EXTRACTING STEAM FROM A TURBINE

• US 20170096913A1
• Filed: 12/22/2015
• Published: 04/06/2017
• Est. Priority Date: 10/06/2015
• Status: Active Grant

• Current Assignee: Nuovo Pignone Tecnologie SRL (Baker Hughes Company)
• Original Assignee: Nuovo Pignone SRL (Baker Hughes Company)
• Inventors: Pieri, Marco
• Granted Patent: US 10,030,544 B2
• Time in Patent Office: Days
• CPC Class Codes: F01D 17/00 Regulating or controlling by varying flow for reversing F01D1/30; by varying rotor-blade position F01D7/00; specially for starting F01D19/00; shutting-down F01D21/00; regulating or controlling in general G05 ; specially adapted for hand-held tools or the like F01D15/06
• CPC Class Codes: F01D 17/10 Final actuators valves in general F16K ; blades with variable camber F01D5/148
• CPC Class Codes: F01D 17/14 varying effective cross-sectional area of nozzles or guide conduits
• CPC Class Codes: F01D 17/145 by means of valves, e.g. for steam turbines valves in general F16K
• CPC Class Codes: F01K 7/165 Controlling means specially adapted therefor
• CPC Class Codes: F02C 9/00 Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants controlling air intakes F02C7/057; controlling turbines F01D; controlling compressors F04D27/00; controlling in general G05

Abstract

A valve assembly for use to regulate a flow of steam in a flowpath of a turbine. The valve assembly can be configured with a body that circumscribes a rotor. The body is disposed upstream of the rotor blades. In one implementation, the body forms an annular ring with a plurality of arcuate segments, each being configured to move independently of the other segments in the ring to change the size of an annular gap between the arcuate segments and the rotor. The size of the annular gap corresponds with flow parameters for working fluid that flows across the rotor and that exits the turbine for use in pre-heaters and like collateral equipment.

Claims

1. A turbine, comprising:

a casing defining a fluid pathway;

a rotor disposed in the fluid pathway; and

a valve circumscribing the rotor, the valve defining an aperture that forms a flow area through which fluid can flow between the valve and the rotor.

2. The turbine of claim 1, wherein the valve is configured to actuate so as to change the size of the flow area relative to the rotor.

3. The turbine of claim 1, wherein the valve is disposed upstream of blades disposed on the rotor.

4. The turbine of claim 3, wherein the valve is disposed upstream of blades disposed on the casing.

5. The turbine of claim 1, wherein the valve has a body member comprising a plurality of arcuate segments.

6. The turbine of claim 5, wherein each of the plurality of arcuate segments move independent relative to each other and to the rotor.

7. The turbine of claim 5, further comprising a plurality of actuators, one each coupled to the plurality of arcuate segments.

8. The turbine of claim 5, wherein the body member comprises a plurality of coupling members extending between adjacent ones of the plurality of arcuate segments, and wherein the plurality of coupling members are configured to provide continuity between an upstream facing surface on the plurality of arcuate segments to prevent fluid flow through the body member.

9. The turbine of claim 5, wherein the plurality of arcuate segments have an inner peripheral edge that forms a gap with the rotor, and wherein the arcuate segments are configured to assume a position in which the inner peripheral edge interfaces with the rotor.

10. The turbine of claim 9, further comprising a sealing mechanism that is configured to create a seal between the inner peripheral edge and the rotor with the plurality of arcuate segments in the position.

11. A turbine, comprising:

a rotor having a body with a first set of blades;

a casing at least partially surrounding the rotor, the casing having a second set of blades adjacent the first set of blades; and

a ring member circumscribing the rotor, the ring member having an inner peripheral edge that defines a gap with the rotor, the gap extending annularly between the ring member and the rotor,

wherein the ring member is configured to change the gap from a first gap to a second gap to vary flow of working fluid through the ring member and between the ring member and the rotor.

12. The turbine of claim 11, wherein the ring member comprises a first arcuate segment and a second arcuate segment, each configured to move independently of the other to change the gap from the first gap to the second gap.

13. The turbine of claim 12, wherein the ring member comprises a third arcuate segment disposed adjacent the first arcuate segment and the second arcuate segment.

14. The turbine of claim 13, wherein the first arcuate segment, the second arcuate segment, and the third arcuate segment are configured to move radially inwardly and outwardly relative to the rotor.

15. The turbine of claim 11, wherein the second gap configures the ring member to prevent flow across the rotor.

16. The turbine of claim 15, wherein the inner peripheral edge engages the rotor.

17. A method for modulating flow across rotor in a turbine, said method comprising:

locating a ring member about a rotor in a flow pathway of a turbine;

partitioning the ring member into segments; and

allowing the segments to change position relative to one another and relative to the rotor to reduce an annular gap between the ring member and the rotor.

18. The method of claim 17, further comprising:

coupling adjacent segments to prevent flow through the ring member.

19. The method of claim 17, further comprising:

coupling an actuator individually to the segments.

20. The method of claim 17, further comprising

arranging the segments so that each has a first position and a second position that is closer to the rotor than the first position.