WO2015146765A1 - インペラ締結構造及びターボ圧縮機 - Google Patents
インペラ締結構造及びターボ圧縮機 Download PDFInfo
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- WO2015146765A1 WO2015146765A1 PCT/JP2015/058186 JP2015058186W WO2015146765A1 WO 2015146765 A1 WO2015146765 A1 WO 2015146765A1 JP 2015058186 W JP2015058186 W JP 2015058186W WO 2015146765 A1 WO2015146765 A1 WO 2015146765A1
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- Prior art keywords
- axis
- impeller
- bolt
- fastening structure
- shaft
- Prior art date
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- 230000002093 peripheral effect Effects 0.000 claims abstract description 5
- 230000006835 compression Effects 0.000 description 34
- 238000007906 compression Methods 0.000 description 34
- 239000012530 fluid Substances 0.000 description 15
- 230000004048 modification Effects 0.000 description 8
- 238000012986 modification Methods 0.000 description 8
- 238000003754 machining Methods 0.000 description 3
- 230000001105 regulatory effect Effects 0.000 description 2
- 238000013459 approach Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 230000008961 swelling Effects 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
- F04D29/266—Rotors specially for elastic fluids mounting compressor rotors on shafts
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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
- F01D5/025—Fixing blade carrying members on shafts
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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
- F04D25/00—Pumping installations or systems
- F04D25/16—Combinations of two or more pumps ; Producing two or more separate gas flows
- F04D25/163—Combinations of two or more pumps ; Producing two or more separate gas flows driven by a common gearing arrangement
-
- 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
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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
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2220/00—Application
- F05B2220/40—Application in turbochargers
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- 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
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B35/00—Screw-bolts; Stay-bolts; Screw-threaded studs; Screws; Set screws
- F16B35/04—Screw-bolts; Stay-bolts; Screw-threaded studs; Screws; Set screws with specially-shaped head or shaft in order to fix the bolt on or in an object
- F16B35/06—Specially-shaped heads
Definitions
- the present invention relates to an impeller fastening structure and a turbo compressor. This application claims priority based on Japanese Patent Application No. 2014-064179 for which it applied to Japan on March 26, 2014, and uses the content here.
- Patent Document 1 discloses a rotor of a turbo compressor composed of an impeller and a rotating shaft that supports the impeller, a mechanical joint formed on each end face of the impeller and the rotating shaft, and an impeller A tension bolt inserted into a through hole formed at the center of rotation, a tightening nut screwed into a first male screw formed at one end of the tension bolt, and an extension portion of the tension bolt formed on the end surface of the rotating shaft
- a rotor of a turbo compressor provided with a fastening mechanism comprising a housing hole for housing a part of the housing and a female screw formed on the bottom surface of the housing hole and screwed into a second male screw formed at the other end of the tension bolt Is disclosed.
- Such prior art has the following characteristics. (1) When the second male screw of the tension bolt is screwed into the female screw formed on the rotating shaft, the tension bolt is attached to be inclined with respect to the rotating shaft, so that the rotor unbalance may be excessive. This is because it is difficult to achieve the same degree of concentricity in the screw portion composed of the male screw and the female screw. (2) Since the tension bolt is torque-tightened at the terminal end (the innermost part) of the female screw, the stop position (axial position) of the tension bolt with respect to the rotating shaft is not stable, and thus the reproducibility of the rotor assembly is improved. There is a possibility that it cannot be secured.
- the present invention has been made in view of the above-described circumstances, and aims to solve the above two possibilities.
- a rotary shaft having an attachment hole formed at one end along a first axis (rotation axis) and a through-hole along a second axis (impeller axis).
- An impeller fastening structure comprising: an impeller formed with: a stud bolt that is inserted into a through-hole, and one end of which is screwed into a mounting hole; and a nut that is screwed into the other end of the stud bolt;
- the projecting portion projecting in the radial direction is provided at an intermediate position in the axial direction, and the rotating shaft has an impeller fastening structure including a receiving portion that abuts the projecting portion on the opening periphery of the mounting hole.
- the protruding portion includes an inclined surface that is inclined with respect to a third axis that is an axis of the stat bolt, and the receiving portion is inclined.
- a receiving surface that abuts the surface is provided.
- the first aspect further includes a first centering portion that aligns the second axis and the first axis, and the protruding portion includes the third center.
- An orthogonal surface orthogonal to the shaft center (bolt shaft center) is provided, and the receiving portion includes a receiving surface that contacts the orthogonal surface.
- the one end of the stat bolt has a larger shaft diameter than the other end of the stat bolt.
- the fifth aspect of the present invention further includes a second centering portion that aligns the second axis and the third axis in any of the first to fourth aspects.
- the sixth aspect further includes a third centering portion that aligns the first axis and the third axis.
- a seventh aspect of the present invention is a turbo compressor including a rotor in which a rotating shaft and an impeller are fastened by the impeller fastening structure of any of the first to sixth aspects.
- a rotary shaft having an attachment hole formed along one end of the first axis, an impeller formed with a through hole along the second axis, and the through hole.
- An impeller fastening structure including a stat bolt inserted through one end and screwed into the mounting hole, and a nut screwed into the other end of the stat bolt, and the stat bolt is connected to the stud at the end on the one end side.
- the rotating shaft has a receiving portion that is orthogonal to the first axis and is in contact with the orthogonal surface at the innermost portion of the mounting hole. It is an impeller fastening structure provided.
- the one end of the stat bolt has a larger shaft diameter than the other end of the stat bolt.
- a tenth aspect of the present invention further includes a first centering portion that aligns the second axis and the first axis in the aspect of 8 or 9 above.
- the eleventh aspect further includes a second centering portion that aligns the second axis and the third axis.
- the twelfth aspect further includes a third centering portion that aligns the first axis and the third axis.
- a thirteenth aspect of the present invention according to the twelfth aspect further includes an auxiliary third centering portion that aligns the first axis and the third axis.
- a fourteenth aspect of the present invention is a turbo compressor comprising a rotor in which a rotating shaft and an impeller are fastened by the impeller fastening structure described in any of the eighth to thirteenth aspects.
