Patent attributes
A turbine blade having a cooling supply passage formed within the blade, and a blade tip with a squealer tip formed thereon. The blade tip includes a blade top or cap, and includes a plurality of mini-serpentine cooling channels formed within the tip. The mini-serpentine channels can be 2-pass, 3-pass, 4-pass, or 5-pass serpentine channels, and each includes an inlet hole connected to the internal cooling supply passage to pass cooling air through the channels. Each channel includes an exit hole with a diffuser that opens onto the pressure side of the blade to provide film cooling. The mini-serpentine cooling channels can be arranged to flow substantially from blade side to side or from blade edge to edge.