NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
High Temperature Performance Evaluation of a Compliant Foil SealThe key points to be gleaned from the effort reported herein are that the CFS (Compliant Foil Seal) has been demonstrated in conjunction with a foil bearing in a small gas turbine simulator at temperatures as high as 1000 F and outperformed a comparable brush seal. Having demonstrated the feasibility of the CFS, it would appear that this new seal design has application potential in a wide range of machines. What remains is to demonstrate performance at higher pressure ratios, consistent performance at large rotor excursions and the ability to manufacture the seal in much larger sizes exceeding by an order of magnitude that which has been tested to date.
Document ID
20020022541
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Salehi, Mohsen
(Mohawk Innovative Technology, Inc. Albany, NY United States)
Heshmat, Hooshang
(Mohawk Innovative Technology, Inc. Albany, NY United States)
Walton, James F., II
(Mohawk Innovative Technology, Inc. Albany, NY United States)
Date Acquired
August 20, 2013
Publication Date
October 1, 2001
Publication Information
Publication: 2000 NASA Seal/Secondary Air System Workshop
Volume: 1
Subject Category
Mechanical Engineering
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available