- the present invention it is possible to solve the above-described characteristics of the prior art.
- the stop position of the stat bolt (tension bolt) with respect to the rotating shaft is stabilized, the reproducibility of the rotor assembly can be ensured.
- FIG. 1 It is a top view which shows schematic structure of the turbo compressor 1 which concerns on 1st, 2nd embodiment of this invention. It is sectional drawing which shows the principal part of the turbo compressor 1 which concerns on 1st, 2nd embodiment of this invention. It is sectional drawing which shows the impeller fastening structure which concerns on 1st Embodiment of this invention. It is sectional drawing which shows the impeller fastening structure which concerns on 1st Embodiment of this invention. It is sectional drawing which shows the impeller fastening structure which concerns on 2nd Embodiment of this invention. It is sectional drawing which shows the impeller fastening structure which concerns on 2nd Embodiment of this invention.
- the turbo compressor 1 includes a drive motor 2, a connecting shaft 3, a gear device 4, a first stage compression unit 5, a second stage compression unit 6, and a third stage compression unit 7. , A fourth stage compression unit 8, a first intercooler 9, a second intercooler 10, and an aftercooler 11.
- the drive motor 2 is a power source of the turbo compressor 1, and the rotating shaft is connected to one end of the connecting shaft 3.
- One end of the connecting shaft 3 is connected to the rotating shaft of the drive motor 2, and the other end is connected to the drive shaft 4 a (see FIG. 2) of the gear device 4.
- the gear device 4 accelerates the rotation of the drive motor 2 (that is, the connecting shaft 3) and transmits it to the first stage compression unit 5, the second stage compression unit 6, the third stage compression unit 7, and the fourth stage compression unit 8. Power transmission device.
- the first stage compression unit 5, the second stage compression unit 6, the third stage compression unit 7, the fourth stage compression unit 8, the first intercooler 9, the second intercooler 10, and the aftercooler 11 are indicated by broken line arrows in FIG.
- the first-stage compression section 5 ⁇ the first intercooler 9 ⁇ the second-stage compression section 6 ⁇ the second intercooler 10 ⁇ the third-stage compression section 7 ⁇ the after-cooler 11 ⁇ the fourth-stage compression section 8 is connected in accordance with the fluid flow path. Has been.
- the first stage compression unit 5 is located in the uppermost stream of the fluid passage path, compresses the fluid in the first stage, and supplies the fluid to the first intercooler 9.
- the first intercooler 9 cools the fluid (compressed fluid) supplied from the first stage compression unit 5 and supplies it to the second stage compression unit 6.
- the second stage compression unit 6 compresses the compressed fluid supplied from the first intercooler 9 in the second stage and supplies the compressed fluid to the second intercooler 10.
- the second intercooler 10 cools the compressed fluid supplied from the second stage compression unit 6 and supplies it to the third stage compression unit 7.
- the third stage compression unit 7 compresses the compressed fluid supplied from the second intercooler 10 in a third stage and supplies the compressed fluid to the aftercooler 11.
- the aftercooler 11 cools the compressed fluid supplied from the third stage compression unit 7 and supplies it to the fourth stage compression unit 8.
- the fourth stage compression unit 8 compresses the compressed fluid supplied from the aftercooler 11 into the fourth stage and supplies the compressed fluid to the outside.
- a drive shaft 4a of the gear device 4 is rotatably supported by the housing 4b, and a drive gear 4c having a relatively large diameter is attached thereto.
- the drive gear 4c is provided at a substantially intermediate position between the first driven gear 4e having a smaller diameter than the drive gear 4c provided at a substantially intermediate position of the first driven shaft (rotating shaft) 4d and the second driven shaft 4f.
- the second driven gear 4g having a smaller diameter than the drive gear 4c is engaged with each other.
- the first driven shaft 4d is rotatably supported by the housing 4b in a state parallel to the drive shaft 4a, a first impeller (impeller) 5a is attached to one end, and a second impeller 6a is attached to the other end. Is attached.
- the second driven shaft 4f is rotatably supported by the housing 4b in a state parallel to the drive shaft 4a, and has a third impeller 7a attached to one end and the other end.
- the 4th impeller 8a is attached to.
- the first impeller 5 a is accommodated in a first impeller casing 5 b provided on the side of the housing 4 b of the gear device 4, and the second impeller 6 a is a first impeller casing across the housing 4 b of the gear device 4.
- the third impeller 7a is accommodated in a third impeller casing 7b provided on the side of the housing 4b of the gear unit 4 and accommodated in a second impeller casing 6b provided on the side opposite to 5b.
- the fourth impeller 8a is accommodated in a fourth impeller casing 8b provided on the opposite side of the third impeller casing 7b with the casing 4b of the gear device 4 interposed therebetween.
- a fluid intake passage, a diffuser passage, and a scroll passage are formed, respectively.
- a rotating body including the first driven shaft 4d, the first driven gear 4e, the first impeller 5a, and the second impeller 6a is referred to as a first rotor R1
- a rotating body including the impeller 7a and the fourth impeller 8a is referred to as a second rotor R2.
- the number of teeth of the first driven gear 4e is set to be smaller than the number of teeth of the drive gear 4c, and the rotation of the drive motor 2 (that is, the connecting shaft 3) rotates the teeth of the drive gear 4c.
- the speed is increased at a speed increasing ratio (first speed increasing ratio) corresponding to the ratio of the number of teeth to the number of teeth of the first driven gear 4e (first gear ratio) and transmitted to the first driven shaft 4d.
- the number of teeth of the second driven gear 4g is set to be smaller than the number of teeth of the drive gear 4c, and the rotation of the drive motor 2 (that is, the connecting shaft 3) is rotated by the teeth of the drive gear 4c.
- the speed is increased at a speed increasing ratio (second speed increasing ratio) corresponding to the ratio of the number of teeth to the number of teeth of the second driven gear 4g (second tooth number ratio) and transmitted to the second driven shaft 4f.
