Rapid Sustainment Office (RSO) Experimental Purposes: AM Metals Printer and Material Qualifications
Closed Solicitation Posted
- Solicitation number
- FA8684-23-9-R001
- Agency
-
Lifecycle Management Center
Air Force Materiel Command, Department of Defense
- Responses due
- Set-aside
- No set-aside
Opportunity facts
- NAICS code
- 541330 Engineering Services
- PSC
- 7650 Drawings And Specifications
Notice details come from SAM.gov. Updated .
About this opportunity
The Air Force Life Cycle Management Center is soliciting proposals for an experimental project involving the purchase of two metal printers and the testing of high strength aluminum alloys for aircraft component production. The project aims to demonstrate the ability to use metal additive manufacturing technologies to fabricate and develop aerospace parts for flightworthy applications and production support application. The period of performance for this contract is projected to be 15 months for the base, with options for extensions, and proposals are due by August 8, 2023.
Products and Services to be provided:
- Two metal printers of models currently owned by the DAF (EOS, GE M2 Series 5 Concept Laser, Velo3D Sapphire).
- Complete MMPDS equivalent S-basis dataset for a high strength aluminum alloy.
- Testing and evaluation of tensile, fatigue, and physical properties of the selected high strength aluminum alloy.
- Minimum 30 tensile tests per orientation and Minimum 54 fatigue samples.
- Draft specifications for powder, heat treatment, and material printed in the selected printer.
Notice text
The AMPO seeks an innovative solution designed to expand on current DAF capabilities to produce aircraft components via metal additive manufacturing. The desired outcome of this solicitation seeks to acquire two metal printers of models currently owned by the DAF (EOS, GE M2 Series 5 Concept Laser, Velo3D Sapphire) to complete MMPDS equivalent S-basis dataset for a high strength aluminum alloy, such as A6061-RAM2, A7050-RAM2, or A205, sufficient for structural, non-critical applications, demonstrating an ability to use metal AM technologies to fabricate and develop aerospace parts for flightworthy applications and production support application. Experimentation on the selected high strength aluminum alloy shall include testing and evaluation of tensile, fatigue, and physical properties (Young’s and shear modulus, mean coefficient of thermal expansion, thermal conductivity, and specific heat) with Minimum 30 tensile tests per orientation and Minimum 54 fatigue samples, i.e., 9 samples for each stress ratio and level combination (3 stress levels and 2 stress ratios). Draft specifications for powder, heat treatment, and material printed in the selected printer will be developed in the base period. This effort is not intended to be an alloy development effort but is an experimental additive manufacturing evaluation utilizing an available alloy.
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