US20190331115A1 - Screw Compressor - Google Patents
Screw Compressor Download PDFInfo
- Publication number
- US20190331115A1 US20190331115A1 US16/311,424 US201616311424A US2019331115A1 US 20190331115 A1 US20190331115 A1 US 20190331115A1 US 201616311424 A US201616311424 A US 201616311424A US 2019331115 A1 US2019331115 A1 US 2019331115A1
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- Prior art keywords
- rotor
- motor
- screw
- main unit
- shaft portion
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- Abandoned
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- 238000007906 compression Methods 0.000 claims abstract description 22
- 239000007788 liquid Substances 0.000 claims description 21
- 230000000694 effects Effects 0.000 description 9
- 230000004048 modification Effects 0.000 description 7
- 238000012986 modification Methods 0.000 description 7
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 7
- 230000008859 change Effects 0.000 description 4
- 230000009471 action Effects 0.000 description 3
- 238000005096 rolling process Methods 0.000 description 3
- 230000000052 comparative effect Effects 0.000 description 2
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000005549 size reduction Methods 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
- F04C29/02—Lubrication; Lubricant separation
- F04C29/026—Lubricant separation
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
- F04C18/08—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
- F04C18/12—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type
- F04C18/14—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons
- F04C18/16—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons with helical teeth, e.g. chevron-shaped, screw type
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
- F01C21/02—Arrangements of bearings
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C23/00—Combinations of two or more pumps, each being of rotary-piston or oscillating-piston type, specially adapted for elastic fluids; Pumping installations specially adapted for elastic fluids; Multi-stage pumps specially adapted for elastic fluids
- F04C23/02—Pumps characterised by combination with, or adaptation to, specific driving engines or motors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
- F04C29/0042—Driving elements, brakes, couplings, transmissions specially adapted for pumps
- F04C29/0085—Prime movers
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K21/00—Synchronous motors having permanent magnets; Synchronous generators having permanent magnets
- H02K21/12—Synchronous motors having permanent magnets; Synchronous generators having permanent magnets with stationary armatures and rotating magnets
- H02K21/24—Synchronous motors having permanent magnets; Synchronous generators having permanent magnets with stationary armatures and rotating magnets with magnets axially facing the armatures, e.g. hub-type cycle dynamos
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K5/00—Casings; Enclosures; Supports
- H02K5/04—Casings or enclosures characterised by the shape, form or construction thereof
- H02K5/16—Means for supporting bearings, e.g. insulating supports or means for fitting bearings in the bearing-shields
- H02K5/173—Means for supporting bearings, e.g. insulating supports or means for fitting bearings in the bearing-shields using bearings with rolling contact, e.g. ball bearings
- H02K5/1735—Means for supporting bearings, e.g. insulating supports or means for fitting bearings in the bearing-shields using bearings with rolling contact, e.g. ball bearings radially supporting the rotary shaft at only one end of the rotor
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
- H02K7/14—Structural association with mechanical loads, e.g. with hand-held machine tools or fans
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2210/00—Fluid
- F04C2210/10—Fluid working
- F04C2210/1005—Air
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2240/00—Components
- F04C2240/50—Bearings
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2240/00—Components
- F04C2240/50—Bearings
- F04C2240/56—Bearing bushings or details thereof
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2240/00—Components
- F04C2240/80—Other components
- F04C2240/809—Lubricant sump
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2270/00—Control; Monitoring or safety arrangements
- F04C2270/17—Tolerance; Play; Gap
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- 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
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2360/00—Engines or pumps
- F16C2360/43—Screw compressors
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K2205/00—Specific aspects not provided for in the other groups of this subclass relating to casings, enclosures, supports
- H02K2205/03—Machines characterised by thrust bearings
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K2213/00—Specific aspects, not otherwise provided for and not covered by codes H02K2201/00 - H02K2211/00
- H02K2213/03—Machines characterised by numerical values, ranges, mathematical expressions or similar information
Definitions
- the present invention relates generally to screw compressors including liquid-injected compressor main units and axial-gap motors that drive the compressor main units and, more particularly, to a screw compressor in which a screw rotor of a compressor main unit is coaxially connected with a rotary shaft of a motor.
- Patent Document 1 discloses a screw compressor including a liquid-injected compressor main unit and a radial-gap motor that drives the compressor main unit. The following details the screw compressor.
- the radial-gap motor includes a rotor shaft, a rotor mounted on the rotor shaft, and a stator spaced apart from the rotor in a radial direction.
- the rotor shaft is rotated by magnetic action of the stator and the rotor.
- the compressor main unit includes a pair of intermeshing male and female screw rotors.
- One of the screw rotors is coaxially connected with the rotor shaft of the motor. Rotation of the rotor shaft of the motor causes the one of the screw rotors to rotate, which, in turn, rotates the other of the screw rotors in mesh with the one of the screw rotors.
- compression chambers defined by tooth grooves of the screw rotors and an inner wall of a casing move in an axial direction.
- the compression chamber draws in gas via a suction port (opening) on one side in the axial direction and compresses the gas to thereby discharge the compressed gas via a discharge port (opening) on the other side in the axial direction.
- the liquid-injected compressor main unit injects a liquid into the compression chamber.
- the liquid injected in the compression chamber seals gaps in the compression chamber (specifically, a gap between the screw rotors and a gap between the screw rotor and the casing) and cools the compressed gas.
- the screw rotors each include a tooth portion having a plurality of spiral teeth, a suction-side shaft portion (motor-side shaft portion) connected with one side in the axial direction of the tooth portion (suction side, or the motor side), and a discharge-side shaft portion (opposite-side shaft portion) connected with the other side in the axial direction of the tooth portion (discharge side, or the side opposite to the motor).
- the suction-side shaft portion of one screw rotor is connected coaxially with the rotor shaft of the motor.
- each screw rotor is rotatably supported by a plurality of suction-side bearings.
- the discharge-side shaft portion of each screw rotor is rotatably supported by a plurality of discharge-side bearings.
- the discharge-side bearings are a plurality of angular ball bearings held at fixed positions inside the casing.
- the discharge-side bearings restrict axial movement of the discharge-side shaft portion of the screw rotor and bear a radial load and axial loads in both directions (specifically, a forward direction extending from the discharge side toward the suction side and a reverse direction extending from the suction side toward the discharge side).
- the suction-side bearings are a plurality of angular ball bearings held axially movably in the casing.
- the suction-side bearings permit axial movement of the suction-side shaft portion of the screw rotor and support the radial load and the axial load in the forward direction.
- Patent Document 1 JP-2004-150412-A (see FIGS. 1 to 3.)
- the axial-gap motor includes a rotor shaft, at least one rotor mounted on the rotor shaft, and at least one stator spaced apart from the rotor in the axial direction.
- the rotor shaft is rotated by magnetic action of the stator and the rotor.
- the suction-side shaft portion of one screw rotor may be connected coaxially with the rotor shaft of the axial-gap motor. Additionally, as in the configuration disclosed in Patent Document 1, the discharge-side bearings may restrict axial movement of the discharge-side shaft portion (opposite-side shaft portion) of the screw rotor and the suction-side bearings may permit axial movement of the suction-side shaft portion (motor-side shaft portion) of the screw rotor.
