WO2011114716A1 - 軸流圧縮機 - Google Patents
軸流圧縮機 Download PDFInfo
- Publication number
- WO2011114716A1 WO2011114716A1 PCT/JP2011/001513 JP2011001513W WO2011114716A1 WO 2011114716 A1 WO2011114716 A1 WO 2011114716A1 JP 2011001513 W JP2011001513 W JP 2011001513W WO 2011114716 A1 WO2011114716 A1 WO 2011114716A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- electric motor
- shaft
- working fluid
- drive shaft
- compression
- Prior art date
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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
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/54—Fluid-guiding means, e.g. diffusers
- F04D29/541—Specially adapted for elastic fluid pumps
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D19/00—Axial-flow pumps
- F04D19/02—Multi-stage pumps
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D25/00—Pumping installations or systems
- F04D25/02—Units comprising pumps and their driving means
- F04D25/06—Units comprising pumps and their driving means the pump being electrically driven
- F04D25/0606—Units comprising pumps and their driving means the pump being electrically driven the electric motor being specially adapted for integration in the pump
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/05—Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps
- F04D29/053—Shafts
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/54—Fluid-guiding means, e.g. diffusers
- F04D29/56—Fluid-guiding means, e.g. diffusers adjustable
- F04D29/563—Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
- F04D29/668—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps damping or preventing mechanical vibrations
Definitions
- the present invention relates to an axial flow compressor.
- a compressor having a speed increasing mechanism is known.
- a speed increasing mechanism is interposed between the drive shaft of the electric motor and the main shaft of the compression unit, and the compression unit is driven at a rotational speed greater than the rotational speed of the electric motor.
- a compression part can be driven at high speed, making the rotation speed of an electric motor low speed.
- the compression section is provided with a diffuser extending in the radial direction. For this reason, the speed of the pressurized working fluid is reduced by the diffuser while being increased by the action of the impeller of the compression unit. This compressor discharges the working fluid decelerated to a predetermined speed by the diffuser.
- the compressor disclosed in Patent Document 1 has a problem that there is a limit to downsizing.
- this compressor is provided with a speed increasing mechanism, but the speed increasing mechanism is provided on the rotating shaft of the electric motor so as to increase the rotational speed of the main shaft of the compression unit relative to the rotational speed of the driving shaft of the electric motor.
- the diameter of the first gear must be large, and the electric motor is offset with respect to the compression portion so that the first gear meshes with the second gear provided on the main shaft of the compression portion. Must. For this reason, there exists a problem that the radial width of a compression part will become large.
- the diffuser is provided in the compression part and this diffuser extends in the radial direction with respect to the impeller, there is a problem in that the radial width of the compression part also increases in this respect.
- An object of the present invention is to provide an axial compressor that solves the above problems.
- an object of the present invention is to reduce the size of the axial compressor while having a configuration in which the working fluid discharged from the compression unit is decelerated to a predetermined flow velocity.
- An axial-flow compressor is an axial-flow compressor for compressing a working fluid, and is connected to an electric motor having a rotating shaft without being connected to the rotating shaft of the electric motor via a speed increaser.
- a compressor having a drive shaft and a rotor that rotates integrally with the drive shaft, and compressing the working fluid by driving the drive shaft, and a flow velocity of the working fluid discharged from the discharge port of the compressor
- a reduction part having a space for reducing the motor, the rotating shaft of the electric motor is connected to the end of the drive shaft on the discharge port side, and the reduction part is arranged so as to surround the electric motor Yes.
- the axial flow compressor 10 is configured as a compressor provided in a refrigerator, and is provided in a refrigerant circuit 14 having an evaporator 12 and a condenser 13. Yes.
- the axial flow compressor 10 compresses water vapor as a working fluid (refrigerant) evaporated by the evaporator 12. This water vapor is a relatively low temperature, low pressure water vapor.
- the water vapor that is the working fluid compressed by the axial compressor 10 of the present embodiment has a temperature of 150 ° C. or less at a discharge pressure of the axial compressor 10, for example, at a pressure below atmospheric pressure.
