You are here

A Novel Erosion Resistant Coating for High-Temperature Composites

Award Information
Agency: Department of Defense
Branch: Air Force
Contract: FA8650-04-M-5007
Agency Tracking Number: F041-131-1862
Amount: $100,000.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: AF04-131
Solicitation Number: 2004.1
Timeline
Solicitation Year: 2004
Award Year: 2004
Award Start Date (Proposal Award Date): 2004-03-10
Award End Date (Contract End Date): 2004-12-10
Small Business Information
7607 Eastmark Drive, Suite 102
College Station, TX 77840
United States
DUNS: 184758308
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Charles Tennakoon
 Senior Research Scientist
 (979) 693-0017
 charles.tennakoon@lynntech.com
Business Contact
 G. Hitchens
Title: Vice President
Phone: (979) 693-0017
Email: duncan.hitchens@lynntech.com
Research Institution
N/A
Abstract

High-temperature polymer matrix composite (HTPMC) components for gas turbine engines have significant advantages over the currently used metal components, including weight savings, strength improvements, lower part counts, and reduced manufacturing costs. However, HTPMCs have a critical need for developing an improved metallic bond coat with a highly erosion resistant top coat before they can be widely used. Lynntech, Inc. proposes a novel process to deposit a functionally gradient metal matrix ceramic composite coating on a metallic bond coat followed by a surface modification process to produce a highly erosion resistant crack-free coating. Both coating and surface modification steps are suited for implementation on HTPMC surfaces. In Phase I, appropriate coating compositions will be determined by erosion resistance measurements conducted in an independent laboratory. The erosion test results will be submitted to the engine manufacturer supplying the HTPMCs; optimization work will be done with their consultation. The successful completion of this Phase I study will enable the coating process to be implemented on engine components to be tested by an already identified turbine engine manufacturer during a possible follow-on-Phase II project.

* Information listed above is at the time of submission. *

US Flag An Official Website of the United States Government