B).
- the cutting condition setting unit 7 includes a region including a radially outer peripheral portion among the plurality of regions A1, A2, and A3. That is, a region A1 located on the outermost radial direction is selected, and a cutting position and a cutting amount of the selected region A1 are obtained.
- the cutting work unit 11 performs the first cutting removal with the calculated cutting amount at the cutting position in the selected region A1 (step 104). Then, the number of deletions n is set to 1 (step 105). Then, the amount and position of the unbalanced compressor wheel 72 that has been cut and removed are obtained again by the unbalance measuring unit 5 (step 106). If the amount of imbalance obtained in step 106 is less than or equal to the threshold value, the process is terminated, and if not less than the threshold value, the process proceeds to step 108 (step 107). Based on the balance amount and position, any one of the plurality of areas A1, A2, A3 other than the already selected area A1 is selected (step 108a, see FIG. 5).
- the additional region it is desirable to set the order of A2 and A3 so as to gradually go inward in the radial direction.
- the allowable cutting amount in the selected region is larger than the cutting amount obtained in step 103.
- A3 may be selected before A2.
- the cutting condition setting unit 7 obtains the cutting position of the selected additional region (see step 108b, FIG. 5).
- obtaining the cutting position an intersection between the center line in the width direction in the selected additional region and the virtual line passing through the rotation center O of the compressor wheel 72 and the measured unbalance position is set.
- the intersection is determined to be located on the resectable center line closest to the intersection. That is, if the cutting removal part in the area A1 cannot be a point on the imaginary line K because it avoids the blade, the unbalanced vector before cutting and the remaining unbalanced vector may be different.
- the unbalance can be effectively reduced, and the accuracy of the unbalance correction can be increased.
- the cutting condition setting unit 7 obtains the cutting amount of the selected region A2 (see step 108c, FIG. 5).
- the cutting amount is obtained, it is obtained based on the map 9 in accordance with the unbalance amount obtained in step 103. For this reason, the cutting amount can be easily obtained via the map 9. For this reason, when calculating
- the cutting work unit 11 performs the second cutting removal with the cutting amount obtained in the sixth step at the cutting position in the additional region selected in step 108a (step 109).
- the compressor wheel (rotation) whose unbalance is corrected by the two cutting removal portions 74c provided at different positions on the outer peripheral surface 74a of the boss portion 74, as shown in FIGS. Fluid element) 72 is completed.
- step 111 If the amount of imbalance obtained in step 111 is less than or equal to the threshold value, the process ends, and if not less than the threshold value, the process proceeds to step 113 (step 112). In step 113, if the number of times of cutting exceeds the threshold value, the process ends. If it exceeds, the process returns to step 108 and the third unbalance adjustment is performed.
- the compressor wheel 72 unbalance-corrected in step 109 is positioned in the substantially central portion of a pair of blades 76 adjacent to each other in the circumferential direction in the radially outermost region A1 (hereinafter referred to as “radial outer peripheral edge”).
- the first cutting / removing portion 74c1 cut and removed in the portion Pa1), and in the additional region radially inward of the region A1 and in the radially inner portion Pa2 of the first cutting / removing portion 74c1.
- the additional cutting removal part 74c2 thus provided is provided.
- the first cutting / removing portion 74c1 and the additional cutting / removing portion 74c2 realize a compressor wheel 72 (rotating fluid element) that has been subjected to highly accurate imbalance correction without reducing the strength of the blade 75.
- the region setting unit 3 uses a plurality of regions A1, A2, A3 based on the amount and position of the unbalance obtained in step 111.
- One of the additional areas (A3) other than the already selected areas A1 and A2 is selected (step 108a, see FIG. 5).
- the cutting condition setting unit 7 obtains the cutting position of the selected additional region (see step 108b, FIG. 5).
- obtaining the cutting position an intersection between the center line in the width direction in the selected additional region and the virtual line passing through the rotation center O of the compressor wheel 72 and the measured unbalance position is set.
- the intersection is determined to be located on the resectable center line closest to the intersection. That is, if the cutting removal part in the area A1 cannot be a point on the imaginary line K because it avoids the blade, the unbalanced vector before cutting and the remaining unbalanced vector may be different.
- the unbalance can be effectively reduced, and the accuracy of the unbalance correction can be increased.