- the working fluid compressed by the axial flow compressor 10 is sent to the condenser 13 and condensed in the condenser 13.
- the working fluid circulates through the refrigerant circuit 14 with a phase change.
- cold heat can be supplied to the secondary heat medium.
- This secondary heat medium is supplied to a utilization side device (not shown) to cool indoor air or the like as a cooling target.
- the axial flow compressor 10 includes a compression unit 20 having a compression space CS for compressing the working fluid, an electric motor 22 for driving the compression unit 20, and a flow rate of the working fluid discharged from the compression space CS. And a speed reduction unit 24.
- the casing 26 of the axial flow compressor 10 includes a cylindrical first case portion 27 disposed in the compression portion 20, a second case portion 28 disposed on one end side (upstream side) of the compression portion 20, and a compression portion. And a third case portion 29 disposed in the speed reduction portion 24 which is the other end side (downstream side) of 20.
- the compression unit 20 includes a first case portion 27 and a rotor 31 disposed in the first case portion 27.
- a space between the first case portion 27 and the rotor 31 functions as a compression space CS for compressing the working fluid.
- the compression space CS has a suction port CS1 on the left side in FIG. 1 and a discharge port CS2 on the right side. Therefore, the working fluid evaporated in the evaporator 12 is sucked into the compression space CS through the left suction port CS1 in FIG. 1, and this working fluid is compressed as it moves in the compression space CS from the left to the right in FIG. It is discharged from the discharge port CS2.
- a plurality of stationary blades 33 are fixed to the inner peripheral surface of the first case portion 27, and the stationary blades 33 are arranged at intervals in the axial direction.
- the first case portion 27 is installed such that the axial direction is horizontal.
- the rotor 31 includes a plurality of moving blades 34 and a plurality of spacers 35.
- the plurality of moving blades 34 are arranged at intervals in the axial direction so as to be alternately located with the stationary blades 33.
- the spacer 35 is a member formed in a cylindrical shape, and the spacer 35 is disposed on the inner side in the radial direction of the stationary blade 33 and is disposed between the adjacent moving blades 34 and 34. In the illustrated example, a configuration in which four moving blades 34 and four spacers 35 are provided is shown, but the present invention is not limited to this.
- the moving blade 34 includes a cylindrical boss portion 37 and a wing portion 38 integrally formed around the boss portion 37.
- each of the moving blades 34 is made of aluminum or an aluminum alloy, and is an integrally molded product formed by cutting out from one material.
- a plurality of wing portions 38 are formed in the circumferential direction of the boss portion 37.
- the outer peripheral surface and inner peripheral surface of the boss portion 37 are flush with the outer peripheral surface and inner peripheral surface of the spacer 35.
- the compression unit 20 includes a drive shaft 40, a first pressing member 41, a second pressing member 42, a nut 43 as an example of a fixing unit, and a disk-shaped member 44.
- the drive shaft 40 includes a rotor shaft portion 46 and two end shaft portions 47 and 47 disposed at both ends of the rotor shaft portion 46, respectively.
- the rotor shaft portion 46 is disposed on the axial center of the first case portion 27 and extends along the axial direction of the first case portion 27. Both end portions of the rotor shaft portion 46 are located outside the rotor blades 34 and the spacers 35 in the axial direction. Male screw portions (not shown) are provided at both ends of the rotor shaft portion 46, respectively.
- the first pressing member 41 is disposed so as to contact the uppermost-stage moving blade 34, and the second pressing member 42 is disposed so as to contact the spacer 35 positioned outside the most downstream-stage moving blade 34.
- the first pressing member 41 and the second pressing member 42 are members having the same configuration, but are disposed in opposite directions in the axial direction.
- the first pressing member 41 is formed in a disc shape, and the pressing members 41 and 42 are formed with a central through hole through which the rotor shaft portion 46 is inserted.
- the axial center of the first pressing member 41 and the axial center of the uppermost moving blade 34 coincide with each other.
- the end shaft portion (first end shaft portion) 47 to the first pressing member 41 with a bolt, the end shaft portion 47 and the first pressing member 41 become coaxial.