- the impeller fastening structure according to the first embodiment of the present invention that is, the fastening structure of the first impeller 5a and the second impeller 6a with respect to the first driven shaft 4d and the second driven shaft of the third impeller 7a and the fourth impeller 8a.
- the fastening structure with respect to 4f is demonstrated with reference to FIG. 3A and FIG. 3B.
- the fastening structure with respect to the 1st driven shaft 4d of the 1st impeller 5a is demonstrated as a representative.
- an attachment hole H extending in the direction along the first axis (rotation axis L1) is formed in the vicinity of the center of the one end surface E of the first driven shaft 4d.
- a polygonal fitting surface (shaft fitting surface M) having a predetermined width in the direction of the rotation axis L1 is formed on the outer periphery of the one end surface E.
- the one end surface E is an orthogonal surface orthogonal to the rotation axis L1.
- a through hole K is formed in the first impeller 5a along the second axis (impeller axis L2).
- the first impeller 5a is fastened to one end of the first driven shaft 4d by a tension bolt B (stat bolt) and a nut N.
- first impeller fitting surface J1 that is concentric with the impeller shaft center L2 and has a predetermined width in the direction of the impeller shaft center L2.
- the first impeller fitting surface J1 is fitted with the above-described shaft fitting surface M so that the impeller shaft center L2 and the rotation shaft shaft center L1 are concentric.
- the first impeller fitting surface J1 and the shaft fitting surface M as described above constitute a first centering portion F1.
- a cylindrical fitting surface (second impeller fitting surface J2) that is concentric with the impeller shaft center L2 and has a predetermined width in the direction of the impeller shaft center L2 is formed. ing.
- the first centering portion F1 prevents the first impeller 5a from falling.
- the first centering portion F1 employs a polygon fit for fitting the polygonal shaft fitting surface M and the first impeller fitting surface J1, but instead of this, the shaft fitting surface M is used.
- the inlay which forms the 1st impeller fitting surface J1 in a column shape may be employ
- the tension bolt B is a round bar-shaped member having a predetermined length, and has a first male screw portion b1 having a predetermined length at one end and a second male screw having a predetermined length at the other end. It is a stat bolt in which a screw part b2 is formed.
- the shaft diameter of the first male screw portion b1 is slightly larger than the shaft diameter of the second male screw portion b2 as shown in the figure.
- the shaft diameter of the first male screw portion b1 is 1.2 to 2.0 times the shaft diameter of the second male screw portion b2.
- a cylindrical fitting surface (bolt fitting surface) is provided inside the second male screw portion b2 (that is, on the first male screw portion b1 side) so as to be adjacent to the second male screw portion b2. b5) is provided.
- the bolt fitting surface b5 is a cylindrical surface that is concentric with the third shaft center (bolt shaft center L3) and has a predetermined width in the direction of the bolt shaft center L3, and the second impeller fitting surface J2 described above. Mating.
- such a bolt fitting surface b5 and the second impeller fitting surface J2 align (concentrize) the impeller shaft center L2 and the shaft center (bolt shaft center L3) of the tension bolt B.
- a centering portion F2 (inlay) is configured. The second centering portion F2 assists in preventing the first impeller 5a from falling.
- the tension bolt B is arranged in the radial direction (bolt axis center) at a midpoint in the direction (axial center direction) of the third axis (bolt axis L3), for example, at a position adjacent to the first male screw portion b1 as shown in the drawing. And a projecting portion b3 projecting in a direction orthogonal to L3.
- a tightening force from a tool such as a wrench causes the projecting portion b3 to move. Via the tension bolt B.
- a tool such as a wrench
- the protruding portion b3 includes a tapered surface b4 (inclined surface) that is linearly inclined with respect to the bolt axis L3.
- the inclination angle of the tapered surface b4 is, for example, 30 to 45 °.
- the taper surface b4 is an annular surface that continuously extends around the bolt axis L3 with the bolt axis L3 as the center, and is reduced in diameter as it approaches the first male screw part b1. Moreover, in this taper surface b4, the shaft diameter of the portion closest to the first male screw portion b1 is equal to the shaft diameter of the first male screw portion b1. A slight gap is provided between the first male screw portion b1 and the tapered surface b4 of the projecting portion b3 as shown in the figure.
- the mounting hole H of the first driven shaft 4d is provided with a receiving surface h1 (receiving portion) that comes into contact with the tapered surface b4 at the opening periphery (inlet periphery).
- the receiving surface h1 is a tapered surface that is linearly inclined with respect to the rotation axis L1.
- the receiving surface h1 is an annular surface that extends continuously around the rotation axis L1 with the rotation axis L1 as the center, and is reduced in diameter as the distance from the one end surface E increases.
- the inclination angle of the receiving surface h1 is equivalent to the inclination angle of the taper surface b4 of the tension bolt B.
- a female screw part h2 having a predetermined length is provided with a slight gap (first buffer part) interposed therebetween, and further on the inner side of the female screw part h2 (the innermost part).
- a complete screw portion h3 (second buffer portion) is formed.
- the first buffer portion and the second buffer portion are portions having shaft diameters slightly larger than the shaft diameter of the female screw portion h2.
- the tension bolt B is attached to the first driven shaft 4d by screwing the first male screw portion b1 of the tension bolt B with the female screw portion h2 of the first driven shaft 4d.
- the tension can be obtained only by screwing the first male screw portion b1 into the female screw portion h2.
- the bolt shaft center L3 of the bolt B is not coaxial with the rotation shaft center L1 of the first driven shaft 4d.
- the tension bolt B is provided with the tapered surface b4 and the first driven shaft 4d is provided with the receiving surface h1, the first male screw portion b1 is screwed into the female screw portion h2.
- the taper surface b4 and the receiving surface h1 are in contact with each other, and the bolt axis L3 of the tension bolt B is coaxial with the rotation axis L1 of the first driven shaft 4d. That is, the taper surface b4 of the tension bolt B and the receiving surface h1 have a third centering portion F3 that aligns (concentrizes) the rotation axis L1 and the axis of the tension bolt B (bolt axis L3). It is composed.
