Development of a Nonmetallic Abradable Material System for Gas Turbine Applications PUBLIC ACCESS

[+] Author Affiliations
Daniel P. Rose, Jr., George D. Price

Allied Signal Aerospace Company, Phoenix, AZ

Alexander Bosna

Copperlok, Inc, Hatboro, PA

Paper No. 93-GT-425, pp. V03CT17A086; 9 pages
  • ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 3C: General
  • Cincinnati, Ohio, USA, May 24–27, 1993
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7892-7
  • Copyright © 1993 by ASME


The performance of gas turbine engines is highly dependent upon the clearance between compressor rotating blades or stator vanes, and adjacent shrouds. Auxiliary power units (APU) incorporate abradable coatings on compressor shrouds to allow for very small clearances and rub tolerance. The operating environment of the APU may result in a combination of abrasion between airfoil tips and shrouds, as well as galvanic corrosion of the abradable material. Experience has shown that established thermal spray abradable material systems that offer desirable abradability properties in laboratory testing may perform poorly when subjected to a combination of galvanic corrosion and abradable environment.

This paper discusses development and evaluation of an abradable material that is composed of nonmetallic constituents. This material is not susceptible to galvanic corrosion, and maintains its abradable properties when operating in a combined corrosive and abradable environment. The material development, microstructure, and physical properties are discussed. In addition, the performance of the material in abradability testing, and warm salt fog testing is presented.

Copyright © 1993 by ASME
Topics: Gas turbines
This article is only available in the PDF format.



Interactive Graphics


Country-Specific Mortality and Growth Failure in Infancy and Yound Children and Association With Material Stature

Use interactive graphics and maps to view and sort country-specific infant and early dhildhood mortality and growth failure data and their association with maternal

Citing articles are presented as examples only. In non-demo SCM6 implementation, integration with CrossRef’s "Cited By" API will populate this tab (http://www.crossref.org/citedby.html).

Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In