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Title: Cooled snubber structure for turbine blades

Patent ·
OSTI ID:1129071

A turbine blade assembly in a turbine engine. The turbine blade assembly includes a turbine blade and a first snubber structure. The turbine blade includes an internal cooling passage containing cooling air. The first snubber structure extends outwardly from a sidewall of the turbine blade and includes a hollow interior portion that receives cooling air from the internal cooling passage of the turbine blade.

Research Organization:
Siemens Energy, Inc., Orlando, FL (United States)
Sponsoring Organization:
USDOE
DOE Contract Number:
FC26-05NT42644
Assignee:
Siemens Energy, Inc. (Orlando, FL)
Patent Number(s):
8,684,692
Application Number:
13/023,651
OSTI ID:
1129071
Resource Relation:
Patent File Date: 2011 Feb 09
Country of Publication:
United States
Language:
English

References (8)

Method of repairing turbine blades patent September 1989
Turbine lashing structure patent November 1993
Rotor blade damping structure for axial-flow turbine patent April 1996
Aerodynamically optimized mid-span snubber for combustion turbine blade patent December 1997
Moving blades for steam turbine patent January 2004
Serpentine cooling circuit and method for cooling tip shroud patent March 2010
Part span shrouded fan blisk patent July 2010
Turbine blade damping device with controlled loading patent September 2013

Cited By (2)

Turbine blade mid-span shroud patent March 2017
Turbine blade mid-span shroud assembly patent February 2017

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