- the screw rotor expands by compression heat and the rotor shaft of the motor expands by heat generated by the motor.
- the restriction of the axial movement of the discharge-side shaft portion of the screw rotor can considerably reduce changes in the gap between a discharge-side end face of the tooth portion of the screw rotor and a wall surface of the casing. Performance of the compressor main unit can thereby be enhanced. Meanwhile, a gap between the rotor and the stator of the motor is affected by not only the thermal expansion of the rotor shaft of the motor, but also the thermal expansion of the screw rotor, resulting in large changes in the gap. Thus, performance of the motor is degraded.
- the present invention has been accomplished in light of such circumstances and one of the problems to be solved is to enhance performance of the compressor main unit and the motor by reducing changes in the gap between the discharge-side end face of the tooth portion of the screw rotor and the wall surface of the casing and in the gap between the rotor and the stator of the motor.
- the present invention includes a plurality of means for solving the problem.
- One exemplary aspect of the present invention provides a screw compressor including a liquid-injected compressor main unit that includes a screw rotor and compresses gas with injecting liquid in a compression chamber defined by a tooth groove of the screw rotor and an axial-gap motor that drives the compressor main unit.
- the screw rotor has a motor-side shaft portion connected coaxially with a rotor shaft of the motor.
- the screw compressor includes a bearing that rotatably supports the motor-side shaft portion of the screw rotor. In this screw compressor, the bearing restricts axial movement of the motor-side shaft portion and bears a radial load and axial loads in both directions.
- the aspect of the present invention can reduce changes in a gap between a discharge-side end face of a tooth portion of the screw rotor and a wall surface of a casing and in a gap between the rotor and the stator of the motor, to thereby enhance performance of the compressor main unit and the motor.
- FIG. 1 is a vertical cross-sectional view of a configuration of a screw compressor according to a first embodiment of the present invention, depicting a rated operation state of the compressor.
- FIG. 2 is a vertical cross-sectional view of a configuration of the screw compressor according to the first embodiment of the present invention, depicting a stationary state of the compressor.
- FIG. 3 is a vertical cross-sectional view of a configuration of a screw compressor according to a first modification of the present invention, depicting a stationary state of the compressor.
- FIG. 4 is a vertical cross-sectional view of a configuration of a screw compressor according to a second modification of the present invention, depicting a stationary state of the compressor.
- FIG. 5 is a vertical cross-sectional view of a configuration of a screw compressor according to a second embodiment of the present invention, depicting a rated operation state of the compressor.
- FIGS. 1 and 2 are vertical cross-sectional views of configurations of a screw compressor according to the present embodiment.
- FIG. 1 depicts a rated operation state (high temperature state) of the compressor.
- FIG. 2 depicts a stationary state (room temperature state) of the compressor.
- the screw compressor of the present embodiment includes an oil-injected compressor main unit 1 and a radial-gap motor 2 , which drives the compressor main unit 1 .
- the compressor main unit 1 is integrated with the motor 2 .
- the compressor main unit 1 and the motor 2 are disposed vertically such that screw rotors of the compressor main unit 1 and a rotor shaft of the motor 2 to be described later extend in the vertical direction.
- the motor 2 is disposed on the upper side of the compressor main unit 1 .
- the motor 2 includes a rotor shaft (shaft) 3 , a rotor 4 A, a rotor 4 B, a stator 5 , and a motor casing 6 .
- the rotor 4 A is mounted on an output side (side adjacent to the compressor main unit 1 ) of the rotor shaft 3 .
- the rotor 4 B is mounted on a non-output side (side opposite to the compressor main unit 1 ) of the rotor shaft 3 .
- the stator 5 is disposed between the rotors 4 A and 4 B so as to be spaced axially apart from the rotors 4 A and 4 B.
- the motor casing 6 houses thereinside the rotors 4 A and 4 B and the stator 5 and supports the stator 5 .
- the motor casing 6 includes a motor main casing and an end cover removably mounted in an upper end opening of the motor main casing.
- the rotors 4 A and 4 B are each a permanent magnet type rotor, for example.
- the stator 5 is a winding type stator, for example.
- the rotor shaft 3 is rotated by magnetic action of the rotors 4 A and 4 B and the stator 5 .
- the compressor main unit 1 includes a pair of intermeshing male and female screw rotors (specifically, a male rotor 7 and a female rotor not depicted) and a compressor main unit casing 8 , which houses thereinside the screw rotors. Tooth grooves in the screw rotors and an inner wall of the compressor main unit casing 8 define compression chambers 9 .
- the compressor main unit casing 8 includes a main casing 10 and a suction-side casing 11 , which is coupled with an upper side (suction side) of the main casing 10 .
- the suction-side casing 11 is coupled with the motor main casing.
- the male rotor 7 is coaxially connected with the rotor shaft 3 of the motor 2 .
- Rotation of the rotor shaft 3 of the motor 2 causes the male rotor 7 to rotate and the female rotor in mesh with the male rotor 7 to rotate.
- the rotation of the male rotor 7 and the female rotor causes the compression chamber 9 to move in the axial direction.
- the compression chamber 9 draws in air (gas) from a suction flow path 13 via a suction port 12 (opening) on one side in the axial direction (the side adjacent to the motor) and compresses the air to thereby discharge the compressed air (compressed gas) to a discharge flow path 15 via a discharge port 14 (opening) on the other side in the axial direction (the side opposite to the motor).
- the oil-injected (liquid-injected) compressor main unit 1 is configured to inject oil (liquid) into the compression chamber 9 on a suction stroke.
- the oil injected in the compression chamber 9 seals gaps in the compression chamber 9 (specifically, a gap between the male rotor 7 and the female rotor and a gap between the male rotor 7 or the female rotor and the casing 8 ) and cools the compressed air.
- the male rotor 7 includes a tooth portion 16 having a plurality of spiral teeth, a suction-side shaft portion (motor-side shaft portion) 17 connected with one side in the axial direction of the tooth portion 16 , and a discharge-side shaft portion (opposite-side shaft portion) 18 connected with the other side in the axial direction of the tooth portion 16 .
- the female rotor includes a tooth portion, a suction-side shaft portion, and a discharge-side shaft portion.
- the suction-side shaft portion 17 of the male rotor 7 is coaxially connected with the rotor shaft 3 of the motor 2 as described previously by being integrally molded with the rotor shaft 3 of the motor 2 .
- the tooth portion 16 of the male rotor 7 and the tooth portion of the female rotor are housed in a tooth portion housing chamber 19 of the main casing 10 .
- the discharge-side shaft portion 18 of the male rotor 7 and the discharge-side shaft portion of the female rotor are housed in the main casing 10 .
- the suction-side shaft portion 17 of the male rotor 7 and the suction-side shaft portion of the female rotor are housed in the suction-side casing 11 .
- the suction-side shaft portion 17 of the male rotor 7 is rotatably supported by a plurality of suction-side bearings 20 .
- the discharge-side shaft portion 18 of the male rotor 7 is rotatably supported by a single discharge-side bearing 21 .
