NASA SBIR SUCCESS STORY

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Glenn Research Center 
1993 Phase II

A Software Tool to Design Thermal Barrier Coatings

Deformation Control Technology, Inc.

Cleveland, OH

INNOVATION
Software that enables design of ceramic coatings to enhance coating life and coated component life
Coated Aircraft Gas Turbine Stator Vane
Coated Aircraft Gas Turbine Stator Vane

 

ACCOMPLISHMENTS
  • Successful incorporation of 5 main stress drivers into Thermal Barrier Coating (TBC) model, including oxidation
  • First fundamental description of the role of oxidation in TBC failure
  • Provided first basic statistical descriptors for quantifying interactive material property effects
  • Provided basis for NASA TBC design innovation, patent pending
COMMERCIALIZATION
  • In use to analyze test results and design TBCs for electric power generation turbine applications
  • Commercial contract in excess of $10K was initiated prior to completion of Phase II work
  • Strong commercial interest in future analysis based on the success of an exploratory contract
  • This SBIR project resulted in an increase in employment, from 2 to 3 employees
GOVERNMENT/SCIENCE APPLICATIONS
  • Presently in use to define failure mechanisms in TBCs
  • Continued use to reduce costly experimentation while developing new TBC concepts
  • In support of NASA HITEMP and Hybrid-Hyperspeed programs
For more information about this firm, please send e-mail to company representative

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Curator: SBIR Support                   3/17/06