- the cutting condition setting unit 7 obtains the cutting amount of the selected region A3 (step 108c, see FIG. 5).
- the cutting amount is obtained, it is obtained based on the map 9 according to the unbalance amount obtained in step 108. For this reason, the cutting amount can be easily obtained via the map 9. For this reason, when calculating
- the cutting position P1 obtained in the already selected region A1 and the compressor wheel 72 are determined.
- the cutting position is determined so as to be positioned on an imaginary line K connecting the rotation center O. For this reason, as shown in FIGS. 7A and 7B, for a corresponding portion of the nut 80 arranged on the imaginary line connecting the first cutting position P1 and the rotation center O of the compressor wheel 72.
- the cutting removal for correcting the imbalance can be performed. Therefore, the unbalance can be corrected even for a larger unbalance amount. Therefore, the imbalance correction accuracy can be further increased, and the yield of the turbocharger 70 as a product can be improved.
- a plurality of annular regions A1, A2, and A3 having different radii that are concentric with the rotation center O of the compressor wheel 72 are set.
- It may be set as a pair of phase regions B1 and B2 that are arranged at positions opposite to each other on one side in the radial direction and the other side in the radial direction with respect to the rotation center O.
- the cutting amount obtained in step 102 is larger than the cutting amount obtained in step 101 so that an unbalance amount smaller than the unbalance amount obtained in step 101 occurs in the opposite phase region B1. The amount of cutting.
- step 103 based on the cutting amount obtained in step 102, the cutting work unit 11 cuts and removes the selected phase region B1, and in step 106, the unbalance amount and position obtained in step 104. Based on the above, the phase region B1 on the opposite side is cut and removed, and an unbalance corrected compressor wheel (rotating fluid element) 72 is completed.
- the unbalance-corrected compressor wheel 72 ′ is cut and removed at the radially outer peripheral edge Pa 1 in the substantially central portion of the pair of blades 76 adjacent in the circumferential direction in the phase region B 1.
- 74c1 and an additional cutting removal portion 74c2 that is in the phase region B2 opposite to the phase region B1 and is in a phase opposite to that of the first cutting removal portion 74c1 and cut and removed at the radially inner portion Pa2.
- the first cutting / removing part 74c1 and the additional cutting / removing part 74c2 realize a compressor wheel 72 ′ (rotating fluid element) that has been subjected to highly accurate imbalance correction without reducing the strength of the blade 75.
- the cutting position P1 that is removed by the first cutting and the cutting position P2 that is removed by the second cutting are in different phase regions B1 and B2. For this reason, it is possible to perform fine adjustment during the second correction process of the unbalance remaining at the first time, and the accuracy of the unbalance correction can be increased.
- the plurality of regions are set as a plurality of annular regions A1, A2, and A3 having different radii that are concentric with the rotation center O of the compressor wheel 72, and each region is cut and removed.
- the case where it was made not to overlap each other was shown, as shown in FIG. 9, in the blade
- the compressor wheel (rotating fluid element) 72 ′′ with the unbalance corrected may be completed by cutting into a long hole extending continuously.
- the unbalance-corrected compressor wheel 72 ′′ includes a first cutting removal portion 74c1 that is cut and removed to a radially outer peripheral edge portion Pa1 between a pair of blades 76 that are adjacent to each other in the circumferential direction in the region A1.
- An additional cutting removal portion 74c2 that is cut and removed from the one cutting removal portion 74c1 to the radially inner portion Pa2 extending from the region A1, the region A2, the region A3, and the region A4 is provided.
- the first cutting / removing part 74c1 and the additional cutting / removing part 74c2 realize a compressor wheel 72 ′′ (rotating fluid element) that has been subjected to highly accurate imbalance correction without reducing the strength of the blades 75.
- the first cutting removal part 74c1 and the additional cutting removal part 74c2 are connected to each other and formed in the shape of an elongated hole, so that the amount of unbalance correction can be increased. Therefore, the unbalance can be corrected even for a larger unbalance amount. Therefore, the imbalance correction accuracy can be further increased, and the yield of the turbocharger 70 as a product can be improved.
- the plurality of regions are set as a plurality of annular regions A1, A2, and A3 having different radii that are concentric with the rotation center O of the compressor wheel 72, and each region is cut and removed.
