
Mechanical Property Characterization and Modeling for Structural Mo-Si-B Alloys for High Temperature ApplicationsAward last edited on: 10/25/2018
Sponsored Program
STTRAwarding Agency
DOD : NavyTotal Award Amount
$1,634,726Award Phase
2Solicitation Topic Code
N13A-T012Principal Investigator
Oliver StrbikCompany Information
Phase I
Contract Number: N00014-13-P-1181Start Date: 7/1/2013 Completed: 4/30/2014
Phase I year
2013Phase I Amount
$149,998Benefit:
Mo-Si-B is being investigated as a potential replacement for superalloys. Successful development of Mo-Si-B will result in significant opportunity to: use U.S.-sourced material, improve technical performance of many high-temperature systems, reduce cost, and minimize environmental impact. The successful development of Mo-Si-B promises advantages over superalloys. Mo-Si-B exhibits significantly better oxidation resistance at high temperatures. This makes it useful for many high temperature applications including heat exchangers, furnace elements, and ultimately gas turbine engines. It is estimated that Mo-Si-B used in turbines will allow jets to improve fuel efficiency by 30% via increased hot section temperatures. From a military perspective, increased fuel savings and higher performance engines will allow the U.S. to maintain superiority over adversaries. From a dual use perspective, increased fuel efficiency in commercial aircraft will result in a reduced operating costs and a decrease in the carbon footprint. Thus, Mo-Si-B is also green 0x9D technology. Another important military advantage is that the base materials, molybdenum, silicon, and boron are sourced from U.S. mines. Thus a stable supply of Mo-Si-B is available regardless of international political circumstances.
Keywords:
Superalloy, Superalloy, ICME, Mo-Si-B, Boron, silcon, Molybdenum, MoSiB, Integrated Computational Materials Engineering, Mo-3Si-B
Phase II
Contract Number: N00014-15-C-0069Start Date: 8/6/2015 Completed: 9/25/2019
Phase II year
2015Phase II Amount
$1,484,728Benefit:
Components constructed of Mo-Si-B alloys operating in air at 1300C without cooling would greatly advance turbine technology. This advancement would cut fuel cost and or increase performance of both military and commercial aircraft. In regard to military operation, this material promises higher speed and stronger lift capabilities. In regard to commercial airlines, this material cut fuel cost by 20-40% with a savings approaching the realm of $500 Billion/yr.
Keywords:
refractory metal, Intermetallic, characterization, Mo-Si-B, Oxidation Resistant Alloys, High Temperature, ICME, Molybdenum Alloys