- the third centering portion F3 prevents the tension bolt B from falling.
- the tension bolt B attached coaxially to the first driven shaft 4d in this way is inserted into the through hole K so that the second male screw portion b2 of the tension bolt B is exposed from the first impeller 5a. Further, the first impeller 5a is attached to the first driven shaft 4d by screwing the nut N into the second male screw portion b2.
- the rotation axis L1 of the first driven shaft 4d and the axis L2 (impeller axis L2) of the first impeller 5a are made concentric, and the second core.
- the leading portion F2 prevents the first impeller 5a from collapsing, the bolt shaft center L3 of the tension bolt B and the impeller shaft center L2 of the first impeller 5a are concentric, and the third centering portion F3 allows the tension bolt B to The fall is prevented, and the rotation axis L1 and the bolt axis L3 of the tension bolt B are concentric.
- the nut N is screwed into the second male screw portion b2 in a state where the three members are concentric as described above, whereby the first impeller 5a is fixed to the first driven shaft 4d via the tension bolt B. .
- the tightening torque of the nut N is controlled so that a predetermined axial force is generated on the tension bolt B.
- the tightening depth of the first male threaded portion b1 of the tension bolt B with respect to the mounting hole H of the first driven shaft 4d that is, the direction of the rotational axis L1 (bolt axis L3).
- the positional relationship between the tension bolt B and the first male threaded portion b1 in FIG. 3B is such that the taper surface b4 of the tension bolt B and the receiving surface h1 of the first driven shaft 4d come into contact with each other.
- the male screw part b1 is regulated so as not to reach the incomplete screw part h3.
- the shaft diameter of the first male screw portion b1 is larger than the shaft diameter of the second male screw portion b2, so that the first male screw portion b1 is fastened when fastened to the female screw portion h2.
- the torque becomes larger than the tightening torque when the nut N is tightened to the second male screw portion b2.
- the tightening torque of the tension bolt B is set so that the axial force generated by the tightening torque is larger than the axial force generated by the tightening torque of the nut N, and the contact between the tension bolt B and the first driven shaft 4d. It is necessary to prevent the surface, that is, the tapered surface b4 and the receiving surface h1 from separating.
- the tapered surface b4 that is linearly inclined with respect to the bolt shaft center L3 is provided as the inclined surface.
- the inclined surface is limited to such a tapered surface b4.
- it may be a curved surface having a predetermined radius of curvature.
- a curved surface in a state of swelling with respect to the bolt axis L3 and a curved surface in a depressed state are preferable, but a curved surface in a swollen state is preferable.
- an impeller fastening structure according to a second embodiment of the present invention will be described with reference to FIGS. 2, 4A, and 4B.
- the first driven shaft (rotating shaft) 4d ′ of the first impeller 5a of the first rotor R1 ′ which is a rotating body composed of the first impeller 5a and the second impeller 6a in FIG.
- a fastening structure will be described. 4A and 4B, the same components as those in FIGS. 3A and 3B are denoted by the same reference numerals.
- the impeller fastening structure according to the second embodiment includes a protruding portion b3 ′ instead of the tension bolt B including the protruding portion b3 of the first embodiment described above.
- the tension bolt B ' is provided with a second bolt fitting surface b7 so as to be adjacent to one end side of the tension bolt B' with respect to the protruding portion b3 'in the direction of the bolt axis L3'.
- the second bolt fitting surface b7 is a cylindrical fitting surface that is concentric with the bolt axis L3 'and has a predetermined width in the direction of the bolt axis L3'.
- the first driven shaft 4d ' is employed instead of the first driven shaft 4d of the first embodiment.
- the first driven shaft 4d ' includes an attachment hole H' instead of the attachment hole H of the first embodiment.
- one end surface E orthogonal surface orthogonal to the rotation axis L1'
- the mounting hole H ′ is provided with a female screw portion h2 having a predetermined length at a position close to the one end surface E (receiving surface), and further, an incomplete screw portion h3 at the back (most innermost portion) of the female screw portion h2. Is formed. Further, on the other end side of the tension bolt B ′ with respect to the female screw portion h2, the opening peripheral edge (entrance peripheral edge) of the attachment hole H ′ is concentric with the rotational axis L1 ′ and the rotational axis L1 ′. A cylindrical fitting surface (second shaft fitting surface M2) having a predetermined width in the direction is formed.
- the second shaft fitting surface M2 is fitted with the above-described second bolt fitting surface b7, thereby concentrating the rotation shaft axis L1 'and the bolt shaft L3'.
- the second shaft fitting surface M2 and the second bolt fitting surface b7 constitute a third centering portion F3 (inlay).
- the third centering portion F3 prevents the tension bolt B 'from falling.
- the shaft diameter of the first male screw portion b1 is larger than the shaft diameter of the second male screw portion b2, so that the first male screw portion b1 is fastened when fastened to the female screw portion h2.
- the torque can be set larger than the tightening torque when tightening the nut N to the second male screw portion b2. Therefore, it is possible to prevent the tension bolt B 'from being rotated together with the nut N when the nut N is tightened to the second male screw portion b2.
- the tightening torque of the tension bolt B ′ is set so that the axial force generated by the tightening torque is larger than the axial force generated by the tightening torque of the nut N, and the tension bolt B ′ and the first driven shaft 4d ′ It is preferable that the abutting surface, that is, the orthogonal surface b6 and the one end surface E are not separated.
- FIGS. 5A and 5B As the impeller fastening structure according to the modification of the second embodiment, the structures shown in FIGS. 5A and 5B can be considered.
- the first driven shaft (rotating shaft) of the first impeller 5a of the first rotor R1 ′′ which is a rotating body composed of the first impeller 5a and the second impeller 6a in FIG.
- a fastening structure for 4d ′′ will be described.
- 5A and 5B the same components as those in FIGS. 3A and 3B are denoted by the same reference numerals.
- the impeller fastening structure according to the present modification employs a tension bolt B ′′ (stat bolt) having a protruding portion b3 ′′ instead of the protruding portion b3 ′ described above.
