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NASA NTRS ยท 20050179437

Compressor Case Manufactured Using High-Temperature Polyimides

Abstract

High-temperature polymer composites (PMC's) offer lighter weight and higher specific strengths than titanium alloys for advanced aircraft engine applications-especially in fan and compressor components, where temperatures do not exceed 550 F (288 C). VCAP, a polyimide resin developed at the NASA Lewis Research Center, was filament wound at Lincoln Composites in Lincoln, Nebraska, with graphite and glass fibers to produce a lightweight compressor case for an Integrated High Performance Turbine Engine Technology (IHPTET) engine. This engine application requires a PMC that can withstand air pressures (60 psi) and temperatures exceeding the degradation limits of other high-temperature polyimides, such as PMR-15.

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BibTeXRIS

Sutter, James K.. 1997-03-01. Compressor Case Manufactured Using High-Temperature Polyimides. https://ntrs.nasa.gov/citations/20050179437

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