Title:
二相流タービン動翼、二相流タービン、及び、冷凍サイクルシステム
Document Type and Number:
Japanese Patent JP7168376
Kind Code:
B2
Abstract:
A two-phase flow turbine provided upon a hub coupled to a rotating shaft and driven by receiving two-phase flow including a liquid phase component and a gas phase component. This rotor blade comprises: a rotor blade main body fixed to the hub and having a pressure surface that receives the two-phase flow; and at least one groove section extending above the pressure surface so as to intersect the radial direction of the rotating shaft.
Inventors:
▲高▼田 亮
Yasushi Hasegawa
Naoki Kobayashi
Yasushi Hasegawa
Naoki Kobayashi
Application Number:
JP2018152940A
Publication Date:
November 09, 2022
Filing Date:
August 15, 2018
Export Citation:
Assignee:
Mitsubishi Heavy Industries Thermal Systems Co., Ltd.
International Classes:
F01D5/14; F01K25/08; F25B11/02
Domestic Patent References:
| JP2016166569A | ||||
| JP2001516420A | ||||
| JP2008267381A | ||||
| JP2049931A | ||||
| JP6123202A | ||||
| JP53011257A | ||||
| JP54017083B2 | ||||
| JP2009216090A | ||||
| JP2017002756A | ||||
| JP2007309235A |
Foreign References:
| US3301529 |
Attorney, Agent or Firm:
SSIP Patent Attorney Corporation