- the protruding portion b3 ′′ includes a protruding portion b8 whose outer peripheral portion protrudes toward the first male screw portion b1 in the direction of the bolt axis L3 ′′, and at the tip of the protruding portion b8 with respect to the bolt axis L3 ′′.
- An orthogonal plane b9 is provided.
- the orthogonal surface b9 is an annular surface continuously extending around the bolt axis L3 ′′ with the bolt axis L3 ′′ as the center. That is, the orthogonal surface b9 in the present modification is located at a position where the protruding portion b8 is present, that is, at a position farther from the bolt axis L3 ′′ (bolt axis L3 ′) than the orthogonal surface b6 of the second embodiment described above. 1 abuts against one end surface E (receiving surface) of the driven shaft 4d ′′.
- the first driven shaft 4d ′′ has a mounting hole H ′′ formed on one end surface E (receiving surface) by machining (drilling), the vicinity of the mounting hole H ′′ on the one end surface E (receiving surface) is the above-described machining.
- the orthogonal surface b9 of the tension bolt B ′′ is brought into contact with one end surface E (receiving surface) of the first driven shaft 4d ′′ at a position slightly away from the mounting hole H ′′.
- the tension bolt B ′′ is provided with a second bolt fitting surface b10 so as to be adjacent to the protruding portion b3 ′′ in the direction of the bolt axis L3 ′′.
- This second bolt fitting surface b10. Is a cylindrical fitting surface that is concentric with the bolt axis L3 ′′ and has a predetermined width in the direction of the bolt axis L3 ′′.
- the second shaft fitting surface M2 similar to the second embodiment is concentric with the rotary shaft axis L1 ′′ and the bolt shaft center L3 ′′ by fitting with the above-described second bolt fitting surface b10. To do.
- the second shaft fitting surface M2 and the second bolt fitting surface b10 constitute a third centering portion F3 (inlay), and the third centering portion F3 is a tension bolt B. ”To prevent the fall.
- the shaft diameter of the first male screw portion b1 is larger than the shaft diameter of the second male screw portion b2
- the tightening when the first male screw portion b1 is fastened to the female screw portion h2 is performed.
- the torque can be set larger than the tightening torque when tightening the nut N to the second male screw portion b2. Therefore, it is possible to prevent the tension bolt B ′′ from being rotated together with the nut N when the nut N is tightened to the second male screw portion b2.
- the tightening torque of the tension bolt B ′′ is generated by this tightening torque.
- the axial force is set to be larger than the axial force generated by the tightening torque of the nut N, and the contact surface between the tension bolt B ′′ and the first driven shaft 4d ′′, that is, the orthogonal surface b9 and the one end surface E are separated. It is preferable not to do so.
- the impeller fastening structure which concerns on 3rd Embodiment of this invention is demonstrated with reference to FIG. 6A and FIG. 6B.
- the first driven shaft (rotating shaft) 4d of the first impeller 5a of the first rotor R1 ′ ′′ which is a rotating body composed of the first impeller 5a and the second impeller 6a in FIG.
- the fastening structure for '' ' will be described.
- 6A and 6B the same components as those in FIGS. 3A and 3B are denoted by the same reference numerals.
- the protruding portion b3 ′ ′′ instead of the tension bolt B provided with the protruding portion b3 of the first embodiment described above, the protruding portion b3 ′ ′′.
- Tension bolt B '' '(Stat bolt) equipped with is adopted.
- the protruding portion b3 ′ ′′ does not include a surface that requires machining accuracy, such as the tapered surface b4 of the protruding portion b3 of the first embodiment and the orthogonal surface b6 of the protruding portion b3 ′ of the second embodiment.
- the tension bolt B ′ ′′ includes a second bolt fitting surface b11 on one end side of the tension bolt B ′ ′′ with respect to the projecting portion b3 ′ ′′ in the direction of the bolt axis L3 ′ ′′.
- the second bolt fitting surface b11 is a cylindrical fitting surface that is concentric with the bolt shaft center L3 "" and has a predetermined width in the direction of the bolt shaft center L3 "".
- a first male screw portion b1 of the tension bolt B ′ ′′ is provided on one end side of the tension bolt B ′ ′′ with respect to the second bolt fitting surface b11, and further than the first male screw portion b1.
- a third bolt fitting surface b12 is provided on one end side of the tension bolt B ′ ′′.
- the third bolt fitting surface b12 is also a cylindrical fitting surface that is concentric with the bolt shaft center L3 "" and has a predetermined width in the direction of the bolt shaft center L3 "".
- a cylindrical portion having a predetermined width in the direction of the bolt shaft center L3 ′ ′′ and concentric with the bolt shaft center L3 ′′ ′′ on one end side of the tension bolt B ′ ′′ from the third bolt fitting surface b12. b13 is provided, and an orthogonal surface b14 orthogonal to the bolt axis L3 ′ ′′ is provided at the tip of one end side of the tension bolt B ′ ′′ of the cylindrical portion b13.
- the first driven shaft 4d ′ ′′ is adopted instead of the first driven shaft 4d of the first embodiment.
- the first driven shaft 4d ′ ′′ includes a mounting hole H ′ ′′ in place of the mounting hole H of the first embodiment.
- the axis of rotation axis is located at a position advanced a predetermined distance from the one end surface E of the mounting hole H ′ ′′ to the back side of the mounting hole H ′ ′′.
- a cylindrical fitting surface (second shaft fitting surface M3) is formed concentrically with L1 ′ ′′ and having a predetermined width in the direction of the rotation axis L1 ′ ′′.
- the second shaft fitting surface M3 is fitted with the above-described second bolt fitting surface b11, thereby concentrating the rotation shaft axis L1 ′ ′′ and the bolt shaft L3 ′ ′′.
- the second shaft fitting surface M3 and the second bolt fitting surface b11 constitute a third centering portion F3 (inlay), and the third centering portion F3 is a tension bolt B. Prevent the fall of '''.
