Gas expansion system

Patent metadata

Field	Value
Publication number	US-11493240-B2
Application number	US-201816759588-A
Country	US
Kind code	B2
Filing date	Oct 10, 2018
Priority date	Oct 27, 2017
Publication date	Nov 8, 2022
Grant date	Nov 8, 2022

Abstract

The amount of consumption of gas is reduced when the gas is expanded to be cooled by using a plurality of expansion turbines. A high-pressure expansion turbine includes: a gas supply passage through which bearing gas is supplied to a bearing portion; and a gas discharge passage through which the bearing gas which has been supplied from the gas supply passage to the bearing portion is discharged from the bearing portion. A low-pressure expansion turbine includes: a gas supply passage through which the bearing gas is supplied to a bearing portion; and a gas discharge passage through which the bearing gas which has been supplied from the gas supply passage to the bearing portion is discharged from the bearing portion. The bearing gas discharged from the gas discharge passage of the high-pressure expansion turbine is supplied to the gas supply passage of the low-pressure expansion turbine.

First claim

The invention claimed is:

1. A gas expansion system comprising:
a first expansion turbine including
a first rotating shaft,
a first impeller attached to the first rotating shaft and configured to, when the first rotating shaft rotates, expand a gas while taking the gas into the first impeller,
a first bearing portion supporting the first rotating shaft,
a first gas supply passage through which bearing gas is supplied to the first bearing portion, and
a first gas discharge passage through which the bearing gas which has been supplied from the first gas supply passage to the first bearing portion is discharged from the first bearing portion; and

a second expansion turbine including
a second rotating shaft,
a second impeller attached to the second rotating shaft and configured to, when the second rotating shaft rotates, expand the gas while taking the gas into the second impeller,
a second bearing portion supporting the second rotating shaft,
a second gas supply passage through which the bearing gas is supplied to the second bearing portion, and
a second gas discharge passage through which the bearing gas which has been supplied from the second gas supply passage to the second bearing portion is discharged from the second bearing portion, wherein:

the first expansion turbine and the second expansion turbine are connected to each other in series such that the gas expanded by the first impeller of the first expansion turbine is supplied to the second impeller of the second expansion turbine;
the first gas discharge passage and the second gas supply passage are directly connected to each other; and
the bearing gas discharged from the first gas discharge passage is directly supplied to the second gas supply passage.

2. The gas expansion system according to claim 1 , wherein:
the first bearing portion includes a first radial bearing portion supporting the first rotating shaft in a radial direction; and
the second bearing portion includes a second radial bearing portion supporting the second rotating shaft in the radial direction.

3. The expansion system according to claim 2 , wherein:
the first bearing portion includes a first thrust bearing portion supporting the first rotating shaft in an axial direction; and
the second bearing portion includes a second thrust bearing portion supporting the second rotating shaft in the axial direction.

4. The expansion system according to claim 1 , wherein:
the first expansion turbine includes
a first radial bearing portion supporting the first rotating shaft in a radial direction and
a first thrust bearing portion supporting the first rotating shaft in an axial direction;

the second expansion turbine includes
a second radial bearing portion supporting the second rotating shaft in a radial direction and
a second thrust bearing portion supporting the second rotating shaft in an axial direction;

the first bearing portion is only the first radial bearing portion out of the first radial bearing portion and the first thrust bearing portion; and
the second bearing portion is only the second radial bearing portion out of the second radial bearing portion and the second thrust bearing portion.

5. The expansion system according to claim 1 , wherein:
the second bearing portion is a sealing portion configured to prevent the gas, expanded by the second impeller attached to a first end of the second rotating shaft, from flowing toward a second end of the second rotating shaft along the axial direction of the second rotating shaft; and
the bearing gas supplied through the second gas supply passage to the sealing portion is higher in pressure than the gas expanded by the second impeller.

6. The expansion system according to claim 5 , wherein the bearing gas is seal gas that pushes out the gas from the sealing portion toward the first end.

Assignees

• Kawasaki Heavy Ind Ltd

Inventors

• Saito Yuichi
• Ishimaru Hidetsugu
• Takeuchi Ryota
• Adachi Toshimitsu
• Kariya Daisuke
• Sakai Naoto

Classifications

• F25J1/0279

  Compression of refrigerant or internal recycle fluid, e.g. kind of compressor, accumulator, suction drum etc. · CPC title

• F25J2270/16

  with mutliple gas expansion loops of the same refrigerant · CPC title

• F25J1/0221

  using the cold stored in an external cryogenic component in an open refrigeration loop · CPC title

• F25J1/0007

  Helium · CPC title

• F16C33/748

  flowing to or from the sealing gap, e.g. vacuum seals with differential exhaust · CPC title