- the suction-side bearings 20 are a plurality of angular ball bearings (specifically, combined angular contact ball bearings for face to face type or back to back type) and outer rings thereof are held at fixed positions in the suction-side casing 11 and inner rings thereof are fixed at fixed positions of the suction-side shaft portion 17 of the male rotor 7 .
- the suction-side bearings 20 restrict axial movement of the suction-side shaft portion 17 of the male rotor 7 and bear a radial load and axial loads in both directions (specifically, a forward direction extending from the discharge side toward the suction side and a reverse direction extending from the suction side toward the discharge side).
- the discharge-side bearing 21 is a cylindrical roller bearing (specifically, cylindrical roller bearing in which an outer ring or an inner ring has no flanges and the outer ring and the inner ring are axially movable relative to each other) and the outer ring thereof is held at a fixed position in the main casing 10 and the inner ring thereof is fixed at a fixed position of the discharge-side shaft portion 18 of the male rotor 7 .
- the discharge-side bearing 21 bears a radial load, while permitting axial movement of the discharge-side shaft portion 18 as a result of thermal expansion of the male rotor 7 .
- suction-side shaft portion of the female rotor is rotatably supported by suction-side bearings 20 .
- the discharge-side shaft portion of the female rotor is rotatably supported by discharge-side bearing 21 .
- the suction-side bearings 20 restrict axial movement of the suction-side shaft portion (motor-side shaft portion) of the male rotor 7 and the discharge-side bearing 21 permits axial movement of the discharge-side shaft portion 18 (opposite-side shaft portion) of the male rotor 7 .
- a gap between a discharge-side end face of the tooth portion 16 of the male rotor 7 and a wall surface of the casing 8 is affected by the thermal expansion of the male rotor 7 , but not by the thermal expansion of the rotor shaft 3 of the motor 2 . Changes can thus be reduced in the gap between the discharge-side end face of the tooth portion 16 of the male rotor 7 and the wall surface of the casing 8 .
- a gap between the rotor 4 A and the stator 5 and a gap between the rotor 4 B and the stator 5 are affected by the thermal expansion of the rotor shaft 3 of the motor 2 , but not the thermal expansion of the male rotor 7 .
- changes can be reduced in the gap between the rotor 4 A and the stator 5 and the gap between the rotor 4 B and the stator 5 .
- motor efficiency can be enhanced by setting dimensions of the foregoing gaps to optimum values and performance of the motor 2 can be improved.
- the present embodiment can have the discharge-side shaft portion 18 of the male rotor 7 and the discharge-side shaft portion of the female rotor shorter in length.
- the compressor main unit 1 can be reduced in size. Or, because a degree of freedom in design of the discharge flow path 15 is increased, performance of the compressor main unit 1 can be enhanced.
- a dimension D of the gap between the discharge-side end face of the tooth portion 16 of the male rotor 7 and the wall surface of the casing 8 under a rated operation state (at high temperature) of the compressor is given by expression ( 1 ) given below, where Do denotes a dimension of the gap between the discharge-side end face of the tooth portion 16 of the male rotor 7 and the wall surface of the casing 8 under a stationary state (at room temperature) of the compressor (Do>D).
- ⁇ Ls denotes an amount of thermal expansion of the tooth portion 16
- ⁇ Lb denotes an amount of thermal expansion of the tooth portion housing chamber 19 ( ⁇ Ls> ⁇ Lb).
- a dimension Ma of the gap between the rotor 4 A and the stator 5 under the rated operation state (at high temperature) of the compressor is given by expression (3) given below.
- Mao denotes a dimension of the gap between the rotor 4 A and the stator 5 under the stationary state (at room temperature) of the compressor
- ⁇ Ma denotes an amount of change in the dimension of the gap between the rotor 4 A and the stator 5 ( ⁇ Ma>0).
- a dimension Mb of the gap between the rotor 4 B and the stator 5 under the rated operation state (at high temperature) of the compressor is given by expression (4) given below.
- Mbo denotes a dimension of the gap between the rotor 4 B and the stator 5 under the stationary state (at room temperature) of the compressor
- ⁇ Mb denotes an amount of change in the dimension of the gap between the rotor 4 B and the stator 5 ( ⁇ Mb>0, ⁇ Mb ⁇ Ma).
- the axial-gap motor 2 includes the two rotors 4 A and 4 B and the one stator 5 disposed between the rotors 4 A and 4 B.
- This configuration is, however, illustrative only and not limiting and various changes may be made therein without departing from the spirit and scope of the invention.
- the axial-gap motor is only required to include at least one rotor and at least one stator disposed to be spaced apart from the rotor in the axial direction.
- an axial-gap motor 2 A may include a rotor 4 mounted on a rotor shaft, a stator 5 A disposed on an output side (side adjacent to a compressor main unit 1 ) with respect to the rotor 4 , and a stator 5 B disposed on a non-output side (side opposite to the compressor main unit 1 ) with respect to the rotor 4 . Effects identical to the effects achieved by the first embodiment can be achieved even in the modification.
- a dimension Mc of a gap between the rotor 4 and the stator 5 A under the rated operation state (at high temperature) of the compressor is given by expression (6) given below.
- Mco denotes a dimension of the gap between the rotor 4 and the stator 5 A under the stationary state (at room temperature) of the compressor
- ⁇ Mc denotes an amount of change in the dimension of the gap between the rotor 4 and the stator 5 A ( ⁇ Mc>0).
- Mc Mco+ ⁇ Mc (6)
- a dimension Md of a gap between the rotor 4 and the stator 5 B under the rated operation state (at high temperature) of the compressor is given by expression (7) given below.
- Mdo denotes a dimension of the gap between the rotor 4 and the stator 5 B under the stationary state (at room temperature) of the compressor
- ⁇ Md denotes an amount of change in the dimension of the gap between the rotor 4 and the stator 5 B ( ⁇ Md>0, ⁇ Mc ⁇ Md).
- the first embodiment has been described for an exemplary configuration in which the compressor main unit casing 8 includes the main casing 10 and the suction-side casing 11 , which is coupled with the upper side (suction side) of the main casing 10 .
- This configuration is, however, illustrative only and not limiting and various changes may be made therein without departing from the spirit and scope of the invention.
- a compressor main unit casing 8 may include a main casing 10 A, a suction-side casing 11 , which is coupled with an upper side (suction side) of the main casing 10 A, and a discharge-side casing 22 , which is coupled with a lower side (discharge side) of the main casing 10 A.
- the main casing 10 A may house the tooth portions of the screw rotors and the discharge-side casing 22 may house the discharge-side shaft portions of the screw rotors and the discharge-side bearings.
- machining accuracy of the discharge flow path 15 can be enhanced compared with the first embodiment.
- the compressor main unit 1 has been described as an oil-injected type to compress air with injecting oil in the compression chamber 9 .
- This configuration is, however, illustrative only and not limiting and various changes may be made therein without departing from the spirit and scope of the invention.
- the compressor main unit may, for example, be a water-injected type (liquid-injected type) to compress air (gas) with injecting water (liquid) in the compression chamber 9 .