- a female screw portion h2 having a predetermined length that is screwed into the first male screw portion b1 is provided adjacent to the back side of the mounting hole H ′ ′′ from the second shaft fitting surface M3.
- a cylindrical fitting surface (first shape) that is concentric with the rotation axis L 1 ′ ′′ and has a predetermined width in the direction of the rotation axis L 1 ′ ′′.
- 3 shaft fitting surfaces M4 are formed.
- the third shaft fitting surface M4 is fitted with the above-described third bolt fitting surface b12, thereby concentrating the rotation shaft axis L1 "" and the bolt axis L3 "".
- the third shaft fitting surface M4 and the third bolt fitting surface b12 constitute an auxiliary third centering portion F3 ′ (inlay), and this auxiliary third centering surface.
- the part F3 ′ supplementarily prevents the tension bolt B ′ ′′ from collapsing.
- the one end surface E ′′ ′′ is a receiving surface (receiving portion) that contacts the orthogonal surface b ⁇ b> 14.
- the positional relationship between the tension bolt B ′ ′′ and the first driven shaft 4d ′ ′′ in the direction of the rotation axis L1 ′ ′′ is as shown in FIG.
- the orthogonal surface b14 of the tension bolt B ′ ′′ and the one end surface E ′ ′′ (receiving surface) of the first driven shaft 4d ′ ′′ come into contact with each other, whereby the tension bolt B ′ ′′
- the position in the direction of the bolt axis L3 ′ ′′ is restricted, and the first male screw portion b1 does not reach the incomplete screw portion h3.
- the tension bolt B ′ ′ is brought into contact with the orthogonal surface b14 of the tension bolt B ′ ′′ and one end surface E ′ ′′ (receiving surface) of the first driven shaft 4d ′ ′′.
- the projecting portion b3 ′ ′′ Since the position in the direction of the bolt axis L3 ′ ′′ is restricted, the projecting portion b3 ′ ′′ is not involved in the restriction of the position in the direction of the bolt axis L3 ′ ′′. As a result, the protruding portion b3 ′ ′′ can be formed with a small diameter, and as shown in FIG. 6B, the thickness of the hollow cylindrical portion T around the protruding portion b3 ′ ′′ can be increased, As a result, deformation of the hollow cylindrical portion T due to centrifugal force can be suppressed. Therefore, it can be said that the third embodiment is suitable when it is desired to suppress deformation due to the centrifugal force of the hollow cylindrical portion T of the first impeller 5a.
- the orthogonal surface b14 comes into contact with the one end surface E ′ ′′, so that a static frictional force is generated between the orthogonal surface b14 and the one end surface E ′ ′′. Therefore, it is possible to prevent the tension bolt B ′ ′′ from being rotated together with the nut N when the nut N is fastened to the second male screw portion b2. Therefore, the reproducibility of the assembly of the first rotor R1 ′′ ′ can be ensured.
- the second shaft fitting surface M3 and the second bolt fitting surface b11 constitute a third centering portion F3 (inlay), and the third shaft fitting.
- the surface M4 and the third bolt fitting surface b12 constitute an auxiliary third centering portion F3 ′ (inlay).
- only the third centering portion F3 may be provided.
- both the third centering portion F3 and the auxiliary third centering portion F3 ′ are provided, even if the tension bolt B ′ ′′ is long, the axis of rotation axis L1 ′ ′′ and the bolt axis L3 ′ ′′ can be concentric.
- a plurality of auxiliary third centering portions F3 ′ may be provided according to the length of the tension bolt B ′ ′′, for example. Further, in the tension bolt B ′ ′′, slight gaps S3 and S4 as shown in FIG. 6A are formed between the adjacent first male screw portion b1, the third bolt fitting surface b12, and the cylindrical portion b13. May be.
- the shape of the opening periphery of the mounting hole H ′ ′′ of the first driven shaft 4d ′ ′′ is such that the tension bolt B ′ ′′ is the first driven as shown in FIG. 6B.
- FIGS. 6A and 6B Although there is no particular limitation as long as it does not interfere with the protruding portion b3 ′ ′′ of the tension bolt B ′ ′′ when screwed to the shaft 4d ′ ′′, a tapered shape as shown in FIGS. 6A and 6B is preferable.
- the impeller fastening structure according to the present invention is applied to fastening the impeller and the rotary shaft in a turbo compressor having a four-stage configuration, but the present invention is not limited to this.
- the impeller fastening structure according to the present invention can be applied to various turbo compressors other than the four-stage configuration, or rotating machines other than the turbo compressor, for example, a supercharger.
- the stat bolt tension bolt
- the stop position of the stat bolt (tension bolt) with respect to the rotating shaft is stabilized, the reproducibility of the rotor assembly can be ensured.
