SBIR/STTR Research Award
Coated Ceramic Matrix Composite (CMC) Low Pressure Turbine (LPT) Blade Development
Award amount
$99,957Program and phase
SBIR · Phase IAward year
2009Award details
- Awarding agency
- Department of Defense
- Branch
- Air Force
- Recipient company
- DIVERSITECH, INC.
- Proposal award date
- 2009-04-05
- Contract end date
- 2010-01-05
- UEI
- H6CYJE7JM175
- Solicitation number
- 2008.3
- Topic code
- AF083-108
Research abstract
The objective of this program is to develop an integrated approach for the development of methods for the prediction and manufacture of special features such as holes, cooling channels, dovetails, leading and trailing edges in ceramic composite turbine blades. BENEFIT: The development of cooled ceramic composite turbine components will extend the engine operating efficiencies to a new level. This will aid the reduction in fuel consumption and reduced engine weights for future engine applications
Technology keywords
Not reported
Other awards by this recipient
Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.
- Rotating Intershaft Brush Seals For Sealing Between Two Rotating Shafts
- Rotating Intershaft Brush Seals For Sealing Between Two Rotating Shafts
- Shrink Fit Bling Shroud
- LOW NOISE EXHAUST NOZZLE FOR A HIGH FLOW,LOW PRESSURE HSCT ENGINE
- Variable Flow Fan
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Ceramic Matrix Composite Low Pressure Turbine Blade Development
- Ceramic Matrix Composite (CMC) Low Pressure Turbine (LPT) Blade Development
- Coated Ceramic Matrix Composite (CMC) Low Pressure Turbine (LPT) Blade Development
Research funding history
8 SBIR/STTR records share this UEI (1995–2009). Reported award amounts total $1,956,755. Reported amounts are not federal obligations.
Phases: Phase I, Phase II
Agencies: Department of Defense, National Aeronautics and Space Administration