- liquid-injected type liquid-injected type
- the screw compressor has been described for an exemplary configuration in which the screw rotors of the compressor main unit 1 and the rotor shaft 3 of the motor 2 extend in the vertical direction.
- This configuration is, however, illustrative only and not limiting and various changes may be made therein without departing from the spirit and scope of the invention.
- the screw compressor may be configured such that the screw rotors of the compressor main unit and the rotor shaft of the motor extend in the horizontal direction. The same effects as those described above can be achieved in this case, too.
- FIG. 5 is a vertical cross-sectional view of a configuration of a screw compressor according to the present embodiment of the present invention, depicting the rated operation state (high temperature state) of the compressor.
- like or corresponding parts are identified by the same reference numerals as those used in the first embodiment and descriptions for those parts will be omitted as appropriate.
- the screw compressor in the present embodiment includes an oil-injected compressor main unit 1 , an axial-gap motor 2 which drives the compressor main unit 1 , and an oil separator 23 (gas-liquid separator) which separates oil (liquid) from compressed air (compressed gas) discharged from the compressor main unit 1 .
- the compressor main unit 1 , the motor 2 , and the oil separator 23 are integrated with each other.
- the compressor main unit 1 and the motor 2 are disposed vertically such that screw rotors of the compressor main unit 1 and a rotor shaft 3 of the motor 2 extend in the vertical direction.
- the motor 2 is disposed on an upper side (suction side) of the compressor main unit 1 and the oil separator 23 is disposed on a lower side (discharge side) of the compressor main unit 1 .
- the oil separator 23 includes an inner tube 24 and an outer tube casing 26 .
- the inner tube 24 is disposed on a lower side of the compressor main unit 1 .
- the outer tube casing 26 is integrally molded with a compressor main unit casing 8 and forms a swirl flow path 25 between a lower portion of the compressor main unit 1 and the inner tube 24 .
- the swirl flow path 25 is connected with a discharge flow path 15 of the compressor main unit 1 .
- Compressed air discharged from the compressor main unit 1 is given a swirl in the swirl flow path 25 (see the arrow in FIG. 5 ), so that oil contained in the compressed air is centrifugally separated.
- the separated oil falls along the outer tube casing 26 and is collected in an oil storage portion 27 formed on a lower side of the outer tube casing 26 .
- the oil collected in the oil storage portion 27 is supplied to a compression chamber 9 on a suction stroke by way of a flow path not depicted. Meanwhile, the compressed air from which the oil has been separated flows into an inside of the inner tube 24 and flows out through a flow path not depicted.
- suction-side bearings 20 restrict axial movement of the suction-side shaft portion (motor-side shaft portion) of the screw rotor and a discharge-side bearing 21 permits axial movement of the discharge-side shaft portion (opposite-side shaft portion) of the screw rotor.
- changes are reduced in the gap between the discharge-side end face of the tooth portion of the screw rotor and the wall surface of the casing and in the gap between the rotor and the stator of the motor, so that performances of the compressor main unit 1 and of the motor 2 can be improved.
- discharge-side shaft portion of the screw rotor can be made shorter in length as in the first embodiment. This feature increases the degree of freedom in design of the discharge flow path 15 and the swirl flow path 25 , so that performance of the compressor main unit 1 and performance of the oil separator 23 can be improved.
- the screw compressor has been described as having a configuration including the oil-injected compressor main unit 1 , which compresses air with injecting oil in the compression chamber 9 , and the oil separator 23 , which separates oil from the compressed air discharged from the compressor main unit 1 .
- This configuration is, however, illustrative only and not limiting and various changes may be made therein without departing from the spirit and scope of the invention.
- the screw compressor may include, for example, a compressor main unit that is a water-injected type (liquid-injected type) and a water separator (gas-liquid separator).
- the compressor main unit compresses air (gas) with injecting water (liquid) in the compression chamber 9 .
- the water separator separates water from the compressed air (compressed gas) discharged from the compressor main unit.
- first and second embodiments have been described for a configuration in which a plurality of angular ball bearings (specifically, combined angular contact ball bearings for face to face type or back to back type) are employed as the suction-side bearings 20 , which rotatably support the suction-side shaft portion of each screw rotor.
- This configuration is, however, illustrative only and not limiting and various changes may be made therein without departing from the spirit and scope of the invention.
- any other type of rolling bearing may be employed when the suction-side bearings 20 restrict axial movement of the suction-side shaft portion of the screw rotor and support the radial load and the axial loads in both directions.
- a double-row angular ball bearing for face to face type or back to back type or a deep-groove ball bearing may be employed.
- a plurality of suction-side bearings that rotatably support the suction-side shaft portion of each screw rotor a plurality of tapered roller bearings (specifically, combined tapered roller bearings for face to face type or back to back type) may be employed.
- a double-row tapered roller bearing for face to face type or back to back type may be employed as one suction-side bearing that rotatably supports the suction-side shaft portion of each screw rotor.
- first and second embodiments have been described for a configuration in which a cylindrical roller bearing is employed as a single discharge-side bearing that rotatably supports the discharge-side shaft portion of each screw rotor.
- This configuration is, however, illustrative only and not limiting and various changes may be made therein without departing from the spirit and scope of the invention.
- any other type of rolling bearing may be employed when the discharge-side bearing permits axial movement of the discharge-side shaft portion of the screw rotor.
- the rolling bearing may be held in the casing movably in the axial direction.
- the first and second embodiments have been described for an exemplary configuration in which the rotor shaft 3 of the motor 2 is integrally molded with the suction-side shaft portion 17 of the male rotor 7 to thereby be coaxially connected therewith.
- This configuration is, however, illustrative only and not limiting and various changes may be made therein without departing from the spirit and scope of the invention.
- the rotor shaft 3 of the motor 2 may be coaxially connected with the suction-side shaft portion 17 of the male rotor 7 through a coupling.
- the rotor shaft 3 of the motor 2 may be coaxially connected with the suction-side shaft portion of the female rotor. In either case, the same effects as those described above can be achieved.
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Abstract
Description
- The present invention relates generally to screw compressors including liquid-injected compressor main units and axial-gap motors that drive the compressor main units and, more particularly, to a screw compressor in which a screw rotor of a compressor main unit is coaxially connected with a rotary shaft of a motor.
-
Patent Document 1 discloses a screw compressor including a liquid-injected compressor main unit and a radial-gap motor that drives the compressor main unit. The following details the screw compressor. - The radial-gap motor includes a rotor shaft, a rotor mounted on the rotor shaft, and a stator spaced apart from the rotor in a radial direction. The rotor shaft is rotated by magnetic action of the stator and the rotor.
- The compressor main unit includes a pair of intermeshing male and female screw rotors. One of the screw rotors is coaxially connected with the rotor shaft of the motor. Rotation of the rotor shaft of the motor causes the one of the screw rotors to rotate, which, in turn, rotates the other of the screw rotors in mesh with the one of the screw rotors. As the pair of screw rotors rotates, compression chambers defined by tooth grooves of the screw rotors and an inner wall of a casing move in an axial direction. The compression chamber draws in gas via a suction port (opening) on one side in the axial direction and compresses the gas to thereby discharge the compressed gas via a discharge port (opening) on the other side in the axial direction.