- the first cutting removal unit 74c1 is connected to the compressor in the blade space 76 provided with the first cutting removal unit 74c1 in the region A1.
- An unbalance-corrected compressor wheel (rotating fluid element) 72 ′ ′′ may be produced by cutting into a long hole extending continuously in a direction orthogonal to the centripetal direction of the wheel 72.
- the unbalance-corrected compressor wheel 72 ′ ′′ includes a first cutting removal portion 74c1 that is cut and removed in the radially outer peripheral edge portion Pa1 between the pair of blades 76 that are adjacent to each other in the circumferential direction in the region A1.
- An elongated hole-shaped additional cutting removal portion 74c2 that is cut and removed from the first cutting removal portion 74c1 in a radially inner portion Pa2 continuously extending in a direction orthogonal to the centripetal direction of the compressor wheel 72 is provided.
- the first cutting / removing part 74c1 and the additional cutting / removing part 74c2 realize a compressor wheel 72 ′ ′′ (rotating fluid element) that is highly accurate unbalance correction without reducing the strength of the blades 75. .
- the radius r1 from the rotation center O of the radially outer peripheral edge portion Pa1 and the radius r2 from the rotation center O of the radially inner edge portion Pa2 have a relationship of radius r1> radius r2.
- the first cutting removal part 74c1 and the additional cutting removal part 74c2 are connected to each other and formed in a straight line, so that the amount of unbalance correction can be increased. Therefore, the unbalance can be corrected even for a larger unbalance amount. Therefore, the imbalance correction accuracy can be further increased, and the yield of the turbocharger 70 as a product can be improved.
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Abstract
Description
ボス部の外周面に遠心方向に延びて円周方向に間隔を有して配設された複数の翼を備え、円周方向に隣接する翼間にアンバランスを低減するための切削除去部が設けられた回転流体要素において、
前記切削除去部は、
前記翼間の径方向外側周縁部位に切削除去された第1切削除去部と、
前記第1切削除去部(74c1)よりも径方向内側部位に切削除去された1つ以上の追加切削除去部と、を含むように構成される。
前記第1切削除去部は、前記回転流体要素の回転中心と同心円とする半径が異なる複数の環状の領域のうち最も径方向外側に位置する環状の領域内に設けられ、
前記追加切削除去部は、前記最も径方向外側に位置する環状の領域以外の環状の領域内に設けられ、
さらに、前記追加切削除去部が複数ある場合は、それぞれが異なる環状の領域に設けられているように構成される。