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Abstract
Description
本願は、2014年3月26日に日本国に出願された特願2014-064179号に基づき優先権を主張し、その内容をここに援用する。
(1)回転軸に形成されたメネジにテンションボルトの第二オネジをねじ込む際に、テンションボルトが回転軸に対して傾いて取り付けられるため、ロータのアンバランスが過大となる可能性がある。これは、オネジとメネジよりなるネジ部に同軸度を出すことが難しいためである。
(2)メネジの終端部(最奥部)にてテンションボルトをトルク締めしているため、回転軸に対するテンションボルトの止まり位置(軸方向の位置)が安定せず、よってロータ組立の再現性を確保できない可能性がある。
本発明の第7の態様は、上記第1~第6のいずれかの態様のインペラ締結構造によって回転軸とインペラとが締結されたロータを備えるターボ圧縮機である。
本発明の第8の態様は、第1の軸心に沿った取付孔が一端に形成された回転軸と、第2の軸心に沿って貫通孔が形成されたインペラと、上記貫通孔に挿通され、一端が上記取付孔に螺合するスタットボルトと、上記スタットボルトの他端に螺合するナットとを備えるインペラ締結構造であって、上記スタットボルトは、上記一端側の先端に上記スタッドボルトの軸心である第3の軸心に直交する直交面を備え、上記回転軸は、上記取付孔の最奥部に上記第1の軸心に直交し上記直交面に当接する受け部を備えるインペラ締結構造である。
本発明の第9の態様は、上記第8の態様において、上記スタットボルトの上記一端は、上記スタットボルトの上記他端よりも軸径が大きい。
本発明の第10の態様は、上記8又は9の態様において、上記第2の軸心と上記第1の軸心とを揃える第1の芯出し部をさらに備える。
本発明の第11の態様は、上記第8~第10のいずれかの態様において、上記第2の軸心と上記第3の軸心とを揃える第2の芯出し部をさらに備える。
本発明の第12の態様は、上記第8~11のいずれかの態様において、上記第1の軸心と上記第3の軸心とを揃える第3の芯出し部をさらに備える。
本発明の第13の態様は、上記第12の態様において、上記第1の軸心と上記第3の軸心とを揃える補助的な第3の芯出し部をさらに備える。
本発明の第14の態様は、上記第8~13のいずれかの態様に記載のインペラ締結構造によって回転軸とインペラとが締結されたロータを備えるターボ圧縮機である。
すなわち、本発明によれば、スタットボルト(テンションボルト)が回転軸に対して傾いて取り付けられることを防止することができるので、ロータのアンバランスが過大となる可能性がない。
また、本発明によれば、回転軸に対するスタットボルト(テンションボルト)の止まり位置が安定するので、ロータ組立の再現性を確保できる。
すなわち、本変形例に係るインペラ締結構造は、上述した突設部b3’に代えて、突設部b3”を備えるテンションボルトB” (スタットボルト)を採用する。突設部b3”は、外周部がボルト軸心L3”の方向において第1雄ネジ部b1側に突出する突出部b8を備え、かつ、突出部b8の先端にボルト軸心L3”に対して直交する直交面b9を備える。
なお、テンションボルトB”には、ボルト軸心L3”の方向において突設部b3”に隣接するように第2のボルト嵌め合い面b10が設けられている。この第2のボルト嵌め合い面b10は、ボルト軸心L3”と同心かつボルト軸心L3”の方向に所定幅を有する円筒状の嵌め合い面である。
第2実施形態と同様の第2の軸嵌め合い面M2は、上述した第2のボルト嵌め合い面b10と嵌合することにより、回転軸軸心L1”とボルト軸心L3”とを同心化する。このような第2の軸嵌め合い面M2と第2のボルト嵌め合い面b10とは、第3の芯出し部F3(インロー)を構成し、この第3の芯出し部F3は、テンションボルトB”の倒れを防止する。
また、第2実施形態と同様に、第1雄ネジ部b1の軸径が第2雄ネジ部b2の軸径よりも大きいので、第1雄ネジ部b1を雌ネジ部h2に締め付ける際の締め付けトルクがナットNを第2雄ネジ部b2に締め付ける際の締め付けトルクよりも大きく設定することができる。したがって、ナットNを第2雄ネジ部b2に締め付ける際にテンションボルトB”がナットNと共に連れ回ることを防止することができる。なお、テンションボルトB”の締め付けトルクは、この締め付けトルクによって発生する軸力がナットNの締め付けトルクによって発生する軸力より大きくなるように設定され、テンションボルトB”と第1従動軸4d”との当接面、即ち、直交面b9と一端面Eとが離れないようにすることが好ましい。
この取付孔H’’’においては、図6Aに示すように、取付孔H’’’の一端面Eよりも取付孔H’’’の奥側に所定距離進んだ箇所に、回転軸軸心L1’’’と同心かつ回転軸軸心L1’’’の方向に所定幅を有する円筒状の嵌め合い面(第2の軸嵌め合い面M3)が形成されている。この第2の軸嵌め合い面M3は、上述した第2のボルト嵌め合い面b11と嵌合することにより、回転軸軸心L1’’’とボルト軸心L3’’’とを同心化する。このような第2の軸嵌め合い面M3と第2のボルト嵌め合い面b11とは、第3の芯出し部F3(インロー)を構成し、この第3の芯出し部F3は、テンションボルトB’’’の倒れを防止する。
また、一般的に、第1インペラ5aの第1従動軸4d’’’側の中空円柱部Tの肉厚が小さい場合、第1インペラ5aが高速で回転した際に、遠心力により中空円柱部Tが第1インペラ5aの半径方向に拡径する方向に変形する可能性がある。中空円柱部Tが第1インペラ5aの半径方向に拡径する方向に変形すると、結果として第1ロータR1’’’のアンバランスが増す可能性がある。本第3実施形態によれば、テンションボルトB’’’の直交面b14と第1従動軸4d’’’の一端面E’’’(受け面)とが当接することによって、テンションボルトB’’’のボルト軸心L3’’’の方向における位置を規制しているため、突設部b3’’’はボルト軸心L3’’’の方向における位置の規制に関与しない。その結果、突設部b3’’’を小径に形成することができ、図6Bに示すように、突設部b3’’’の周囲における中空円柱部Tの肉厚を大きくすることができ、結果として、遠心力による中空円柱部Tの変形を抑えることができる。従って、第1インペラ5aの中空円柱部Tの遠心力による変形を抑えたい場合には、本第3実施形態は適しているといえる。
また、このインペラ締結構造によれば、直交面b14が一端面E’’’に当接することで、直交面b14と一端面E’’’との間に静止摩擦力が発生する。したがって、ナットNを第2雄ネジ部b2に締め付ける際にテンションボルトB’’’がナットNと共に連れ回ることを防止することができる。そのため、第1ロータR1’’’の組立の再現性を確保できる。
また、テンションボルトB’’’において、隣接する第1雄ネジ部b1、第3のボルト嵌め合い面b12、円筒部b13の間には、図6Aに示すような若干の隙間S3,S4が形成されていても良い。
ここで、本第3実施形態においては、第1従動軸4d’’’の取付孔H’’’の開口周縁の形状は、図6Bに示すように、テンションボルトB’’’が第1従動軸4d’’’に螺合した際にテンションボルトB’’’の突設部b3’’’に干渉しない限りは特に制限はないが、図6A、図6Bに示すようなテーパ状が好ましい。
また、本発明によれば、回転軸に対するスタットボルト(テンションボルト)の止まり位置が安定するので、ロータ組立の再現性を確保できる。
Claims (13)
