Turbine and methods of assembling the same

Patent metadata

Field	Value
Publication number	US-10208609-B2
Application number	US-201414299280-A
Country	US
Kind code	B2
Filing date	Jun 9, 2014
Priority date	Jun 9, 2014
Publication date	Feb 19, 2019
Grant date	Feb 19, 2019

Abstract

A turbine operable with a first fluid and a second fluid is provided. The turbine includes a shaft and having a dry gas seal area, a balance area, and a shaft surface. The turbine also includes a stationary component coupled to a housing and having a first side and a second side and defining a channel in flow communication with the shaft surface. A heat exchange assembly is coupled to the housing and in flow communication with the shaft and the stationary component. The heat exchange assembly includes a first flow path coupled in flow communication with the dry gas seal area and the channel and configured to direct the first fluid along the first side. Heat exchange assembly also includes a second flow path coupled in flow communication with the balance area and channel and configured to direct the second fluid along the second side.

First claim

What is claimed is:

1. A turbine operable with a first fluid and a second fluid, said turbine comprising:
a housing;
a rotatable shaft supported within said housing and comprising a dry gas seal area, a balance area, and a shaft surface extending between said dry gas seal area and said balance area;
a stationary component coupled to said housing and comprising a first side and a second side and defining a first channel in flow communication with said shaft surface, said stationary component further comprising an end wall defined between said first side and said second side;
a seal assembly coupled to said shaft surface and extending into said first channel, said seal assembly comprising a first seal and a second seal; and
a heat exchange assembly coupled to said housing and in flow communication with said rotatable shaft and said stationary component, said heat exchange assembly comprising:
a first flow path comprising a first inlet, a first outlet coupled in flow communication with said first channel, and a second channel extending between said first inlet and said first outlet,
wherein said second channel is configured to discharge said first fluid into said first channel,
wherein said first flow path is coupled in flow communication with said dry gas seal area and said first channel, and
further wherein said first flow path is configured to direct said first fluid along said first side at a first pressure;
a first vent coupled in flow communication with said first outlet and said first side, said first seal positioned between said first flow path and said first vent, and said first vent oriented such that the first fluid channeled through said first flow path and then past said first seal is then directed along said first side and past said end wall;
a second flow path comprising a second inlet, a second outlet coupled in flow communication with said first channel, and a third channel extending between said second inlet and said second outlet,
wherein said third channel is configured to discharge said second fluid into said second channel,
wherein said second flow path is coupled in flow communication with said balance area and said first channel, and
further wherein said second flow path is configured to direct said second fluid along said second side at a second pressure substantially similar to the first pressure; and
a second vent coupled in flow communication with said second outlet and said second side, said second seal positioned between said second flow path and said second vent, and said second vent oriented such that the second fluid channeled through said second flow path and then past said second seal is then directed along said second side and past said end wall.

2. The turbine of claim 1 , wherein said heat exchange assembly comprises an insulator coupled to said stationary component.

3. The turbine of claim 1 , wherein said heat exchange assembly comprises a baffle coupled to said housing and in flow communication with said second flow path.

4. The turbine of claim 1 , wherein said heat exchange assembly comprises a cooling channel coupled in flow communication with said first flow path and said second flow path.

5. The turbine of claim 1 , wherein said first flow path, said second flow path, and said seal assembly are configured to reduce flows of the first fluid and the second fluid within said first channel.

6. The turbine of claim 1 , wherein said stationary component comprises a stator.

7. The turbine of claim 1 , wherein said first seal is coupled to said shaft surface and said second seal is coupled to said shaft surface.

8. A power generation system comprising:
a waste heat recovery unit configured to heat a supercritical working fluid having a Biot number of at least one;
a turbine coupled in flow communication with said waste heat recovery unit, said turbine comprising:
a housing;
a rotatable shaft supported within said housing; and
a stator coupled to the housing and comprising a first side and a second side and defining a first channel in flow communication with said rotatable shaft, said stator further comprising an end wall defined between said first side and said second side;
a seal assembly coupled to said housing and extending into said first channel, said seal assembly comprising a first seal and a second seal; and
a heat exchange assembly coupled to said turbine and in flow communication with said rotatable shaft and said stator, said heat exchange assembly comprising:
a first flow path comprising a first inlet a first outlet coupled in flow communication with said first channel, a second channel extending between said first inlet and said first outlet and configured to discharge said first fluid into said first channel, and a first vent coupled in flow communication with said first outlet and said first side, said first seal positioned between said first flow path and said first vent, and said first vent oriented such that a fluid channeled through said first flow path and then past said first seal is then directed along said first side and past said end wall at a first pressure; and
a second flow path comprising a second inlet, a second outlet coupled in flow communication with said first channel, a third channel extending between said second inlet and said second outlet and configured to discharge said second fluid into said second channel, and a second vent coupled in flow communication with said second outlet and said second side, said second seal positioned between second flow path and said second vent, and said second vent oriented such that the supercritical fluid channeled through said second flow path and then past said second seal is then directed along said second side and past said end wall at a second pressure substantially similar to the first pressure.

9. The power generation system of claim 8 , wherein said rotatable shaft comprises a thermal conductivity less than an effective heat transfer coefficient of the supercritical fluid.

10. The power generation system of claim 8 , wherein said first vent is coupled in flow communication with said first channel and comprises at least one of a square channel and a round channel.

11. The power generation system of claim 8 , wherein said second vent is coupled in flow communication with said first channel and comprises at least one of a square channel and a round channel.

12. The power generation system of claim 8 , wherein said seal assembly comprises at least one of a labyrinth seal, a brush seal, and a honeycomb seal coupled to shaft surface and extending into said channel.

13. The power generation system of claim 8 , wherein said shaft is configured operable with the supercritical fluid comprising carbon dioxide having a Biot number with a range from about 5 to about 50.

14. A method of assembling a turbine within a housing, said method comprising:
coupling a rotatable shaft to the housing, the rotatable shaft comprising a dry gas seal area, a balance area, and a shaft surface extending between the dry gas seal area and the balance area;
coupling a stationary component to the housing and comprising a first side and a second side and defining a first channel in flow communication with the shaft surface, said stationary component further comprising an end wall defined between said first side and said second side;
coupling a seal assembly to the rotatable shaft and extending into the first channel, the seal assembly including a first seal and a second seal; and
coupling a heat exchange assembly in flow communication with the rotatable shaft and the stationary component, the heat exchange assembly comprising:
a firs

Assignees

• Gen Electric

Inventors

• Kalra Chiranjeev Singh
• Thatte Azam Mihir
• Hofer Douglas Carl

Classifications

• F02C6/18

  using the waste heat of gas-turbine plants outside the plants themselves, e.g. gas-turbine power heat plants (using waste heat as source of energy for refrigeration plants F25B27/02; using the waste heat of a gasturbine for steam generation or in a steam cycle see F01K23/10) · CPC title

• F01D1/02

  with stationary working-fluid guiding means and bladed or like rotor, {e.g. multi-bladed impulse steam turbines}(F01D1/24 takes precedence; without stationary working-fluid guiding means F01D1/18) · CPC title

• F01D11/003 Primary

  by packing rings; Mechanical seals · CPC title

• F05D2260/20

  Heat transfer, e.g. cooling · CPC title

• B23P15/04

  turbine or like blades from several pieces · CPC title