前記第1切削除去部は、前記回転流体要素の回転中心に対して径方向一方側及び径方向他方側であって互いに逆位相に位置する一対の位相領域のいずれかの領域内に設けられ、
前記追加切削除去部は、前記第1切削除去部が設けられた位相領域と反対側の位相領域内に設けられているように構成される。
前記追加切削除去部は、前記第1切削除去部が設けられた翼間内において、該第1切削除去部から径方向内側に連続的に延びて設けられるように構成される。
前記追加切削除去部は、前記第1切削除去部が設けられた翼間内において、該第1切削除去部から前記回転流体要素の求心方向に直交する方向に延びて設けられているように構成される。
ボス部の外周面に遠心方向に延びて円周方向に間隔を有して配設された複数の翼を備え、円周方向に隣接する翼間にアンバランスを低減する切削除去部を設けるための回転流体要素のアンバランス修正方法であって、
前記回転流体要素の周方向に隣接する復数の翼間に径方向外側周縁部位を含む領域と、該領域よりも径方向内側に位置する領域を含む復数の領域を設定する第1ステップと、
前記回転流体要素のアンバランスの量と位置を求める第2ステップと、
前記第2ステップで求められた前記回転流体要素のアンバランスの量と位置に基づいて、前記複数の領域のうち前記径方向外側周縁部位を含む領域を選択し、選択された領域の切削位置と切削量を求める第3ステップと、
前記第3ステップで求められた前記切削位置及び前記切削量に基づいて、該切削位置において前記第3ステップで求められた切削量で第1回目の切削除去を行って第1切削除去部を設ける第4ステップと、
前記第1回目の切削除去がされた回転流体要素のアンバランスの量と位置を求める第5ステップと、
前記第5ステップで求められたアンバランスの量と位置に基づいて、前記複数の領域のうち前記選択された領域以外の領域を選択し、この選択された領域の切削位置と切削量を求める第6ステップと
前記第6ステップで求められた切削位置及び切削量に基づいて、該切削位置において第6ステップで求められた切削量で第2回目の切削除去を行って追加切削除去部を設ける第7ステップと、を含むように構成される。
前記第5ステップから前記第7ステップまでを、
所定のアンバランス量以下になるまで繰り返すように構成される。
前記第1ステップで設定される複数の領域は、前記回転流体要素の回転中心と同心円とする半径が異なる複数の環状の領域として設定され、
前記第3ステップで選択される領域は、前記複数の環状の領域のうち最も径方向外側に位置する環状の領域であり、
前記第6ステップで選択される領域は、前記第5ステップで求められたアンバランスの量と位置に基づいて、前記最も径方向外側に位置する環状の領域以外の環状の領域が選択されるように構成される。
前記複数の領域のそれぞれには、切削除去可能な許容切削量が設定され、
前記第6ステップで選択される領域は、前記許容切削量を超えない領域のいずれかであるように構成される。
前記第6ステップで求められる切削位置は、選択された領域内において前記第3ステップで求められた切削位置と前記回転流体要素の回転中心とを繋ぐ仮想線上の位置であるように構成される。
前記回転流体要素のアンバランスの量に対する切削量を前記複数の領域ごとに設定したマップを予め設け、
前記第6ステップで求められる切削量は、前記第5ステップで求められたアンバランスの量に応じて前記マップに基づいて求められるように構成される。
前記第1ステップで設定される複数の領域は、前記回転流体要素の回転中心に対して径方向一方側及び径方向他方側であって互いに逆位相の位置に配置される一対の位相領域として設定され、
前記第3ステップで選択される領域は、前記一対の位相領域のうち前記径方向外側周縁部位を含む位相領域のいずれかであり、
前記第6ステップで選択される領域は、前記第3ステップで選択された位相領域と反対側の位相領域であるように構成される。
前記第3ステップで求められる前記切削量は、前記第2ステップで求められるアンバランスの量よりも小さいアンバランスの量が前記反対側の位相領域に生じるように、前記第2ステップで求められる切削量よりも大きな切削量であり、
前記第4ステップにおいて、前記第3ステップで求められた前記切削量に基づいて、選択された位相領域を切削除去し、
前記第6ステップにおいて、前記第5ステップで求められるアンバランスの量と位置に基づいて、前記反対側の位相領域を切削除去するように構成される。
3 領域設定部
5 アンバランス計測部
7、23 切削条件設定部
9 マップ
11 切削作業部
12 ドリル
70 ターボ過給機
71 タービンホイール
72、72'、72''、72''' コンプレッサホイール(回転流体要素)
73 背面板
74 ボス部
74a 外周面
74b 貫通孔
74c 切削除去部
74c1 第1切削除去部
74c2 追加切削除去部
75 翼
76 翼間
78 回転軸
79 軸受ハウジング
80 ナット
A1、A2、A3 領域
B1、B2 位相領域
K 仮想線
O 回転中心
P1、P2 切削位置
Pa1 径方向外側周縁部位
Pa2 径方向内側部位
Claims (12)
- ボス部の外周面に遠心方向に延びて円周方向に間隔を有して配設された複数の翼を備え、翼間にアンバランスを低減するための切削除去部が設けられた回転流体要素において、
