Cooling/heating augmentation during turbine startup/shutdown using a seal positioned by thermal response of turbine parts and consequent relative movement thereof

• US 6,146,090 A
• Filed: 12/22/1998
• Issued: 11/14/2000
• Est. Priority Date: 12/22/1998
• Status: Expired due to Term

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Schmidt, Mark Christopher
• Primary Examiner(s): VERDIER, CHRISTOPHER M
• Application Number:
  US09/218,228
• Time in Patent Office: 693 Days
• Field of Search: 415/47, 415/48, 415/115, 415/116, 415/117, 415/175-178, 415/134, 415/136, 415/138, 416/39, 416/95, 416/96 R, 416/96 A, 416/97 R, 416/198 A, 416/200 A, 416/201 R
• US Class Current: 415/47
• CPC Class Codes: F01D 11/24 by selectively cooling-heating stator or rotor components
• CPC Class Codes: F01D 5/084 the fluid circulating at the periphery of a multistage rotor, e.g. of drum type

Abstract

In a turbine rotor, a thermal mismatch between various component parts of the rotor occurs particularly during transient operations such as shutdown and startup. A thermal medium flows past and heats or cools one part of the turbine which may have a deleterious thermal mismatch with another part. By passively controlling the flow of cooling medium past the one part in response to relative movement of thermally responsive parts of the turbine, the flow of thermal medium along the flow path can be regulated to increase or reduce the flow, thereby to regulate the temperature of the one part to maintain the thermal mismatch within predetermined limits.

Claims

1. A turbine, comprising:

first and second parts defining a flow path in the turbine for flowing a thermal medium, said parts having different thermal responses to applied temperatures generating relative movement between said parts;

a seal carried by one of said first and second parts and in said flow path;

said seal being responsive to said relative movement between said parts to regulate the flow of the thermal medium along said flow path, thereby increasing or reducing the flow of thermal medium along the flow path to regulate the temperature of said second part;

wherein said second part and a third part are connected to one another and are responsive to different applied temperatures creating a transient thermal mismatch therebetween, said seal regulating the flow of thermal medium along said flow path to either heat or cool said second part to a temperature enabling the magnitude of the thermal mismatch of said second part and said third part to lie within a predetermined thermal mismatch; and

wherein said third part comprises a turbine rotor wheel for mounting buckets and said second part comprises an adjoining wheel having a rabbeted joint with said turbine rotor wheel, said adjoining wheel being heated or cooled to reduce the thermal mismatch between said turbine rotor wheel and said adjoining wheel to within a predetermined thermal mismatch to preclude relative displacement of the rabbeted joint therebetween.

2. A turbine according to claim 1 wherein said seal reduces flow along said flow path in response to movement of one of said first and second parts toward another of said first and second parts to reduce heat transfer from one or another of said parts to said thermal medium.

3. A turbine according to claim 1 wherein said seal increases flow along said flow path in response to movement of one of said first and second parts away from another of said first and second parts to promote heat transfer from one or another of said parts to said thermal medium.

4. A turbine according to claim 1 wherein said first and second parts comprise stationary and rotating components of the turbine, respectively.