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Title: Gas turbine blade with intra-span snubber

Patent ·
OSTI ID:1149933

A gas turbine blade (10) including a hollow mid-span snubber (16). The snubber is affixed to the airfoil portion (14) of the blade by a fastener (20) passing through an opening (24) cast into the surface (22) of the blade. The opening is defined during an investment casting process by a ceramic pedestal (38) which is positioned between a ceramic core (32) and a surrounding ceramic casting shell (48). The pedestal provides mechanical support for the ceramic core during both wax and molten metal injection steps of the investment casting process.

Research Organization:
National Energy Technology Laboratory (NETL), Pittsburgh, PA, Morgantown, WV (United States)
Sponsoring Organization:
USDOE
DOE Contract Number:
FC26-05NT42644
Assignee:
Siemens Energy, Inc. (Orlando, FL)
Patent Number(s):
8,790,082
Application Number:
12/848,456
OSTI ID:
1149933
Country of Publication:
United States
Language:
English

References (12)

Damping element for independent turbomachine blades patent March 1988
Device for damping vibrations in turbomachinery blades patent October 1991
Components made of hardenable and non-hardenable materials patent September 1993
Investment casting patent April 1996
Aerodynamically optimized mid-span snubber for combustion turbine blade patent December 1997
High efficiency blade configuration for steam turbine patent April 2002
Blade with optimized vibration behavior patent January 2003
Moving blades for steam turbine patent January 2004
Investment casting cores patent August 2005
Aero-mixing of rotating blade structures patent-application June 2008
Snubber Assembly for Turbine Blades patent-application August 2011
Cooled Snubber Structure for Turbine Blades patent-application August 2011

Cited By (3)

Turbine blade mid-span shroud patent March 2017
Turbine blade mid-span shroud assembly patent February 2017
Tapered part-span shroud patent January 2017

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