前記切削除去部は、
前記翼間の径方向外側部位に切削除去された第1切削除去部と、
前記第1切削除去部よりも径方向内側部位に切削除去された1つ以上の追加切削除去部と、を含む
ことを特徴とする回転流体要素。 - 前記第1切削除去部は、前記回転流体要素の回転中心と同心円とする半径が異なる複数の環状の領域のうち最も径方向外側に位置する環状の領域内に設けられ、
前記追加切削除去部は、前記最も径方向外側に位置する環状の領域以外の環状の領域内に設けられ、
さらに、前記追加切削除去部が複数ある場合は、それぞれが異なる環状の領域に設けられている
ことを特徴とする請求項1に記載の回転流体要素。 - 前記第1切削除去部は、前記回転流体要素の回転中心に対して径方向一方側及び径方向他方側であって互いに逆位相に位置する一対の位相領域のいずれかの領域内に設けられ、
前記追加切削除去部は、前記第1切削除去部が設けられた位相領域と反対側の位相領域内に設けられている
ことを特徴とする請求項1に記載の回転流体要素。 - 前記追加切削除去部は、前記第1切削除去部が設けられた翼間内において、該第1切削除去部から径方向内側に連続的に延びて設けられている
ことを特徴とする請求項1に記載の回転流体要素。 - 前記追加切削除去部は、前記第1切削除去部が設けられた翼間内において、該第1切削除去部から前記回転流体要素の求心方向に直交する方向に延びて設けられている
ことを特徴とする請求項1に記載の回転流体要素。 - ボス部の外周面に遠心方向に延びて円周方向に間隔を有して配設された複数の翼を備え、円周方向に隣接する翼間にアンバランスを低減する切削除去部を設けるための回転流体要素のアンバランス修正方法であって、
前記回転流体要素の周方向に隣接する復数の翼間に径方向外側周縁部位を含む領域と、該領域よりも径方向内側に位置する領域を含む復数の領域を設定する第1ステップと、
前記回転流体要素のアンバランスの量と位置を求める第2ステップと、
前記第2ステップで求められた前記回転流体要素のアンバランスの量と位置に基づいて、前記複数の領域のうち前記径方向外側周縁部位を含む領域を選択し、選択された領域の切削位置と切削量を求める第3ステップと、
前記第3ステップで求められた前記切削位置及び前記切削量に基づいて、該切削位置において前記第3ステップで求められた切削量で第1回目の切削除去を行って第1切削除去部を設ける第4ステップと、
前記切削除去がされた回転流体要素のアンバランスの量と位置を求める第5ステップと、
前記第5ステップで求められたアンバランスの量と位置に基づいて、前記複数の領域のうち前記選択された領域以外の追加領域を選択し、この選択された追加領域の切削位置と切削量を求める第6ステップと
前記第6ステップで求められた切削位置及び切削量に基づいて、該切削位置において第6ステップで求められた切削量で追加の切削除去を行って追加削除去部を設ける第7ステップと、を含む
ことを特徴とする回転流体要素のアンバランス修正方法。 - 前記第5ステップから前記第7ステップまでを、
所定のアンバランス量以下になるまで繰り返す
ことを特徴とした請求項6に記載のアンバランス修正方法。 - 前記第1ステップで設定される複数の領域は、前記回転流体要素の回転中心と同心円とする半径が異なる複数の環状の領域として設定され、
前記第3ステップで選択される領域は、前記複数の環状の領域のうち最も径方向外側に位置する環状の領域であり、
前記第6ステップで選択される領域は、前記第5ステップで求められたアンバランスの量と位置に基づいて、前記最も径方向外側に位置する環状の領域以外の環状の領域が選択される
ことを特徴とする請求項6に記載の回転流体要素のアンバランス修正方法。 - 前記複数の領域のそれぞれには、切削除去可能な許容切削量が設定され、
前記第6ステップで選択される領域は、前記許容切削量を超えない領域のいずれかである
ことを特徴とする請求項8に記載の回転流体要素のアンバランス修正方法。 - 前記第6ステップで求められる切削位置は、選択された領域内において前記第3ステップで求められた切削位置と前記回転流体要素の回転中心とを繋ぐ仮想線上の位置である
ことを特徴とする請求項9に記載の回転流体要素のアンバランス修正方法。 - 前記回転流体要素のアンバランスの量に対する切削量を前記複数の領域ごとに設定したマップを予め設け、
前記第6ステップで求められる切削量は、前記第3ステップで求められたアンバランスの量に応じて前記マップに基づいて求められる
ことを特徴とする請求項10に記載の回転流体要素のアンバランス修正方法。 - 前記第1ステップで設定される複数の領域は、前記回転流体要素の回転中心に対して径方向一方側及び径方向他方側であって互いに逆位相の位置に配置される一対の位相領域として設定され、
前記第3ステップで選択される領域は、前記一対の位相領域のうち前記径方向外側周縁部位を含む位相領域のいずれかであり、
前記第6ステップで選択される領域は、前記第3ステップで選択された位相領域と反対側の位相領域である
ことを特徴とする請求項6に記載の回転流体要素のアンバランス修正方法。
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