- The liquid-injected compressor main unit injects a liquid into the compression chamber. The liquid injected in the compression chamber seals gaps in the compression chamber (specifically, a gap between the screw rotors and a gap between the screw rotor and the casing) and cools the compressed gas.
- The screw rotors each include a tooth portion having a plurality of spiral teeth, a suction-side shaft portion (motor-side shaft portion) connected with one side in the axial direction of the tooth portion (suction side, or the motor side), and a discharge-side shaft portion (opposite-side shaft portion) connected with the other side in the axial direction of the tooth portion (discharge side, or the side opposite to the motor). As described previously, the suction-side shaft portion of one screw rotor is connected coaxially with the rotor shaft of the motor.
- The suction-side shaft portion of each screw rotor is rotatably supported by a plurality of suction-side bearings. The discharge-side shaft portion of each screw rotor is rotatably supported by a plurality of discharge-side bearings. The discharge-side bearings are a plurality of angular ball bearings held at fixed positions inside the casing. The discharge-side bearings restrict axial movement of the discharge-side shaft portion of the screw rotor and bear a radial load and axial loads in both directions (specifically, a forward direction extending from the discharge side toward the suction side and a reverse direction extending from the suction side toward the discharge side). The suction-side bearings are a plurality of angular ball bearings held axially movably in the casing. The suction-side bearings permit axial movement of the suction-side shaft portion of the screw rotor and support the radial load and the axial load in the forward direction.
- Patent Document 1: JP-2004-150412-A (see FIGS. 1 to 3.)
- For a reason of size reduction, for example, adoption of an axial-gap motor in place of the radial-gap motor described above is being studied. The axial-gap motor includes a rotor shaft, at least one rotor mounted on the rotor shaft, and at least one stator spaced apart from the rotor in the axial direction. The rotor shaft is rotated by magnetic action of the stator and the rotor.
- As in the configuration disclosed in
Patent Document 1, the suction-side shaft portion of one screw rotor may be connected coaxially with the rotor shaft of the axial-gap motor. Additionally, as in the configuration disclosed inPatent Document 1, the discharge-side bearings may restrict axial movement of the discharge-side shaft portion (opposite-side shaft portion) of the screw rotor and the suction-side bearings may permit axial movement of the suction-side shaft portion (motor-side shaft portion) of the screw rotor. The foregoing arrangements, however, pose the following problem. - The screw rotor expands by compression heat and the rotor shaft of the motor expands by heat generated by the motor. The restriction of the axial movement of the discharge-side shaft portion of the screw rotor can considerably reduce changes in the gap between a discharge-side end face of the tooth portion of the screw rotor and a wall surface of the casing. Performance of the compressor main unit can thereby be enhanced. Meanwhile, a gap between the rotor and the stator of the motor is affected by not only the thermal expansion of the rotor shaft of the motor, but also the thermal expansion of the screw rotor, resulting in large changes in the gap. Thus, performance of the motor is degraded.
- The present invention has been accomplished in light of such circumstances and one of the problems to be solved is to enhance performance of the compressor main unit and the motor by reducing changes in the gap between the discharge-side end face of the tooth portion of the screw rotor and the wall surface of the casing and in the gap between the rotor and the stator of the motor.
- To solve the foregoing problem, configurations defined in the scope of the claims are applied. The present invention includes a plurality of means for solving the problem. One exemplary aspect of the present invention provides a screw compressor including a liquid-injected compressor main unit that includes a screw rotor and compresses gas with injecting liquid in a compression chamber defined by a tooth groove of the screw rotor and an axial-gap motor that drives the compressor main unit. The screw rotor has a motor-side shaft portion connected coaxially with a rotor shaft of the motor. The screw compressor includes a bearing that rotatably supports the motor-side shaft portion of the screw rotor. In this screw compressor, the bearing restricts axial movement of the motor-side shaft portion and bears a radial load and axial loads in both directions.
- The aspect of the present invention can reduce changes in a gap between a discharge-side end face of a tooth portion of the screw rotor and a wall surface of a casing and in a gap between the rotor and the stator of the motor, to thereby enhance performance of the compressor main unit and the motor.
- Objects, configurations, and effects other than those described above will become apparent from the following description of embodiments.
-
FIG. 1 is a vertical cross-sectional view of a configuration of a screw compressor according to a first embodiment of the present invention, depicting a rated operation state of the compressor. -
FIG. 2 is a vertical cross-sectional view of a configuration of the screw compressor according to the first embodiment of the present invention, depicting a stationary state of the compressor. -
FIG. 3 is a vertical cross-sectional view of a configuration of a screw compressor according to a first modification of the present invention, depicting a stationary state of the compressor. -
FIG. 4 is a vertical cross-sectional view of a configuration of a screw compressor according to a second modification of the present invention, depicting a stationary state of the compressor. -
FIG. 5 is a vertical cross-sectional view of a configuration of a screw compressor according to a second embodiment of the present invention, depicting a rated operation state of the compressor. - A first embodiment of the present invention will be described with reference to
FIGS. 1 and 2 .FIGS. 1 and 2 are vertical cross-sectional views of configurations of a screw compressor according to the present embodiment.FIG. 1 depicts a rated operation state (high temperature state) of the compressor.FIG. 2 depicts a stationary state (room temperature state) of the compressor. - The screw compressor of the present embodiment includes an oil-injected compressor
main unit 1 and a radial-gap motor 2, which drives the compressormain unit 1. The compressormain unit 1 is integrated with themotor 2. Specifically, the compressormain unit 1 and themotor 2 are disposed vertically such that screw rotors of the compressormain unit 1 and a rotor shaft of themotor 2 to be described later extend in the vertical direction. Themotor 2 is disposed on the upper side of the compressormain unit 1. - The
motor 2 includes a rotor shaft (shaft) 3, arotor 4A, arotor 4B, astator 5, and amotor casing 6. Therotor 4A is mounted on an output side (side adjacent to the compressor main unit 1) of therotor shaft 3. Therotor 4B is mounted on a non-output side (side opposite to the compressor main unit 1) of therotor shaft 3. Thestator 5 is disposed between therotors rotors motor casing 6 houses thereinside therotors stator 5 and supports thestator 5. - As depicted in the figure, the
motor casing 6 includes a motor main casing and an end cover removably mounted in an upper end opening of the motor main casing. Therotors stator 5 is a winding type stator, for example. Therotor shaft 3 is rotated by magnetic action of therotors stator 5. - The compressor
main unit 1 includes a pair of intermeshing male and female screw rotors (specifically, amale rotor 7 and a female rotor not depicted) and a compressormain unit casing 8, which houses thereinside the screw rotors. Tooth grooves in the screw rotors and an inner wall of the compressormain unit casing 8 definecompression chambers 9. The compressormain unit casing 8 includes amain casing 10 and a suction-side casing 11, which is coupled with an upper side (suction side) of themain casing 10. The suction-side casing 11 is coupled with the motor main casing. - The