- 第1の軸心に沿った取付孔が一端に形成された回転軸と、第2の軸心に沿って貫通孔が形成されたインペラと、前記貫通孔に挿通され、一端が前記取付孔に螺合するスタットボルトと、前記スタットボルトの他端に螺合するナットとを備えるインペラ締結構造であって、
前記スタットボルトは、前記スタットボルトの軸心である第3の軸心方向の途中部位に半径方向に突出する突設部を備え、
前記回転軸は、前記取付孔の開口周縁に前記突設部に当接する受け部を備える
インペラ締結構造。 - 前記突設部は、前記第3の軸心に対して傾斜する傾斜面を備え、
前記受け部は、前記傾斜面に当接する受け面を備える請求項1記載のインペラ締結構造。 - 前記第2の軸心と前記第1の軸心とを揃える第1の芯出し部をさらに備え、
前記突設部は、前記第3の軸心に直交する直交面を備え、前記受け部は、前記直交面に当接する受け面を備える請求項1記載のインペラ締結構造。 - 前記スタットボルトの前記一端は、前記スタットボルトの前記他端よりも軸径が大きい請求項1~3のいずれか一項に記載のインペラ締結構造。
- 前記第2の軸心と前記第3の軸心とを揃える第2の芯出し部をさらに備える請求項1~4のいずれか一項に記載のインペラ締結構造。
- 前記第1の軸心と前記第3の軸心とを揃える第3の芯出し部をさらに備える請求項3~5のいずれか一項に記載のインペラ締結構造。
- 請求項1~6のいずれか一項に記載のインペラ締結構造によって回転軸とインペラとが締結されたロータを備えるターボ圧縮機。
- 第1の軸心に沿った取付孔が一端に形成された回転軸と、第2の軸心に沿って貫通孔が形成されたインペラと、前記貫通孔に挿通され、一端が前記取付孔に螺合するスタットボルトと、前記スタットボルトの他端に螺合するナットとを備えるインペラ締結構造であって、
前記スタットボルトは、前記一端側の先端に前記スタットボルトの軸心である第3の軸心に直交する直交面を備え、
前記回転軸は、前記取付孔の最奥部に前記第1の軸心に直交し前記直交面に当接する受け部を備えるインペラ締結構造。 - 前記第2の軸心と前記第1の軸心とを揃える第1の芯出し部をさらに備える請求項8記載のインペラ締結構造。
- 前記第2の軸心と前記第3の軸心とを揃える第2の芯出し部をさらに備える請求項8又は9に記載のインペラ締結構造。
- 前記第1の軸心と前記第3の軸心とを揃える第3の芯出し部をさらに備える請求項8~10のいずれか一項に記載のインペラ締結構造。
- 前記第1の軸心と前記第3の軸心とを揃える補助的な第3の芯出し部をさらに備える請求項11に記載のインペラ締結構造。
- 請求項8~12のいずれか一項に記載のインペラ締結構造によって回転軸とインペラとが締結されたロータを備えるターボ圧縮機。
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US (1) | US20160319832A1 (ja) |
EP (1) | EP3124792A4 (ja) |
JP (1) | JP6135821B2 (ja) |
KR (1) | KR101825509B1 (ja) |
CN (1) | CN106255829B (ja) |
WO (1) | WO2015146765A1 (ja) |
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WO2017094546A1 (ja) * | 2015-12-01 | 2017-06-08 | 株式会社Ihi | 取付構造、および、過給機 |
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US10830247B2 (en) * | 2018-08-17 | 2020-11-10 | Caterpillar Inc. | Remanufactured turbocharger shaft and method |
US10914231B2 (en) * | 2018-08-21 | 2021-02-09 | Ryan Harold SALENBIEN | Hub-less and nut-less turbine wheel and compressor wheel design for turbochargers |
US11598294B2 (en) | 2018-08-21 | 2023-03-07 | Apexturbo Llc | Hub-less and nut-less turbine wheel and compressor wheel designs and installation/removal tool |
CN109538622A (zh) * | 2018-12-27 | 2019-03-29 | 无锡市海星船舶动力有限公司 | 船舶用发动机叶轮轴总成 |
US11401942B2 (en) * | 2020-05-15 | 2022-08-02 | Garrett Transportation I Inc | Fastener arrangement for rotating group of turbomachine |
JP7561656B2 (ja) * | 2021-02-25 | 2024-10-04 | 三菱重工コンプレッサ株式会社 | 回転機械及び回転機械の組立方法 |
CN113580068A (zh) * | 2021-07-21 | 2021-11-02 | 福建福清核电有限公司 | 一种核电厂液环真空泵叶轮安装装置及方法 |
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Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2017094546A1 (ja) * | 2015-12-01 | 2017-06-08 | 株式会社Ihi | 取付構造、および、過給機 |
CN108350798A (zh) * | 2015-12-01 | 2018-07-31 | 株式会社Ihi | 安装构造以及增压器 |
JPWO2017094546A1 (ja) * | 2015-12-01 | 2018-09-13 | 株式会社Ihi | 取付構造、および、過給機 |
CN108350798B (zh) * | 2015-12-01 | 2020-05-26 | 株式会社Ihi | 安装构造以及增压器 |
US10753367B2 (en) | 2015-12-01 | 2020-08-25 | Ihi Corporation | Mounting structure and turbocharger |
Also Published As
Publication number | Publication date |
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EP3124792A4 (en) | 2017-11-15 |
US20160319832A1 (en) | 2016-11-03 |
CN106255829B (zh) | 2019-05-31 |
KR20160057476A (ko) | 2016-05-23 |
JP6135821B2 (ja) | 2017-05-31 |
CN106255829A (zh) | 2016-12-21 |
JPWO2015146765A1 (ja) | 2017-04-13 |
KR101825509B1 (ko) | 2018-02-05 |
EP3124792A1 (en) | 2017-02-01 |
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