Gas turbine and turbine stationary blade for same

Patent metadata

Field	Value
Publication number	US-9234432-B2
Application number	US-201113641063-A
Country	US
Kind code	B2
Filing date	Apr 11, 2011
Priority date	Apr 15, 2010
Publication date	Jan 12, 2016
Grant date	Jan 12, 2016

Abstract

A gas turbine engine and a turbine stator assembly which is capable of being cooled effectively with a small amount of air. The stator assembly comprises a stator vane disposed to be exposed to a combustion gas passage. The stator vane comprises a cooling passage defined therein. The cooling passage is disposed on an upstream of the gas turbine engine and extending in a radial direction with respect to a central axis of the gas turbine engine. The stator vane also has an inlet communicated to a radially outward end of the cooling passage. The stator vane further has an adjustment member secured to the stator vane so that it covers the inlet. The adjustment member has two apertures for guiding a cooling air radially inwardly through the inlet into the cooling passage. The two apertures are spaced away from each other along a camber line of the stator vane.

First claim

The invention claimed is:

1. A stator blade supported by a turbine casing of a gas turbine engine, the gas turbine engine having a compressor for compressing air, combustors for combusting a mixture of fuel and compressed air supplied from the compressor, and a turbine to be driven by high-temperature and high-pressure combustion gas from the combustors, the turbine having stator assemblies and rotor assemblies positioned alternately in a direction parallel to a central axis of the gas turbine engine, the stator assemblies each having a number stator blades, wherein
the stator blade has
a single air passage defined in the stator blade, the single air passage having a portion positioned on an upstream side and extending in a radial direction of the gas turbine engine;
a single inlet defined in the stator blade to open radially outwardly in communication with the upstream portion of the single air passage;
an adjustment plate covering the single inlet, the adjustment plate having two apertures defined therein for introducing a cooling air radially inwardly into the single inlet, the two apertures being positioned and spaced away from each other on a camber line of the stator blade, the single inlet being elongated along the camber line and having a length along the camber line, one of the two apertures on the upstream side being positioned L/4 to L/3 away from an upstream end of the single inlet and the other on the downstream side being positioned 2L/3 to 3L/4 away from the upstream end of the single inlet; and
a radially outward flange defined in the stator blade, the flange having the single inlet formed therewith and a radially outward surface on which the adjustment plate is fixed.

2. The stator blade of claim 1 , wherein the two apertures are circular in shape having the same inner diameter.

Assignees

• Shinoda Yuji
• Taniguchi Tomoki
• Kawasaki Heavy Ind Ltd

Inventors

• Shinoda Yuji
• Taniguchi Tomoki

Classifications

• F01D9/065 Primary

  Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids (see also F01D25/16, F01D25/24 and F01D25/26) · CPC title

• F01D9/02

  Nozzles; Nozzle boxes; Stator blades; Guide conduits {, e.g. individual nozzles (nozzle boxes F01D9/047)} · CPC title

• F05D2260/201

  by impingement of a fluid · CPC title

• F05D2260/20

  Heat transfer, e.g. cooling · CPC title

• F05D2250/185

  serpentine-like · CPC title