Turbine impeller comprising blade with squealer tip

Patent metadata

Field	Value
Publication number	US-9255481-B2
Application number	US-201213706522-A
Country	US
Kind code	B2
Filing date	Dec 6, 2012
Priority date	Dec 6, 2011
Publication date	Feb 9, 2016
Grant date	Feb 9, 2016

Abstract

A turbine impeller including a rotor; a blade extending from the rotor from a first end of the blade; and a squealer tip provided at a second end opposite to the first end of the blade, wherein at least one perforated portion penetrates through the squealer tip.

First claim

What is claimed is:

1. A turbine impeller comprising:
a rotor;
a blade extending from the rotor from a first end of the blade; and
a squealer tip provided at a second end of the blade opposite to the first end,
wherein at least one perforated portion penetrates through the squealer tip,
wherein a first perforated portion of the at least one perforated portion penetrates through a portion of a pressure surface of the blade closer to a leading edge of the blade than to a trailing edge of the blade,
wherein a second perforated portion of the at least one perforated portion penetrates through a portion of a suction surface of the blade closer to the trailing edge of the blade than to the leading edge of the blade,
wherein the first perforated portion of the pressure surface of the blade is configured to guide a fluid to flow from an exterior of the blade into the squealer tip and the second perforated portion of the suction surface of the blade is configured to guide the fluid from the interior of the squealer tip to the exterior of the blade,
wherein a cross-sectional area of the first perforated portion of the pressure surface of the blade decreases in a direction from the exterior of the blade to an interior of the squealer tip, and
wherein a cross-sectional area of the second perforated portion of the suction surface of the blade decreases in a direction from the interior of the squealer tip to the exterior of the blade.

2. The turbine impeller of claim 1 , wherein surfaces of the squealer tip contacting the at least one perforated portion comprise nozzle shapes.

3. The turbine impeller of claim 1 , wherein the cross-sectional area of the first perforated portion continuously decreases from a first surface provided on the exterior of the blade to a second surface provided on the interior of the squealer tip, and
wherein the cross-sectional area of the second perforated portion continuously decreases from a third surface provided on the interior of the squealer tip to a fourth surface provided on the exterior of the blade.

4. The turbine impeller of claim 1 , wherein each of the first perforated portion and the second perforated portion has a non-divergent nozzle shape.

Assignees

• Hanwha Techwin Co Ltd

Inventors

• Lim Chan-Sun

Classifications

• F01D5/20 Primary

  Specially-shaped blade tips to seal space between tips and stator {(F01D5/225 takes precedence)} · CPC title

• F01D5/145 Primary

  Means for influencing boundary layers or secondary circulations (for compressors F04D29/68) · CPC title

• F01D5/02

  Blade-carrying members, e.g. rotors (rotors of non-bladed type F01D1/34; stators F01D9/00 {; selecting particular materials F01D5/28}) · CPC title

• F01D25/00

  Component parts, details, or accessories, not provided for in, or of interest apart from, other groups · CPC title

• F01D5/14 Primary

  Form or construction (selecting particular materials, measures against erosion or corrosion F01D5/28) · CPC title