Compressor Development for Exoskeletal Turbine-Based Combined Cycle (TBCC) Engine | Summary and Q&A
TL;DR
NASA is researching low-cost alternatives for space access, including the use of an all-composite and ceramic exoskeletal engine design that eliminates heavier metallic turbomachinery found in jet engines.
Key Insights
- π NASA is researching low-cost alternatives for space access and high Mach number propulsion.
- π The exoskeletal engine design replaces heavier metallic turbomachinery with lighter all-composite and ceramic components.
- π The design eliminates stresses on components and increases blade life.
- β The exoskeletal engine design is suitable for powering small unmanned aerial vehicles, mobile power generators, and supersonic/hypersonic applications.
- π Design considerations include the use of high-temperature ceramic-matrix composites, single-crystal superalloys, and continuous-fiber metal-matrix composites.
- π£ 3D-printed exoskeletal compressor development architecture is motivated by materials and structure science technologies.
- π«’ The hollow-core ESE concept addresses hybrid electric gas turbine and turbogenerator needs.
Transcript
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Questions & Answers
Q: How does NASA's exoskeletal engine design differ from conventional jet engines?
The exoskeletal engine design replaces heavy metallic turbomachinery with lighter all-composite and ceramic components, reducing weight and increasing blade life. It uses rotating casings to support the blades in spanwise compression, eliminating stresses on components.
Q: What are the potential applications for the exoskeletal engine design?
The exoskeletal engine design is suitable for small unmanned aerial vehicles, mobile power generators, and supersonic/hypersonic applications. Its reduced weight and small parts count make it ideal for these applications.
Q: What are the key design considerations for the compressor development architecture?
The key design considerations include the use of high-temperature ceramic-matrix composites and single-crystal superalloys, continuous-fiber metal-matrix composites, a 3D-printed exoskeletal compressor development architecture, and the utilization of existing magnetic bearings.
Q: What is the objective of NASA's Exoskeletal Engine Design Challenge?
The objective of the challenge is for teams of undergraduate students to synthesize a compressor development architecture where the rotating blades are in compression rather than tension. NASA Glenn will provide the geometry of the compressor blades.
Summary & Key Takeaways
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NASA Glenn Research Center is researching low-cost alternatives for access to space and high Mach number propulsion.
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The exoskeletal engine design replaces conventional metallic turbomachinery in jet engines with all-composite and ceramic components.
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The design eliminates stresses on components, increases blade life, and is ideal for powering small unmanned aerial vehicles, mobile power generators, and supersonic/hypersonic applications.