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"Turbine Blade Nested Seal Damper Assembly"

Abstract: A turbine blade damper seal assembly includes a seal and a damper that both abut a radially outermost non-gas path surface. The seal is fabricated from a plastically deformable material and nests within a recess of the damper. The damper is fabricated from a rigid material that absorbs vibrational energy generated during operation. The recess within the damper provides for both the damper and the seal to be positioned at the radially outermost non-gas path surface.

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Patent Information

Application #
Filing Date
19 May 2005
Publication Number
02/2007
Publication Type
INA
Invention Field
MECHANICAL ENGINEERING
Status
Email
Parent Application

Applicants

UNITED TECHNOLOGIES CORPORATION
ONE FINANCIAL PLAZA, HARTFORD, CONNECTICUT 06103, U.S.A.

Inventors

1. BEATTIE JEFFREY
29 GREENHURST ROAD, WEST HARTFORD, CONNECTICUT 06107, U.S.A.

Specification

Documents

Application Documents

# Name Date
1 1291-del-2005-form-1.pdf 2011-08-21