Progressive Damage Model Benchmarking for Ceramic Matrix Composite Components in Turbine Engine Applications
Closed Solicitation Posted
This opportunity was awarded. See the award notice from .
- Solicitation number
- FA8650-19-S-5001
- Agency
- Air Force Research Laboratory Air Force Materiel Command, Department of Defense
- Responses due
- Set-aside
- No set-aside
Opportunity facts
- NAICS code
- 541715 Research and Development in the Physical, Engineering, and Life Sciences (except Nanotechnology and Biotechnology)
- PSC
- Not on record
- Place of performance
- Contractor Facility, United States
Notice details come from SAM.gov. Updated .
Notice text
The Air Force Research Laboratory seeks to develop and transition technology for the certification of life critical turbine engine components utilizing advanced high temperature ceramic matrix composite (CMC) materials. Traditionally, life critical engine components are certified and sustained through a damage tolerance assessment approach where part inspection enables safe operation when accurate means are available to predict rate of damage growth. While progressive damage models are well developed and certified for damage tolerance based certification of metal based components, they are not for CMCs. To these end, the Air Force Research Laboratory is seeking to benchmark current capability of progressive damage models for damage tolerance assessment of CMC turbine engine components..
Attachments
| File | Type | Posted |
|---|---|---|
| FA8650-19-S-5001-BAA-Amd3.pdf | ||
| FA8650-19-S-5001-BAA-Amd2.pdf | ||
| FA8650-19-S-5001-BAA-Amd1.pdf | ||
| FA8650-19-S-5001-Atch3.pdf | ||
| FA8650-19-S-5001-Atch1.pdf | ||
| FA8650-19-S-5001-Atch4.pdf | ||
| FA8650-19-S-5001-Atch6.pdf | ||
| FA8650-19-S-5001-Atch2.pdf | ||
| FA8650-19-S-5001-Atch5.pdf | ||
| FA8650-19-S-5001-BAA.pdf |
Notice history
| Notice | Type | Posted |
|---|---|---|
| Progressive Damage Model Benchmarking for Ceramic Matrix Composite Components in Turbine Engine Applications | Award Notice | |
| Progressive Damage Model Benchmarking for Ceramic Matrix Composite Components in Turbine Engine Applications | Solicitation |
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