male rotor 7 is coaxially connected with therotor shaft 3 of themotor 2. Rotation of therotor shaft 3 of themotor 2 causes themale rotor 7 to rotate and the female rotor in mesh with themale rotor 7 to rotate. The rotation of themale rotor 7 and the female rotor causes thecompression chamber 9 to move in the axial direction. Thecompression chamber 9 draws in air (gas) from asuction flow path 13 via a suction port 12 (opening) on one side in the axial direction (the side adjacent to the motor) and compresses the air to thereby discharge the compressed air (compressed gas) to adischarge flow path 15 via a discharge port 14 (opening) on the other side in the axial direction (the side opposite to the motor). - The oil-injected (liquid-injected) compressor
main unit 1 is configured to inject oil (liquid) into thecompression chamber 9 on a suction stroke. The oil injected in thecompression chamber 9 seals gaps in the compression chamber 9 (specifically, a gap between themale rotor 7 and the female rotor and a gap between themale rotor 7 or the female rotor and the casing 8) and cools the compressed air. - The
male rotor 7 includes atooth portion 16 having a plurality of spiral teeth, a suction-side shaft portion (motor-side shaft portion) 17 connected with one side in the axial direction of thetooth portion 16, and a discharge-side shaft portion (opposite-side shaft portion) 18 connected with the other side in the axial direction of thetooth portion 16. Similarly, the female rotor includes a tooth portion, a suction-side shaft portion, and a discharge-side shaft portion. The suction-side shaft portion 17 of themale rotor 7 is coaxially connected with therotor shaft 3 of themotor 2 as described previously by being integrally molded with therotor shaft 3 of themotor 2. - The
tooth portion 16 of themale rotor 7 and the tooth portion of the female rotor are housed in a toothportion housing chamber 19 of themain casing 10. The discharge-side shaft portion 18 of themale rotor 7 and the discharge-side shaft portion of the female rotor are housed in themain casing 10. The suction-side shaft portion 17 of themale rotor 7 and the suction-side shaft portion of the female rotor are housed in the suction-side casing 11. - The suction-
side shaft portion 17 of themale rotor 7 is rotatably supported by a plurality of suction-side bearings 20. The discharge-side shaft portion 18 of themale rotor 7 is rotatably supported by a single discharge-side bearing 21. The suction-side bearings 20 are a plurality of angular ball bearings (specifically, combined angular contact ball bearings for face to face type or back to back type) and outer rings thereof are held at fixed positions in the suction-side casing 11 and inner rings thereof are fixed at fixed positions of the suction-side shaft portion 17 of themale rotor 7. The suction-side bearings 20 restrict axial movement of the suction-side shaft portion 17 of themale rotor 7 and bear a radial load and axial loads in both directions (specifically, a forward direction extending from the discharge side toward the suction side and a reverse direction extending from the suction side toward the discharge side). - The discharge-
side bearing 21 is a cylindrical roller bearing (specifically, cylindrical roller bearing in which an outer ring or an inner ring has no flanges and the outer ring and the inner ring are axially movable relative to each other) and the outer ring thereof is held at a fixed position in themain casing 10 and the inner ring thereof is fixed at a fixed position of the discharge-side shaft portion 18 of themale rotor 7. The discharge-side bearing 21 bears a radial load, while permitting axial movement of the discharge-side shaft portion 18 as a result of thermal expansion of themale rotor 7. - Similarly, the suction-side shaft portion of the female rotor is rotatably supported by suction-
side bearings 20. The discharge-side shaft portion of the female rotor is rotatably supported by discharge-side bearing 21. - Effects of the present embodiment will be described below.
- In the present embodiment, the suction-
side bearings 20 restrict axial movement of the suction-side shaft portion (motor-side shaft portion) of themale rotor 7 and the discharge-side bearing 21 permits axial movement of the discharge-side shaft portion 18 (opposite-side shaft portion) of themale rotor 7. Thus, a gap between a discharge-side end face of thetooth portion 16 of themale rotor 7 and a wall surface of thecasing 8 is affected by the thermal expansion of themale rotor 7, but not by the thermal expansion of therotor shaft 3 of themotor 2. Changes can thus be reduced in the gap between the discharge-side end face of thetooth portion 16 of themale rotor 7 and the wall surface of thecasing 8. Similarly, changes can also be reduced in a gap between a discharge-side end face of the tooth portion of the female rotor and a wall surface of thecasing 8. Thus, dimensions of the gaps described previously can be reduced to prevent leakage of compressed air and performance of the compressormain unit 1 can be enhanced. - A gap between the
rotor 4A and thestator 5 and a gap between therotor 4B and thestator 5 are affected by the thermal expansion of therotor shaft 3 of themotor 2, but not the thermal expansion of themale rotor 7. Thus, changes can be reduced in the gap between therotor 4A and thestator 5 and the gap between therotor 4B and thestator 5. Thus, motor efficiency can be enhanced by setting dimensions of the foregoing gaps to optimum values and performance of themotor 2 can be improved. - Consider a case, as a comparative example, in which axial movement of the discharge-side shaft portion of the male rotor or the discharge-side shaft portion of the female rotor is restricted by a plurality of angular ball bearings and axial movement of the suction-side shaft portion of the male rotor or the suction-side shaft portion of the female rotor is restricted by a single cylindrical roller bearing. As compared with such a comparative example, the present embodiment can have the discharge-
side shaft portion 18 of themale rotor 7 and the discharge-side shaft portion of the female rotor shorter in length. Thus, the compressormain unit 1 can be reduced in size. Or, because a degree of freedom in design of thedischarge flow path 15 is increased, performance of the compressormain unit 1 can be enhanced. - Dimensions of the gaps in the present embodiment will be described below.
- A dimension D of the gap between the discharge-side end face of the
tooth portion 16 of themale rotor 7 and the wall surface of thecasing 8 under a rated operation state (at high temperature) of the compressor is given by expression (1) given below, where Do denotes a dimension of the gap between the discharge-side end face of thetooth portion 16 of themale rotor 7 and the wall surface of thecasing 8 under a stationary state (at room temperature) of the compressor (Do>D). Where, ΔLs denotes an amount of thermal expansion of thetooth portion 16 and ΔLb denotes an amount of thermal expansion of the tooth portion housing chamber 19 (ΔLs>ΔLb). -
D=Do−(ΔLs−ΔLb) (1) - Because D>0, the dimension Do of the gap between the discharge-side end face of the
tooth portion 16 of themale rotor 7 and the wall surface of thecasing 8 under the stationary state (at room temperature) of the compressor is given by expression (2) given below. -
Do>ΔLs−ΔLb (2) - A dimension Ma of the gap between the
rotor 4A and thestator 5 under the rated operation state (at high temperature) of the compressor is given by expression (3) given below. Where, Mao denotes a dimension of the gap between therotor 4A and thestator 5 under the stationary state (at room temperature) of the compressor and ΔMa denotes an amount of change in the dimension of the gap between therotor 4A and the stator 5 (ΔMa>0). -
Ma=Mao−ΔMa (3) - A dimension Mb of the gap between the
rotor 4B and thestator 5 under the rated operation state (at high temperature) of the compressor is given by expression (4) given below. Where, Mbo denotes a dimension of the gap between therotor 4B and thestator 5 under the stationary state (at room temperature) of the compressor and ΔMb denotes an amount of change in the dimension of the gap between therotor 4B and the stator 5 (ΔMb>0, ΔMb≈ΔMa). -
Mb=Mbo+ΔMb (4) - Because preferably Ma≈Mb holds, preferably the relation of expression (5) given below holds.