- the second presser member 42 is fitted to a spacer 35 located outside the rotor blade 34 at the most downstream stage. Thereby, the axial center of the 2nd pressing member 42 and the axial center of the spacer 35 located in the most downstream side correspond. Then, the end shaft portion (second end shaft portion) 47 is fixed to the second pressing member 42 with a bolt, so that the end shaft portion 47 and the second pressing member 42 are coaxial.
- the nut 43 is screwed into the male screw portion of the rotor shaft portion 46 inserted through the central through hole, so that the space between the first presser member 41 and the second presser member 42 is reached.
- the first pressing member 41 and the second pressing member 42 can be clamped from both sides in the axial direction by the nut 43 in a state where the rotor 31 (the moving blade 34 and the spacer 35) is sandwiched therebetween.
- the first pressing member 41 and the second pressing member 42 are tightened with a predetermined torque value.
- the “predetermined torque value” referred to here is based on the difference in the linear expansion coefficient between the rotor 31 and the rotor shaft portion 46, and further on the difference in the amount of expansion during driving of the rotor 31 as will be described later. It is determined in consideration that the coupling force by the nut 43 increases during driving rather than during assembly. Thereby, the moving blade 34 and the spacer 35 adjacent to each other are fitted to each other.
- the inner diameters of the spacer 35 and the boss part 37 are sufficiently larger than the outer diameter of the rotor shaft part 46. For this reason, a space extending in the axial direction is formed between the cylindrical portion formed by connecting the spacer 35 and the boss portion 37 and the rotor shaft portion 46. In this space, that is, the inner space 31 a of the rotor 31, a disk-shaped member 44 is provided.
- the spacer 35 is formed with a recess having a width corresponding to the thickness of the disk-shaped member 44.
- the outer peripheral part of the disk-shaped member 44 is inserted into the recess, and the disk-shaped member 44 and the spacer 35 are fastened with bolts in this state. That is, the disk-shaped member 44 is sandwiched between the boss portion 37 of the rotor blade 34 and the spacer 35 without a gap.
- the disk-shaped member 44 is disposed in a posture that is perpendicular to the rotor shaft portion 46.
- a through-hole penetrating in the thickness direction is formed at the center of the disk-shaped member 44.
- the rotor shaft portion 46 is inserted through the through hole. Therefore, the rotor shaft portion 46 is supported by the disk-like member 44 at a plurality of positions in the intermediate portion.
- the moving blades 34 are all made of aluminum or aluminum alloy, and the spacers 35 are all made of aluminum or aluminum alloy.
- the rotor 31 is made of aluminum or aluminum alloy.
- the rotor shaft portion 46 is made of titanium or a titanium alloy. Therefore, the rotor shaft portion 46 is made of a material having a lower linear expansion coefficient than aluminum. For this reason, when the rotor 31 and the rotor shaft portion 46 expand due to heat generated when the axial flow compressor 10 is driven, the rotor 31 expands more in the axial direction than the rotor shaft portion 46.
- the first pressing member 41 and the second pressing member 42 are made of stainless steel or stainless steel alloy.
- the disk-shaped member 44 is made of aluminum or aluminum alloy.
- the moving blade 34 including the uppermost moving blade 34 is made of aluminum or aluminum alloy. At least the uppermost moving blade 34 may be subjected to an anodic oxide coating treatment. In this case, erosion of the moving blade 34 can be effectively prevented while reducing the weight of the moving blade 34.
- the uppermost moving blade 34 may be made of titanium, titanium alloy, stainless steel, or stainless steel alloy. In this case, it is possible to ensure the durability of the uppermost moving blade 34 while preventing erosion.
- the end shaft portions 47 and 47 at both ends are supported by bearings 55 and 55, respectively, and are arranged coaxially with the rotor shaft portion 46.
- the bearing 55 rotatably supports the end shaft portion 47 at the main portion 47 c of the end shaft portion 47.
- the main portion 47 c is a portion extending coaxially with the rotor shaft portion 46.
- Both bearings 55 and 55 are accommodated in housings 56 and 57, respectively.
