Turbomachine component temperature control

Patent metadata

Field	Value
Publication number	US-9228588-B2
Application number	US-201213680966-A
Country	US
Kind code	B2
Filing date	Nov 19, 2012
Priority date	Jan 6, 2012
Publication date	Jan 5, 2016
Grant date	Jan 5, 2016

Abstract

Apparatus and methods for expanding a process fluid are disclosed. The apparatus includes a casing having an inlet and an outlet, and a component carrier disposed in the casing. The component carrier and the casing defining a cavity therebetween, and the component carrier at least partially defines a process flowpath fluidly communicating with the inlet and the outlet of the casing. The apparatus also includes a rotor disposed at least partially in the component carrier, with the rotor at least partially defining a first expansion stage intersecting the process flowpath. The apparatus also includes a bleed port extending from the process flowpath at a first point of the process flowpath to the cavity, to provide a thermal buffer fluid to the cavity.

First claim

We claim:

1. An apparatus for expanding a process fluid, comprising:
a casing having an inlet and an outlet;
a component carrier disposed in the casing, the component carrier and the casing defining a cavity therebetween, and the component carrier at least partially defining a process flowpath fluidly communicating with the inlet and the outlet of the casing;
a rotor disposed at least partially in the component carrier, the rotor at least partially defining a first expansion stage intersecting the process flowpath; and
a bleed port extending from the process flowpath at a first point of the process flowpath to the cavity, to provide a thermal buffer fluid to the cavity,
wherein the inlet is coupled to the process flowpath by a first transfer conduit disposed at least partially in the cavity, such that the first transfer conduit transfers heat to the thermal buffer fluid, and
wherein the outlet is coupled to the process flowpath by a second transfer conduit disposed at least partially in the cavity, such that the second transfer conduit transfers heat to the thermal buffer fluid.

2. The apparatus of claim 1 , further comprising a return port extending from the cavity to a second point of the process flowpath, the second point being downstream from the first point, to return at least a portion of the thermal buffer fluid to the process flowpath.

3. The apparatus of claim 2 , further comprising:
first and second pressure break-down seals configured to at least partially seal the component carrier and a shaft; and
a low-pressure feed port extending at least partially through the component carrier and to a point between the first and second pressure break-down seals, wherein at least a portion of the thermal buffer fluid in the return port flows across the first pressure break-down seal to the low-pressure feed port.

4. The apparatus of claim 1 , wherein the cavity forms at least part of an annulus extending at least partially around the component carrier.

5. The apparatus of claim 1 , wherein the rotor at least partially defines a second expansion stage intersecting the process flowpath, the first point being between the first and second expansion stages.

6. A rotating machine, comprising:
a casing having a higher-temperature inlet, a higher-temperature outlet, a lower-temperature inlet, and a lower-temperature outlet;
a lower-temperature component carrier disposed in the casing, including a first expansion stage, and defining a first process flowpath intersecting the first expansion stage, wherein the first process flowpath is fluidly coupled to the lower-temperature inlet and the lower-temperature outlet, and wherein the lower temperature component carrier and the casing define a first cavity radially therebetween;
a higher-temperature component carrier disposed in the casing and co-axially aligned with the lower-temperature component carrier, the higher-temperature component carrier including a second expansion stage and defining a second process flowpath intersecting the second expansion stage, wherein the second process flowpath is fluidly coupled to the higher-temperature inlet and the higher-temperature outlet, the higher temperature component carrier and the casing defining a second cavity radially therebetween, the second cavity being in fluid communication with the first cavity; and
a bleed port extending in the lower-temperature component carrier and fluidly communicating with the first process flowpath at a first point of the first process flowpath and with the first cavity, to provide a thermal barrier fluid from the first process flowpath to the second cavity.

7. The rotating machine of claim 6 , wherein the second cavity is configured to receive thermal barrier fluid from the first cavity.

8. The rotating machine of claim 6 , further comprising a first return port extending from the first cavity to the first process flowpath, the first return port being configured to direct fluid from the first cavity to the first process flowpath at a second point located downstream from the first point.

9. The rotating machine of claim 8 , wherein at least a portion of the thermal barrier fluid directed through the first return port migrates across a pressure break-down seal and combines with a spent seal gas flow.

10. The rotating machine of claim 8 , further comprising a second return port extending from the second cavity to the second process flowpath, the second return port being configured to direct thermal barrier fluid from the second cavity to the second process flowpath.

11. The rotating machine of claim 10 , wherein at least one of the lower-temperature outlet and the lower-temperature inlet is disposed at least partially in the first cavity.

12. The rotating machine of claim 11 , wherein at least one of the higher-temperature inlet and the higher-temperature outlet is disposed at least partially in the second cavity.

13. The rotating machine of claim 6 , wherein the first point is located downstream from the first expansion stage and upstream from a third expansion stage defined in the lower-temperature component carrier and intersecting the first process flowpath.

14. The rotating machine of claim 6 , wherein the thermal barrier fluid is substantially CO 2 .

15. A method for controlling temperature in a rotating machine, comprising:
expanding a process fluid in a lower-temperature component carrier and a higher-temperature component carrier;
bleeding a thermal barrier fluid from a process flowpath of the lower-temperature component carrier;
introducing the thermal barrier fluid to a first cavity defined between the lower-temperature component carrier and a casing of the rotating machine such that heat transfers from the lower-temperature component carrier, the higher temperature component carrier, or both to the thermal barrier fluid; and
returning at least a portion of the thermal barrier fluid to the process flowpath via a return port defined in the lower-temperature component carrier.

16. The method of claim 15 , further comprising:
introducing at least a portion of the thermal barrier fluid to a second cavity defined between the higher-temperature component carrier and the casing, such that heat is transferred from the higher-temperature component carrier to the thermal barrier fluid; and
directing at least a portion of the thermal barrier fluid from the second cavity to a process flowpath of the higher-temperature component carrier via a second return port defined in the higher-temperature component carrier.

17. The method of claim 15 , wherein:
bleeding the thermal barrier fluid comprises extracting the thermal barrier fluid from the process flowpath at a point downstream from at least one expansion stage defined in the lower-temperature component carrier; and
returning the at least a portion of the thermal barrier fluid to the process flowpath comprises returning the at least a portion of the thermal barrier fluid to a second point downstream from the first point.

18. The method of claim 17 , further comprising:
referencing an area between at least two pressure break-down seals positioned proximal a distal end of the lower-temperature component carrier to a pressure of a lower-temperature outlet fluidly coupled to the process flowpath of the lower-temperature component carrier;
directing a portion of the thermal barrier fluid across at least one of the pressure break-down seals; and
allowing the portion of the thermal barrier fluid to mix with a spent seal gas.

Assignees

• Maier William C
• Leconte Patrice
• Lucas George M
• Dresser Rand Co

Inventors

• Maier William C
• Leconte Patrice
• Lucas George M

Classifications

• F01D11/10

  using sealing fluid, e.g. steam · CPC title

• F04D3/00 Primary

  Axial-flow pumps (priming or boosting F04D9/00) · CPC title

• F01K7/32

  the engines using steam of critical or overcritical pressure · CPC title

• F02C6/10

  supplying working fluid to a user, e.g. a chemical process, which returns working fluid to a turbine of the plant · CPC title

• F01D25/26

  Double casings; Measures against temperature strain in casings · CPC title