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A Fully Non-metallic Gas Turbine Engine Enabled by Additive ManufacturingThe Non-Metallic Gas Turbine Engine project, funded by NASA Aeronautics Research Institute (NARI), represents the first comprehensive evaluation of emerging materials and manufacturing technologies that will enable fully nonmetallic gas turbine engines. This will be achieved by assessing the feasibility of using additive manufacturing technologies for fabricating polymer matrix composite (PMC) and ceramic matrix composite (CMC) gas turbine engine components. The benefits of the proposed effort include: 50 weight reduction compared to metallic parts, reduced manufacturing costs due to less machining and no tooling requirements, reduced part count due to net shape single component fabrication, and rapid design change and production iterations. Two high payoff metallic components have been identified for replacement with PMCs and will be fabricated using fused deposition modeling (FDM) with high temperature capable polymer filaments. The first component is an acoustic panel treatment with a honeycomb structure with an integrated back sheet and perforated front sheet. The second component is a compressor inlet guide vane. The CMC effort, which is starting at a lower technology readiness level, will use a binder jet process to fabricate silicon carbide test coupons and demonstration articles. The polymer and ceramic additive manufacturing efforts will advance from monolithic materials toward silicon carbide and carbon fiber reinforced composites for improved properties. Microstructural analysis and mechanical testing will be conducted on the PMC and CMC materials. System studies will assess the benefits of fully nonmetallic gas turbine engine in terms of fuel burn, emissions, reduction of part count, and cost. The proposed effort will be focused on a small 7000 lbf gas turbine engine. However, the concepts are equally applicable to large gas turbine engines. The proposed effort includes a multidisciplinary, multiorganization NASA - industry team that includes experts in ceramic materials and CMCs, polymers and PMCs, structural engineering, additive manufacturing, engine design and analysis, and system analysis.
Document ID
20150002084
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Grady, Joseph E.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
February 25, 2015
Publication Date
September 3, 2014
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN17465
Meeting Information
Meeting: JANNAF Technical Interchange Meeting on Additive Manufacturing for Propulsion Applications
Location: Huntsville, AL
Country: United States
Start Date: September 3, 2014
End Date: September 5, 2014
Sponsors: NASA Headquarters, Department of the Navy, Department of the Army
Funding Number(s)
WBS: WBS 694478.02.93.02.14.64.22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
manufacturing
materials
composites
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