Rotor cooling circuit

• US 7,993,102 B2
• Filed: 01/09/2009
• Issued: 08/09/2011
• Est. Priority Date: 01/09/2009
• Status: Active Grant

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Walker, Roger Clayton, Gutta, Richard Francis, Casanova, Fernando J., Desai, Tushar S., Meenaksh, Ravi
• Primary Examiner(s): ZARNEKE, DAVID A
• Application Number:
  US12/351,408
• Publication Number:
  US 20100178168A1
• Time in Patent Office: 942 Days
• Field of Search: 416/97.R, 416/95, 416/1
• US Class Current: 416/97.00R
• CPC Class Codes: F01D 5/082 on the side of the rotor disc
• CPC Class Codes: F01D 5/085 cooling fluid circulating inside the rotor
• CPC Class Codes: F02C 7/18 the medium being gaseous, e.g. air F02C7/125 takes precedence

Abstract

A cooling circuit serves to provide cooling air in a rotor having a compressor rotor and a turbine rotor. The cooling circuit includes a first cooling path through the compressor rotor in series with a second cooling path through the turbine rotor such that one amount of cooling air is used for cooling both the compressor rotor and the turbine rotor. The construction enables a reduction in cooling air requirements, thereby increasing power plant efficiency.

Claims

1. A cooling circuit in a rotor including a compressor rotor and a turbine rotor, the cooling circuit comprising:

a source of cooled cooling air;

a first cooling path defined through openings in rotor wheels of the compressor rotor, the first cooling path directing the cooled cooling air across the rotor wheels and into a bore section of the compressor rotor; and

a second cooling path in series with the first cooling path, the second cooling path directing the cooled cooling air across rotor wheels of the turbine rotor.

2. A cooling circuit according to claim 1, wherein the first cooling path is defined by axial holes formed in an inertia belt of the compressor rotor wheels.

3. A cooling circuit according to claim 2, wherein the first cooling path directs the cooled cooling air across a high pressure packing brush seal, through bypass holes in the high pressure packing brush seal, and across an aft rim of a stage 18 compressor wheel.

4. A cooling circuit according to claim 1, wherein the first cooling path comprising a plurality of metering circuits in the compressor rotor wheels, the metering circuits distributing the cooled cooling airflow at compressor flanges for rim cooling, bore cooling and forward stage cooling.

5. A cooling circuit according to claim 1, further comprising impellers in the compressor bore section, the impellers maintaining flow pressure and swirling the cooled cooling airflow to rotor speed.

6. A method of cooling a rotor including a compressor rotor and a turbine rotor, the method comprising:

directing cooled cooling air along a first cooling path defined through openings in rotor wheels of the compressor rotor, the cooled cooling air being directed across the rotor wheels and into a bore section of the compressor rotor; and

directing the cooled cooling air from the first cooling path along a second cooling path in series with the first cooling path, the cooled cooling air being directed across rotor wheels of the turbine.

7. A method according to claim 6, wherein the first cooling path directs the cooled cooling air across a high pressure packing brush seal, through bypass holes in the high pressure packing brush seal, and across an aft rim of a stage 18 compressor wheel.

8. A method according to claim 6, wherein the first cooling path comprising a plurality of metering circuits in the compressor rotor wheels, the method further distributing the cooled cooling airflow via the metering circuits at compressor flanges for rim cooling, bore cooling and forward stage cooling.

9. A method according to claim 6, further comprising maintaining flow pressure and swirling the cooled cooling airflow to rotor speed using impellers in the compressor bore section.

10. A cooling circuit in a rotor including a compressor rotor and a turbine rotor, the cooling circuit comprising a first cooling path through the compressor rotor in series with a second cooling path through the turbine rotor such that one amount of cooling air is used for cooling both the compressor rotor and the turbine rotor.

11. A cooling circuit according to claim 10, wherein the cooling air is delivered through a compressor discharge casing to the first cooling path, the first cooling path being defined to direct the cooling air aftward across rotor wheels of the compressor turbine into a bore section of the compressor rotor and then forward to the second cooling path.