JP2017106330A5 - Turbomachine and turbomachine refrigerant compression method - Google Patents
Turbomachine and turbomachine refrigerant compression method Download PDFInfo
- Publication number
- JP2017106330A5 JP2017106330A5 JP2015238532A JP2015238532A JP2017106330A5 JP 2017106330 A5 JP2017106330 A5 JP 2017106330A5 JP 2015238532 A JP2015238532 A JP 2015238532A JP 2015238532 A JP2015238532 A JP 2015238532A JP 2017106330 A5 JP2017106330 A5 JP 2017106330A5
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- JP
- Japan
- Prior art keywords
- rotating shaft
- bearing
- partition wall
- phase refrigerant
- gas
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- 239000003507 refrigerant Substances 0.000 title claims 20
- 238000007906 compression Methods 0.000 title claims 2
- 238000005192 partition Methods 0.000 claims 10
- 239000007788 liquid Substances 0.000 claims 8
- 230000002093 peripheral Effects 0.000 claims 3
- 238000007599 discharging Methods 0.000 claims 1
- 238000005461 lubrication Methods 0.000 claims 1
Claims (5)
液冷媒が介在した状態で前記回転軸の外周面と向かい合う軸受面を有する、前記回転軸を支持する軸受と、
前記軸受から排出される前記液冷媒が気相冷媒とともに貯留される排出空間が介在した状態で前記軸受の軸線方向における前記軸受の端面と向かい合っており、前記回転軸が挿入された貫通孔を有する隔壁と、
前記回転軸の軸線方向において前記隔壁から見て前記軸受と反対側で気相冷媒が吸入される吸入空間が介在した状態で前記隔壁と向かい合う前面を有する、前記回転軸に固定された翼車であって、前記回転軸とともに回転することにより前記吸入空間から前記気相冷媒を吸入する翼車と、を備え、
前記隔壁及び前記回転軸は、前記貫通孔を形成する面と前記回転軸の外周面との間に、前記排出空間から供給される前記気相冷媒によって満たされる絞りを形成している、
ターボ機械。 A rotation axis;
A bearing that supports the rotating shaft, and has a bearing surface facing the outer peripheral surface of the rotating shaft in a state where a liquid refrigerant is interposed;
The liquid refrigerant discharged from the bearing faces the end surface of the bearing in the axial direction of the bearing with a discharge space in which the liquid refrigerant is stored together with the gas-phase refrigerant, and has a through hole into which the rotating shaft is inserted. A partition,
An impeller fixed to the rotating shaft, having a front surface facing the partition wall in a state where a suction space for sucking a gas-phase refrigerant is interposed on the opposite side of the bearing as viewed from the partition wall in the axial direction of the rotating shaft. An impeller for sucking the gas-phase refrigerant from the suction space by rotating together with the rotating shaft,
The partition and the rotary shaft form a throttle filled with the gas-phase refrigerant supplied from the discharge space between a surface forming the through hole and an outer peripheral surface of the rotary shaft.
Turbo machine.
前記回転軸と軸受との間に液冷媒を供給して前記軸受及び前記回転軸を潤滑し、Supplying a liquid refrigerant between the rotating shaft and the bearing to lubricate the bearing and the rotating shaft;
潤滑に用いた前記液冷媒のうち少なくとも一部の液冷媒を排出空間に排出し、Discharging at least a portion of the liquid refrigerant used for lubrication into a discharge space;
前記少なくとも一部の液冷媒のうち一部が蒸発した気相冷媒とともに前記少なくとも一部の液冷媒を前記排出空間に貯留し、Storing at least a part of the liquid refrigerant in the discharge space together with a gas phase refrigerant in which a part of the at least part of the liquid refrigerant is evaporated;
前記排出空間に貯留された前記少なくとも一部の液冷媒及び前記気相冷媒のうち前記気相冷媒を、前記排出空間と吸入空間との間に配置された隔壁に形成されて前記回転軸が挿入された貫通孔において前記回転軸と前記隔壁との間に形成された絞りを介して、前記排出空間から前記吸入空間へ供給し、Of the at least part of the liquid refrigerant and the gas phase refrigerant stored in the discharge space, the gas phase refrigerant is formed in a partition wall disposed between the discharge space and the suction space, and the rotating shaft is inserted. Through the throttling formed between the rotating shaft and the partition wall in the through hole is supplied from the discharge space to the suction space,
圧縮されるべき気相冷媒と前記排出空間から供給される前記気相冷媒とで前記吸入空間を満たし、The suction space is filled with the gas phase refrigerant to be compressed and the gas phase refrigerant supplied from the exhaust space,
前記吸入空間を満たす前記気相冷媒を前記翼車の回転により圧縮する、Compressing the gas-phase refrigerant filling the suction space by rotation of the impeller;
ターボ機械の冷媒圧縮方法。Refrigerant compression method for turbomachine.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2015238532A JP2017106330A (en) | 2015-12-07 | 2015-12-07 | Turbomachine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2015238532A JP2017106330A (en) | 2015-12-07 | 2015-12-07 | Turbomachine |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2017106330A JP2017106330A (en) | 2017-06-15 |
JP2017106330A5 true JP2017106330A5 (en) | 2019-01-24 |
Family
ID=59059337
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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JP2015238532A Pending JP2017106330A (en) | 2015-12-07 | 2015-12-07 | Turbomachine |
Country Status (1)
Country | Link |
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JP (1) | JP2017106330A (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10527062B2 (en) * | 2015-11-13 | 2020-01-07 | Mitsubishi Heavy Industries Compressor Corporation | Centrifugal compressor |
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2015
- 2015-12-07 JP JP2015238532A patent/JP2017106330A/en active Pending
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