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Title: Turbine blade with contoured chamfered squealer tip

Abstract

A squealer tip formed from a pressure side tip wall and a suction side tip wall extending radially outward from a tip of the turbine blade is disclosed. The pressure and suction side tip walls may be positioned along the pressure sidewall and the suction sidewall of the turbine blade, respectively. The pressure side tip wall may include a chamfered leading edge with film cooling holes having exhaust outlets positioned therein. An axially extending tip wall may be formed from at least two outer linear surfaces joined together at an intersection forming a concave axially extending tip wall. The axially extending tip wall may include a convex inner surface forming a radially outer end to an inner cavity forming a cooling system. The cooling system may include one or more film cooling holes in the axially extending tip wall proximate to the suction sidewall, which promotes increased cooling at the pressure and suction sidewalls.

Inventors:
Issue Date:
Research Org.:
Siemens Energy, Inc., Orlando, FL (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1166772
Patent Number(s):
8920124
Application Number:
13/767,019
Assignee:
Siemens Energy, Inc. (Orlando, FL)
Patent Classifications (CPCs):
F - MECHANICAL ENGINEERING F01 - MACHINES OR ENGINES IN GENERAL F01D - NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
DOE Contract Number:  
FC26-05NT42644
Resource Type:
Patent
Country of Publication:
United States
Language:
English
Subject:
42 ENGINEERING

Citation Formats

Lee, Ching-Pang. Turbine blade with contoured chamfered squealer tip. United States: N. p., 2014. Web.
Lee, Ching-Pang. Turbine blade with contoured chamfered squealer tip. United States.
Lee, Ching-Pang. Tue . "Turbine blade with contoured chamfered squealer tip". United States. https://www.osti.gov/servlets/purl/1166772.
@article{osti_1166772,
title = {Turbine blade with contoured chamfered squealer tip},
author = {Lee, Ching-Pang},
abstractNote = {A squealer tip formed from a pressure side tip wall and a suction side tip wall extending radially outward from a tip of the turbine blade is disclosed. The pressure and suction side tip walls may be positioned along the pressure sidewall and the suction sidewall of the turbine blade, respectively. The pressure side tip wall may include a chamfered leading edge with film cooling holes having exhaust outlets positioned therein. An axially extending tip wall may be formed from at least two outer linear surfaces joined together at an intersection forming a concave axially extending tip wall. The axially extending tip wall may include a convex inner surface forming a radially outer end to an inner cavity forming a cooling system. The cooling system may include one or more film cooling holes in the axially extending tip wall proximate to the suction sidewall, which promotes increased cooling at the pressure and suction sidewalls.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Tue Dec 30 00:00:00 EST 2014},
month = {Tue Dec 30 00:00:00 EST 2014}
}

Works referenced in this record:

Chordally bifurcated turbine blade
patent, October 1994


Turbine blade having tip slot
patent, April 1996


Slot cooled blade tip
patent, March 1998


Conduction blade tip
patent, April 1998


Ribbed turbine blade tip
patent, December 1999


Tapered tip turbine blade
patent, July 2000


Method and apparatus for reducing turbine blade tip temperatures
patent, July 2002


Foil formed structure for turbine airfoil tip
patent, October 2003


Turbine blade having angled squealer tip
patent, January 2004


Turbine airfoil curved squealer tip with tip shelf
patent, October 2007


Blunt tip turbine blade
patent, October 2007


Turbine airfoil with curved squealer tip
patent, November 2007


Skewed tip hole turbine blade
patent, March 2009


Counter tip baffle airfoil
patent, October 2009


Conformal tip baffle airfoil
patent, March 2010


Plasma blade tip clearance control
patent, October 2010


Method and Apparatus for Reducing Turbine Blade Tip Temperatures
patent-application, July 2002


Cooled thermal barrier coating on a turbine blade tip
patent-application, October 2002


Tip ramp turbine blade
patent-application, February 2008


Cascade tip baffle airfoil
patent-application, December 2009


Aerofoil
patent-application, February 2010


Turbine Blade for a Gas Turbine Engine
patent-application, June 2010


Flared tip turbine blade
patent-application, September 2010


Turbine Blade with Chamfered Squealer Tip and Convective Cooling Holes
patent-application, November 2012


Cooled Turbine Blade for Gas Turbine Engine
patent-application, June 2013