- the upstream housing 56 that houses the bearing 55 on the one end portion side is provided so as to form a cylindrical space between the second case portion 28 and the second housing portion 28. This space becomes the upstream space US through which the working fluid introduced into the compression space CS flows.
- the downstream housing 57 that houses the bearing 55 on the other end side is provided so as to form a cylindrical space with the third case portion 29. This space becomes a downstream space DS through which the working fluid derived from the compression space CS flows.
- the housings 56 and 57 are supported by the second case portion 28 or the third case portion 29 via a plurality of support members 59 and 59.
- Each support member 59 is formed in a rod shape and is radially arranged in the circumferential direction.
- the support members 59 are disposed in the upstream space US and the downstream space DS. Since the cross section of the support member 59 is streamlined, the support member 59 does not hinder the flow of the working fluid.
- the support member 59 in the downstream space DS is configured to enter the inside of the housing 57. However, the part entering the inside of the housing 57 may not be formed in a rod shape. .
- the support member 59 is formed with a supply / discharge passage 59a for supplying and discharging the lubricant.
- the lubricant is introduced from the outside of the second case portion 28 and the third case portion 29, supplied to the bearing 55 through one of the supply / discharge passages 59a, and from the bearing 55 through the other supply / discharge passages 59a. Discharged.
- the end shaft portion 47 on the discharge port CS2 side is disposed in the downstream housing 57, and the end shaft portion 47 is connected to the rotation shaft of the electric motor 22 via a flexible coupling 61 as an example of a vibration damping portion. 22a is connected. Since the drive shaft 40 of the compressor 20 and the rotating shaft 22a of the electric motor 22 are connected without a speed increaser, the rotating speed of the electric motor 22 and the rotating speed of the rotor 31 are the same.
- the deceleration portion 24 has a downstream space DS formed by the third case portion 29.
- the third case portion 29 includes an outer peripheral surface portion 29a connected to one axial end portion of the first case portion 27, an inner peripheral surface portion 29b that is disposed inside the outer peripheral surface portion 29a and extends in the axial direction, and the outer peripheral surface portion 29a and the inner peripheral surface portion. And an end surface portion 29c for connecting the end portions in the axial direction of 29b.
- the outer peripheral surface portion 29a is formed with a flare portion 29d that is formed in a cylindrical shape and has an inner diameter that gradually increases as the distance from the discharge port CS2 increases.
- a portion 29e ahead of the flare portion 29d has a constant inner diameter.
- the inner peripheral surface portion 29b is connected to the end of the downstream housing 57, and is formed in a cylindrical shape having a constant outer diameter along the axial direction. Therefore, in the downstream space DS, the cross section perpendicular to the axial direction is an annular shape, the taper portion where the cross sectional area gradually increases, the cross section perpendicular to the axial direction is the annular shape, and the cross sectional area is constant. And a parallel part.
- At least the taper portion functions as a diffuser that decelerates the working fluid compressed by the compression portion 20 and recovers the pressure.
- the parallel portion functions as a collector that collects the fluid decelerated by the tapered portion.
- the working fluid is sufficiently decelerated in the taper part, so that the pressure can be recovered without causing an excessive loss in the parallel part.
- the inner peripheral surface portion 29b is connected to the housing 57 in a stepped shape, but the stepped portion may be omitted. Further, the inner peripheral surface portion 29b may be configured to have a tapered shape corresponding to the tapered portion of the outer peripheral surface portion 29a. Further, the length of the parallel portion and the like can be appropriately selected according to how much the flow rate of the working fluid discharged from the discharge port CS2 is decelerated.
- a discharge port 65 is provided in a portion 29e constituting the parallel portion.
- a piping for guiding the working fluid decelerated in the downstream space DS to the condenser 13 is connected to the discharge port 65.
- An electric motor support portion 66 is provided on the inner peripheral surface portion 29 b so as to extend radially inward from a connection portion with the housing 57.
- the electric motor 22 is disposed inside the inner peripheral surface portion 29 b of the speed reduction portion 24 and is attached to the electric motor support portion 66.
