# US 6,065,282 A · System for cooling blades in a gas turbine

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- Number: US 6,065,282 A
- Document ID: US6065282A
- Status: Granted
- Kind: A
- Application number: 08/960,466
- Filed: 1997-10-29
- Granted: 2000-05-23
- Earliest claimed: 1997-10-29
- Assignees: Mitsubishi Heavy Industries, Ltd.
- Inventors: Ichiro Fukue; Eiji Akita; Yasuoki Tomita
- Web page: https://patentgrep.com/patent/US6065282A

## CPC

- F02C 7/185: {Cooling means for reducing the temperature of the cooling air or gas}
- F05D 2260/205: Cooling fluid recirculation, i.e. after cooling one or more components is the cooling fluid recovered and used elsewhere for other purposes
- F02C: GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS (construction of turbines F01D; jet-propulsion plants F02K; construction of compressors or fans F04; generating combustion products of high pressure or high velocity F23R; using gas turbines in compression refrigeration plants F25B11/00)
- F05D: INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS

## Abstract

A gas turbine comprises: a first closed circuit in which cooling gas is supplied to a casing, allowed to pass through stationary blades, and removed to the outside of casing after cooling the stationary blades; a second closed circuit in which cooling air is supplied to the casing, allowed to pass through moving blades, and removed to the outside of casing after cooling the moving blades; a cooler for cooling the cooling gas in the first and second closed circuits; and a booster for pressurizing and circulating the cooling gas cooled by the cooler. Also, A gas turbine comprises: a first closed circuit in which cooling air cooled after being extracted from a combustor plenum is allowed to pass through stationary blades successively to cool the stationary blades, and then recovered and returned to a compressor on the upstream side of the combustor plenum; and a second closed circuit in which cooling air cooled after being extracted from the combustor plenum is allowed to pass through moving blades successively to cool the moving blades, and then recovered and returned to the compressor.

## Claims

### Claim 1

A gas turbine comprising: a compressor;
a combustor plenum downstream of said compressor;
stationary and moving blades;
a cooling air cooler;
first and second closed cooling circuits which extract cooling air from said combustor plenum and pass the cooling air through said cooler, the first closed circuit supplying cooling air from said cooler successively through said stationary blades to cool said stationary blades and then recovering the cooling air and returning the cooling air to said compressor, and the second closed circuit supplying cooling air from said cooler successively through said moving blades to cool said moving blades and then recovering the cooling air and returning the cooling air to said compressor; and
a booster returning the cooling air received from the stationary and moving blades of said first and second closed circuits to the compressor.

### Claim 2 (depends on 1)

The gas turbine of claim 1, further comprising a steam turbine operating in conjunction with the gas turbine to form a combined cycle, steam from said steam turbine being supplied to said air cooler for cooling the cooling air.