SBIR/STTR Research Award
Cathodic Arc Synthesis of Sand-Erosion Resistant, Boride Coatings for Titanium Alloy Compressor Impeller Blades
Award amount
$79,959Program and phase
SBIR · Phase IAward year
2005Award details
- Awarding agency
- Department of Defense
- Branch
- Navy
- Recipient company
- HY-Tech Research Corp.
- Proposal award date
- 2004-12-17
- Contract end date
- 2005-06-17
- UEI
- Not reported
- Solicitation number
- 2004.3
- Topic code
- N04-261
Research abstract
In environments where the atmosphere can contain a high concentration of sand, the erosion of jet engine turbine blades becomes a dominant mechanism for reduced aircraft engine lifetime. NAVAIR is seeking a coating solution that will dramatically decrease this sand erosion wear mechanism, especially for titanium alloy impeller blades in the compressor side of its aircraft engines. HY-Tech is offering to apply its surface treatment technology, which is uniquely able to apply a super-high hardness (3 times that of sand), yet low modulus (i.e. elastic, providing good impact resistance), boron-rich thin film coating, with excellent adhesion to titanium alloys (as well as steels). The adhesion is achieved without the need for a bond coating, by using the energetic ions of boron involved in this process to form a reacted diffusion layer. Boron forms strongly bonded compounds with titanium; the compounds themselves are also hard and erosion resistant. The Phase I project will seek to demonstrate this solution by means of sand erosion testing of boron-coated flat-samples at a qualified facility and to determine the relationship of sand erosion performance to the depth and quality of the reacted layer.
Technology keywords
Not reported
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Resistant Coatings for Aircraft Components
- Erosion Resistant Coatings for Shaft-Driven Compressor (SDC) Impellers
- Erosion Resistant Coatings for Shaft-Driven Compressor (SDC) Impellers