Completed Clean Energy Engineering

Greener Aviation with Advanced Propulsion Systems (GAAPS)

In plain English

AI plain-English summary

The next generation of aircraft will rely on propellers that can spin at variable speeds and are not reversible, a radical departure from the constant-rpm, reversible propellers used in aviation today. This matters because new aircraft designs—from small drones to full-scale hybrid-electric passenger planes—cannot use conventional gas turbine engines efficiently. Current propellers are designed for fixed speeds and full pitch reversal, but the new vehicles need propellers that can operate across a wide range of rpm and are fixed-pitch (non-reversible). There is almost no experimental data on how these propellers perform under real flight conditions, which stalls development. If this research succeeds, it will create a public database of propeller performance data that is not tied to any specific aircraft platform. This would allow manufacturers to design and certify new propulsion systems faster, without having to start from scratch. The project combines computer simulations, advanced manufacturing, wind tunnel tests, and open-air flight testing. The work is applied engineering—it directly targets a bottleneck in making greener, quieter, and more efficient aircraft a practical reality.

View original technical description
A number of novel aircraft configurations is likely to be developed in the next decade. These new aircraft will rely almost exclusively on advanced propellers, because they address flight conditions that are not viable with conventional gas turbine engines. First, there are issues of scaling, as the new vehicles target sub-scale (unmanned) to full scale (manned transport). Second, there are opportunities with hybrid or fully electric propulsions, which scale well at the low power outputs, but require variable-speed propellers. Propellers currently used in aviation operate at constant rpm and are fully reversible. The new propellers addressed in this research operate over a wide range of rpm and are mostly non-reversible (fixed-pitch). Thus, the strategic aims of the proposal is to build understanding of these new propeller systems, to create a database of experimental data that do not depend on a specific flight platform and can be used for further development in the industry. The proposal targets a mix of design, simulation models, advanced manufacturing, wind tunnel testing, open-air flight testing, and builds on several years of experience with rotary-wing systems.

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Researchers

Antonio Filippone (Principal Investigator)George Barakos (Co-Investigator)Khristopher Kabbabe (Co-Investigator)Nicholas Michael Bojdo (Co-Investigator)R Green (Co-Investigator)Rene Steijl (Co-Investigator)William Crowther (Co-Investigator)

Related Research

Grants with similar aims, by meaning.

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Distributed Electric Propulsion
Assessment of turbo-electric propulsion architectures for aircraft
Synergistic Integration of Hyperconducting Electric Propulsion and Composite Structures with Intelligent Morphing for Hydrogen-Powered Aviation
Propeller Aerodynamic Interaction and Noise Characteristics in Distributed Propulsion

Original classification

Research Grant

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