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Title: Aerodynamic seal assemblies for turbo-machinery

Patent ·
OSTI ID:1221976

The present application provides an aerodynamic seal assembly for use with a turbo-machine. The aerodynamic seal assembly may include a number of springs, a shoe connected to the springs, and a secondary seal positioned about the springs and the shoe.

Research Organization:
GE Global Research, Niskayuna, New York (United States)
Sponsoring Organization:
USDOE
DOE Contract Number:
FC26-05NT42643
Assignee:
General Electric Company (Niskayuna, NY)
Patent Number(s):
9,145,785
Application Number:
13/040,474
OSTI ID:
1221976
Resource Relation:
Patent File Date: 2011 Mar 04
Country of Publication:
United States
Language:
English

References (10)

Compliant pressure balanced seal apparatus patent May 1997
Compliant foil seal patent January 2003
Turbine rotor-stator leaf seal and related method patent March 2003
Hydrodynamic foil face seal patent August 2007
Sealing device and method for turbomachinery patent October 2008
Seal patent November 2008
Dynamic flange seal and sealing system patent May 2009
Dynamic flange seal and sealing system patent March 2010
Non-Contact Seal for a Gas Turbine Engine patent-application October 2008
Performance of a Complaint Foil Seal in a Small Gas Turbine Engine Simulator Employing a Hybrid Foil/Ball Bearing Support System journal January 2001

Cited By (1)

Aerodynamic seal assemblies for turbo-machinery patent September 2015

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