JP2017106330A5 - Turbomachine and turbomachine refrigerant compression method - Google Patents

Turbomachine and turbomachine refrigerant compression method Download PDF

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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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Japan
Prior art keywords
rotating shaft
bearing
partition wall
phase refrigerant
gas
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Pending
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JP2015238532A
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Japanese (ja)
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JP2017106330A (en
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Priority to JP2015238532A priority Critical patent/JP2017106330A/en
Priority claimed from JP2015238532A external-priority patent/JP2017106330A/en
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Publication of JP2017106330A5 publication Critical patent/JP2017106330A5/en
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Claims (5)

回転軸と、
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.
前記回転軸の軸線方向において前記翼車から見て前記隔壁と反対側で前記翼車に隣接して前記回転軸に取り付けられ、前記回転軸を回転させるモータをさらに備えた、請求項1に記載のターボ機械。   2. The motor according to claim 1, further comprising a motor that is attached to the rotating shaft adjacent to the impeller on the side opposite to the partition wall when viewed from the impeller in the axial direction of the rotating shaft and rotates the rotating shaft. Turbomachine. 前記回転軸の外周面から前記回転軸の半径方向外側に延びつつ環状に形成され、前記排出空間において前記隔壁に隣接して配置されている環状体をさらに備えている、請求項1又は2に記載のターボ機械。   3. The apparatus according to claim 1, further comprising an annular body that is formed in an annular shape while extending radially outward of the rotating shaft from an outer peripheral surface of the rotating shaft, and is disposed adjacent to the partition wall in the discharge space. The listed turbomachine. 前記隔壁は、当該隔壁の内部に断熱構造を有する、請求項1〜3のいずれか1項に記載のターボ機械。   The turbomachine according to claim 1, wherein the partition wall has a heat insulating structure inside the partition wall. 回転軸に固定された翼車を回転させ、Rotate the impeller fixed to the rotating shaft,
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.
JP2015238532A 2015-12-07 2015-12-07 Turbomachine Pending JP2017106330A (en)

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

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JP2015238532A Pending JP2017106330A (en) 2015-12-07 2015-12-07 Turbomachine

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* Cited by examiner, † Cited by third party
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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