SBIR/STTR Research Award

Reinforced High Temperature Titanium Metal Matrix Composite Systems For Impeller Applications In Advanced Army Turboshaft Engines

Award identifier fd1b887cf224fc80dab063ce1d8c99ab2e06356c1da248e2e4a3658199eafbf8Awarding agency Department of Defense · Army

Award amount

$729,991

Program and phase

SBIR · Phase II

Award year

2009

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Award details

Awarding agency
Department of Defense
Branch
Army
Recipient company
FMW COMPOSITE SYSTEMS, INC.
Proposal award date
2009-10-01
Contract end date
2011-09-30
UEI
VPQBVVPXNHA3
Solicitation number
2008.2
Topic code
A08-023

Research abstract

Superior high-temperature performance requirements for highly stressed rotating components of the compressor section in advanced Army turboshaft engines cannot be met by the existing materials and require sophisticated materials solution concepts. The objective of this SBIR program is to develop a reinforced high temperature titanium material system for impeller applications in advanced Army turboshaft engines to increase the performance, reduce the specific fuel consumption, and enhance the affordability. FMW, in collaboration with Honeywell Aerospace (aero engine original equipment manufacturer), proposed a nano-enhancement concept in Phase I and demonstrated the proof-of-concept via design trade studies, subscale article fabrication, and preliminary mechanical property evaluations. Nano-enhancement approach identified exceptional potential to meet the performance challenges in advanced turboshaft engine impellers. In Phase II, FMW-Honeywell team proposes to fully develop, optimize, scale-up, and mature the nano-enhanced titanium alloy impeller technology. A prototype impeller article, representative of the turboshaft engine, will be fabricated and machined into a fully-featured article for spin-pit testing. Manufacturability, machinability, and affordability aspects will be evaluated and risk reduction strategies will be developed. Detailed material characterization that includes microstructural quantifications, grain flow analysis, failure mechanisms, and microstructural variability analysis, will be conducted. Extensive testing on coupons extracted from various locations and orientations of the prototype article will be performed to generate material data under static and dynamic loading conditions at room and elevated temperatures relevant for the impeller. Impeller spin test data will be analyzed and compared with the baseline results to quantify the benefits. Phase II research and development effort will mature the nano-enhanced titanium impeller technology readiness to the level necessary for engine test demonstration.

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.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

15 SBIR/STTR records share this UEI (2003–2009). Reported award amounts total $4,512,550. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration

Agency intelligence

Department of Defense

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