- the drive shaft 40 of the compression unit 20 when the rotating shaft 22a of the electric motor 22 rotates, the drive shaft 40 of the compression unit 20 also rotates at the same rotational speed, and the rotor 31 rotates around the axis. Accordingly, the working fluid in the upstream space US is sucked into the compression space CS through the suction port CS1. In the compression space CS, the working fluid is sent to the right in FIG. 1 while being compressed, and the working fluid is discharged to the downstream space DS through the discharge port CS2. The working fluid is decelerated in the speed reduction unit 24, recovers its pressure, and is discharged through the discharge port 65.
- the drive shaft 40 of the compression unit 20 is connected to the rotating shaft 22a of the electric motor 22 without using a speed increaser. For this reason, it is not necessary to arrange
- the speed increaser is not provided, it is possible to prevent the radial width of the compression unit 20 from increasing from this point.
- the speed reduction unit 24 extends around the electric motor 22 in the axial direction of the drive shaft 40, the volume of the space of the speed reduction unit 24, that is, the volume of the space for reducing the flow rate of the working fluid is secured.
- the radial width of the axial flow compressor 10 can be prevented from increasing.
- the water vapor that is the working fluid to be compressed is, for example, in the range of 5 ° C. to 150 ° C. at a pressure below atmospheric pressure at the discharge port from the inlet of the axial flow compressor 10. This is for compressing water vapor at a temperature (for example, a temperature in the range of 5 ° C. to 250 ° C. when the moving blade has a plurality of stages of about 7 stages). For this reason, the low output electric motor 22 can be utilized. Also from this point, it is possible to prevent the radial width of the compression portion 20 from increasing.
- the pressure recovery efficiency is higher than that of the configuration in which the speed reduction part 24 is bent in the radial direction. Can be improved.
- the rotation shaft 40 of the compression unit 20 and the rotation shaft 22a of the electric motor 22 are connected via the flexible coupling 61, even when the electric motor 22 is driven at a high rotational speed, the rotation shaft It is possible to suppress the vibration of 22a from being transmitted to the drive shaft 40 of the compression unit 20.
- the present invention is not limited to the above-described embodiment, and various modifications and improvements can be made without departing from the spirit of the present invention.
- the said embodiment demonstrated the example comprised as the axial flow compressor 10 used for a refrigerator, it is not restricted to this.
- the working fluid is not limited to water vapor.
- various fluids such as air, oxygen, nitrogen, and hydrocarbon-based process gas can be applied as the working fluid.
- the rotor 31 has a plurality of moving blades 34.
- the present invention is not limited to this, and a configuration having one moving blade 34 may be used.
- the rotary shaft 22a of the electric motor 22 and the drive shaft 40 of the compression unit 20 are connected via the flexible coupling 61.
- the present invention is not limited to this configuration.
- the drive shaft 40 and the rotation shaft 22a may be connected via an intermediate shaft (not shown) to provide a bearing for the intermediate shaft.
- the transmission of the vibration of the rotary shaft 22a to the drive shaft 40 can also be suppressed by this intermediate shaft. That is, this intermediate shaft functions as a vibration damping part.
- a vibration damping part is abbreviate
- the axial flow compressor according to the present embodiment has a configuration in which the drive shaft of the compression unit is connected to the rotating shaft of the electric motor without a speed increaser. For this reason, it is not necessary to arrange
- the speed reduction part may extend to a place beyond the electric motor in the axial direction of the drive shaft.
- the speed reducing portion extends around the electric motor in the axial direction of the drive shaft. For this reason, it is possible to prevent an increase in the radial width of the axial flow compressor while securing the volume of the space of the speed reducing portion, that is, the volume of the space for decelerating the flow rate of the working fluid.
- the drive shaft of the compression unit and the rotation shaft of the electric motor may be connected via a vibration damping unit.