-
Mao>Mbo (5) - The first embodiment has been described for an exemplary configuration in which the axial-
gap motor 2 includes the tworotors stator 5 disposed between therotors - Specifically, as in a first modification depicted in
FIG. 3 , for example, an axial-gap motor 2A may include arotor 4 mounted on a rotor shaft, astator 5A disposed on an output side (side adjacent to a compressor main unit 1) with respect to therotor 4, and astator 5B disposed on a non-output side (side opposite to the compressor main unit 1) with respect to therotor 4. Effects identical to the effects achieved by the first embodiment can be achieved even in the modification. - Dimensions of gaps in the present modification will be described. A dimension Mc of a gap between the
rotor 4 and thestator 5A under the rated operation state (at high temperature) of the compressor is given by expression (6) given below. Where, Mco denotes a dimension of the gap between therotor 4 and thestator 5A under the stationary state (at room temperature) of the compressor and ΔMc denotes an amount of change in the dimension of the gap between therotor 4 and thestator 5A (ΔMc>0). -
Mc=Mco+ΔMc (6) - A dimension Md of a gap between the
rotor 4 and thestator 5B under the rated operation state (at high temperature) of the compressor is given by expression (7) given below. Where, Mdo denotes a dimension of the gap between therotor 4 and thestator 5B under the stationary state (at room temperature) of the compressor and ΔMd denotes an amount of change in the dimension of the gap between therotor 4 and thestator 5B (ΔMd>0, ΔMc≈ΔMd). -
Md=Mdo−ΔMd (7) - Because preferably Mc≈Md holds, preferably the relation of expression (8) given below holds.
-
Mco<Mdo (8) - The first embodiment has been described for an exemplary configuration in which the compressor
main unit casing 8 includes themain casing 10 and the suction-side casing 11, which is coupled with the upper side (suction side) of themain casing 10. This configuration is, however, illustrative only and not limiting and various changes may be made therein without departing from the spirit and scope of the invention. - Specifically, as in a second modification depicted in
FIG. 4 , for example, a compressormain unit casing 8 may include amain casing 10A, a suction-side casing 11, which is coupled with an upper side (suction side) of themain casing 10A, and a discharge-side casing 22, which is coupled with a lower side (discharge side) of themain casing 10A. Then, themain casing 10A may house the tooth portions of the screw rotors and the discharge-side casing 22 may house the discharge-side shaft portions of the screw rotors and the discharge-side bearings. In such a modification, machining accuracy of thedischarge flow path 15 can be enhanced compared with the first embodiment. - Additionally, in the first embodiment, the compressor
main unit 1 has been described as an oil-injected type to compress air with injecting oil in thecompression chamber 9. This configuration is, however, illustrative only and not limiting and various changes may be made therein without departing from the spirit and scope of the invention. Specifically, the compressor main unit may, for example, be a water-injected type (liquid-injected type) to compress air (gas) with injecting water (liquid) in thecompression chamber 9. The same effects as those described above can be achieved in this case, too. - In the first embodiment, the screw compressor has been described for an exemplary configuration in which the screw rotors of the compressor
main unit 1 and therotor shaft 3 of themotor 2 extend in the vertical direction. This configuration is, however, illustrative only and not limiting and various changes may be made therein without departing from the spirit and scope of the invention. Specifically, the screw compressor may be configured such that the screw rotors of the compressor main unit and the rotor shaft of the motor extend in the horizontal direction. The same effects as those described above can be achieved in this case, too. - A second embodiment of the present invention will be described below with reference to
FIG. 5 .FIG. 5 is a vertical cross-sectional view of a configuration of a screw compressor according to the present embodiment of the present invention, depicting the rated operation state (high temperature state) of the compressor. In the present embodiment, like or corresponding parts are identified by the same reference numerals as those used in the first embodiment and descriptions for those parts will be omitted as appropriate. - The screw compressor in the present embodiment includes an oil-injected compressor
main unit 1, an axial-gap motor 2 which drives the compressormain unit 1, and an oil separator 23 (gas-liquid separator) which separates oil (liquid) from compressed air (compressed gas) discharged from the compressormain unit 1. The compressormain unit 1, themotor 2, and theoil separator 23 are integrated with each other. Specifically, the compressormain unit 1 and themotor 2 are disposed vertically such that screw rotors of the compressormain unit 1 and arotor shaft 3 of themotor 2 extend in the vertical direction. Themotor 2 is disposed on an upper side (suction side) of the compressormain unit 1 and theoil separator 23 is disposed on a lower side (discharge side) of the compressormain unit 1. - The
oil separator 23 includes aninner tube 24 and anouter tube casing 26. Theinner tube 24 is disposed on a lower side of the compressormain unit 1. Theouter tube casing 26 is integrally molded with a compressormain unit casing 8 and forms aswirl flow path 25 between a lower portion of the compressormain unit 1 and theinner tube 24. Theswirl flow path 25 is connected with adischarge flow path 15 of the compressormain unit 1. - Compressed air discharged from the compressor
main unit 1 is given a swirl in the swirl flow path 25 (see the arrow inFIG. 5 ), so that oil contained in the compressed air is centrifugally separated. The separated oil falls along theouter tube casing 26 and is collected in anoil storage portion 27 formed on a lower side of theouter tube casing 26. The oil collected in theoil storage portion 27 is supplied to acompression chamber 9 on a suction stroke by way of a flow path not depicted. Meanwhile, the compressed air from which the oil has been separated flows into an inside of theinner tube 24 and flows out through a flow path not depicted. - As in the first embodiment, in the present embodiment, too, suction-
side bearings 20 restrict axial movement of the suction-side shaft portion (motor-side shaft portion) of the screw rotor and a discharge-side bearing 21 permits axial movement of the discharge-side shaft portion (opposite-side shaft portion) of the screw rotor. Thus, changes are reduced in the gap between the discharge-side end face of the tooth portion of the screw rotor and the wall surface of the casing and in the gap between the rotor and the stator of the motor, so that performances of the compressormain unit 1 and of themotor 2 can be improved. - Additionally, the discharge-side shaft portion of the screw rotor can be made shorter in length as in the first embodiment. This feature increases the degree of freedom in design of the
discharge flow path 15 and theswirl flow path 25, so that performance of the compressormain unit 1 and performance of theoil separator 23 can be improved. - It is noted that, in the second embodiment, the screw compressor has been described as having a configuration including the oil-injected compressor
main unit 1, which compresses air with injecting oil in thecompression chamber 9, and theoil separator 23, which separates oil from the compressed air discharged from the compressormain unit 1. This configuration is, however, illustrative only and not limiting and various changes may be made therein without departing from the spirit and scope of the invention. Specifically, the screw compressor may include, for example, a compressor main unit that is a water-injected type (liquid-injected type) and a water separator (gas-liquid separator). The compressor main unit compresses air (gas) with injecting water (liquid) in thecompression chamber 9. The water separator separates water from the compressed air (compressed gas) discharged from the compressor main unit. The same effects as those described above can be achieved in this case, too. - Additionally, the first and second embodiments have been described for a configuration in which a plurality of angular ball bearings (specifically, combined angular contact ball bearings for face to face type or back to back type) are employed as the suction-
side bearings 20, which rotatably support the suction-side shaft portion of each screw rotor. This configuration is, however, illustrative only and not limiting and various changes may be made therein without departing from the spirit and scope of the invention. Specifically, any other type of rolling bearing may be employed when the suction-side bearings 20 restrict axial movement of the suction-side shaft portion of the screw rotor and support the radial load and the axial loads in both directions. - Specifically, as one suction-side bearing that rotatably supports the suction-side shaft portion of each screw rotor, a double-row angular ball bearing for face to face type or back to back type or a deep-groove ball bearing may be employed. Or, as a plurality of suction-side bearings that rotatably support the suction-side shaft portion of each screw rotor, a plurality of tapered roller bearings (specifically, combined tapered roller bearings for face to face type or back to back type) may be employed. Alternatively, as one suction-side bearing that rotatably supports the suction-side shaft portion of each screw rotor, a double-row tapered roller bearing for face to face type or back to back type may be employed.
- Additionally, the first and second embodiments have been described for a configuration in which a cylindrical roller bearing is employed as a single discharge-side bearing that rotatably supports the discharge-side shaft portion of each screw rotor. This configuration is, however, illustrative only and not limiting and various changes may be made therein without departing from the spirit and scope of the invention. Specifically, any other type of rolling bearing may be employed when the discharge-side bearing permits axial movement of the discharge-side shaft portion of the screw rotor. Specifically, the rolling bearing may be held in the casing movably in the axial direction.
- Additionally, the first and second embodiments have been described for an exemplary configuration in which the
rotor shaft 3 of themotor 2 is integrally molded with the suction-side shaft portion 17 of themale rotor 7 to thereby be coaxially connected therewith. This configuration is, however, illustrative only and not limiting and various changes may be made therein without departing from the spirit and scope of the invention. Specifically, therotor shaft 3 of themotor 2 may be coaxially connected with the suction-side shaft portion 17 of themale rotor 7 through a coupling. Alternatively, therotor shaft 3 of themotor 2 may be coaxially connected with the suction-side shaft portion of the female rotor. In either case, the same effects as those described above can be achieved. - 1 Compressor main unit
- 2, 2A Motor
- 3 Rotor shaft
- 4, 4A, 4B Rotor
- 5, 5A, 5B Stator
- 7 Male rotor (Screw rotor)
- 8 Compressor main unit casing
- 9 Compression chamber
- 11 Suction-side casing
- 12 Suction port
- 14 Discharge port
- 17 Suction-side shaft portion (Motor-side shaft portion)
- 20 Suction-side bearing
- 23 Oil separator (Gas-liquid separator)
Claims (6)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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PCT/JP2016/069749 WO2018008054A1 (en) | 2016-07-04 | 2016-07-04 | Screw compressor |
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US20190331115A1 true US20190331115A1 (en) | 2019-10-31 |
Family
ID=60901603
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US16/311,424 Abandoned US20190331115A1 (en) | 2016-07-04 | 2016-07-04 | Screw Compressor |
Country Status (5)
Country | Link |
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US (1) | US20190331115A1 (en) |
EP (1) | EP3480469B1 (en) |
JP (1) | JP6756827B2 (en) |
CN (1) | CN109312741B (en) |
WO (1) | WO2018008054A1 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
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BE1027881B1 (en) * | 2019-12-18 | 2021-07-27 | Atlas Copco Airpower Nv | Compressor device and device equipped with a bearing damper |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS52139413U (en) * | 1976-04-07 | 1977-10-22 | ||
JPS59215986A (en) * | 1983-05-20 | 1984-12-05 | Ebara Corp | Screw compressor |
JP2616922B2 (en) * | 1987-05-22 | 1997-06-04 | 株式会社日立製作所 | Screw compressor |
JPH0579514A (en) * | 1991-09-20 | 1993-03-30 | Hitachi Ltd | Bearing construction and screw fluid machine therewith |
JPH11107951A (en) * | 1997-10-01 | 1999-04-20 | Td Giken:Kk | Postive displacement type pump |
DE29904411U1 (en) * | 1999-03-10 | 2000-07-20 | GHH-RAND Schraubenkompressoren GmbH & Co. KG, 46145 Oberhausen | Screw compressor |
JP3796210B2 (en) * | 2002-11-01 | 2006-07-12 | 株式会社神戸製鋼所 | Screw compressor |
JP4586599B2 (en) * | 2005-03-25 | 2010-11-24 | ダイキン工業株式会社 | Compressor |
JP4618050B2 (en) * | 2005-08-29 | 2011-01-26 | ダイキン工業株式会社 | Compressor |
FI20050866A0 (en) * | 2005-08-31 | 2005-08-31 | Axco Motors Oy | Unit cooling system |
JP4816358B2 (en) * | 2006-09-19 | 2011-11-16 | ダイキン工業株式会社 | Motor and compressor |
JP4835384B2 (en) * | 2006-10-26 | 2011-12-14 | ダイキン工業株式会社 | Compressor |
JP4394115B2 (en) * | 2006-12-26 | 2010-01-06 | 本田技研工業株式会社 | Axial gap type motor |
GB201107451D0 (en) * | 2011-05-05 | 2011-06-15 | Howden Compressors Ltd | Fluid machine |
BE1020312A3 (en) * | 2012-02-28 | 2013-07-02 | Atlas Copco Airpower Nv | COMPRESSOR DEVICE, AS WELL AS USE OF SUCH SET-UP. |
JP6292910B2 (en) * | 2014-02-05 | 2018-03-14 | 株式会社日立産機システム | Liquid supply type compressor and gas-liquid separator |
WO2016157448A1 (en) * | 2015-03-31 | 2016-10-06 | 株式会社日立産機システム | Motor-integrated compressor |
WO2016157447A1 (en) * | 2015-03-31 | 2016-10-06 | 株式会社日立産機システム | Screw compressor |
-
2016
- 2016-07-04 JP JP2018525831A patent/JP6756827B2/en active Active
- 2016-07-04 US US16/311,424 patent/US20190331115A1/en not_active Abandoned
- 2016-07-04 CN CN201680086958.4A patent/CN109312741B/en active Active
- 2016-07-04 EP EP16908098.3A patent/EP3480469B1/en active Active
- 2016-07-04 WO PCT/JP2016/069749 patent/WO2018008054A1/en unknown
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EP3480469A1 (en) | 2019-05-08 |
WO2018008054A1 (en) | 2018-01-11 |
CN109312741B (en) | 2022-04-05 |
CN109312741A (en) | 2019-02-05 |
EP3480469B1 (en) | 2022-12-21 |
EP3480469A4 (en) | 2020-01-29 |
JP6756827B2 (en) | 2020-09-16 |
JPWO2018008054A1 (en) | 2019-04-04 |
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