- a vibration damping unit Even when the electric motor is driven at a high rotational speed, it is possible to suppress the vibration of the rotation shaft from being transmitted to the drive shaft of the compression unit.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
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Abstract
Description
22 電動機
22a 回転軸
24 減速部
31 ロータ
34 動翼
61 フレキシブルカップリング
Claims (3)
- 作動流体を圧縮するための軸流圧縮機であって、
回転軸を有する電動機と、
前記電動機の回転軸に増速機を介することなく接続される駆動軸と、この駆動軸と一体的に回転するロータとを有し、前記駆動軸を駆動することによって作動流体を圧縮する圧縮部と、
前記圧縮部の吐出口から吐出された作動流体の流速を低減させるための空間を有する減速部と、を備え、
前記電動機の回転軸は、前記駆動軸の吐出口側の端部に接続され、
前記減速部は、前記電動機を囲むように配置されている軸流圧縮機。 - 前記減速部は、前記駆動軸の軸方向において前記電動機を越えるところまで延びている請求項1に記載の軸流圧縮機。
- 前記圧縮部の駆動軸と前記電動機の回転軸とは、振動減衰部を介して接続されている請求項1又は2に記載の軸流圧縮機。
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201180014288.2A CN102859202B (zh) | 2010-03-17 | 2011-03-15 | 轴流压缩机 |
EP11755907.0A EP2549120A4 (en) | 2010-03-17 | 2011-03-15 | Axial flow compressor |
US13/635,518 US9206818B2 (en) | 2010-03-17 | 2011-03-15 | Axial flow compressor |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2010060580A JP5819590B2 (ja) | 2010-03-17 | 2010-03-17 | 軸流圧縮機 |
JP2010-060580 | 2010-03-17 |
Publications (1)
Publication Number | Publication Date |
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WO2011114716A1 true WO2011114716A1 (ja) | 2011-09-22 |
Family
ID=44648828
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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PCT/JP2011/001513 WO2011114716A1 (ja) | 2010-03-17 | 2011-03-15 | 軸流圧縮機 |
Country Status (5)
Country | Link |
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US (1) | US9206818B2 (ja) |
EP (1) | EP2549120A4 (ja) |
JP (1) | JP5819590B2 (ja) |
CN (1) | CN102859202B (ja) |
WO (1) | WO2011114716A1 (ja) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
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EP2824330A1 (en) * | 2013-07-12 | 2015-01-14 | Johnson Controls Denmark ApS | An axial compressor and use of an axial compressor |
WO2017184804A1 (en) * | 2016-04-20 | 2017-10-26 | Danfoss A/S | Axial flow compressor for hvac chiller systems |
DE102022110555A1 (de) * | 2022-04-29 | 2023-11-02 | Borgwarner Inc. | Rezirkulationsgebläse |
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GB0304320D0 (en) * | 2003-02-26 | 2003-04-02 | Bladon Jets Ltd | Gas turbine engines |
JP2005120926A (ja) * | 2003-10-17 | 2005-05-12 | Mitsubishi Heavy Ind Ltd | トンネルファン |
CN201129311Y (zh) * | 2007-11-29 | 2008-10-08 | 张伟 | 流体推动机 |
JP5157501B2 (ja) | 2008-02-06 | 2013-03-06 | 株式会社Ihi | 冷凍機 |
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2010
- 2010-03-17 JP JP2010060580A patent/JP5819590B2/ja not_active Expired - Fee Related
-
2011
- 2011-03-15 CN CN201180014288.2A patent/CN102859202B/zh not_active Expired - Fee Related
- 2011-03-15 WO PCT/JP2011/001513 patent/WO2011114716A1/ja active Application Filing
- 2011-03-15 EP EP11755907.0A patent/EP2549120A4/en not_active Withdrawn
- 2011-03-15 US US13/635,518 patent/US9206818B2/en not_active Expired - Fee Related
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Also Published As
Publication number | Publication date |
---|---|
CN102859202A (zh) | 2013-01-02 |
EP2549120A4 (en) | 2017-09-27 |
US20130011280A1 (en) | 2013-01-10 |
JP5819590B2 (ja) | 2015-11-24 |
EP2549120A1 (en) | 2013-01-23 |
JP2011196189A (ja) | 2011-10-06 |
US9206818B2 (en) | 2015-12-08 |
CN102859202B (zh) | 2015-08-12 |
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