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Thermal Management System Design for Electrified Aircraft Propulsion Concepts

2020 AIAA/IEEE Electric Aircraft Technologies Symposium (EATS), 2020
This paper describes the development of thermal management systems (TMS) for three electrified aircraft propulsion (EAP) vehicle concepts released by NASA that span the UAM, regional, and single-aisle markets.
Jeffryes W. Chapman   +2 more
semanticscholar   +1 more source

A Cryogenically-Cooled MW Inverter for Electric Aircraft Propulsion

2020 AIAA/IEEE Electric Aircraft Technologies Symposium (EATS), 2020
Power electronic converter will be a key enabler for future electrified aircraft propulsion system. In aircraft applications, superconducting technologies such as superconducting motors and generators along with supporting power systems will grow in ...
Ruirui Chen   +7 more
semanticscholar   +1 more source

Hybrid-Electric Propulsion for Aircraft

Journal of Aircraft, 2015
Against a background of increasing energy demand and rising fuel prices, hybrid-electric propulsion systems have the potential to significantly reduce fuel consumption in the aviation industry, particularly in the lighter sectors. By taking advantage of both electric motor and internal combustion engine, hybrid-electric propulsion systems provide not ...
C. Friedrich, P.A. Robertson
openaire   +1 more source

Propulsion Powertrain Simulator: Future turboelectric distributed-propulsion aircraft

IEEE Electrification Magazine, 2014
The NASA Glenn Research Center, in collaboration with the aerospace industry and academia, has begun the development of technology for a future hybrid wing-body electric airplane with a turboelectric distributed-propulsion (TeDP) system. It is essential to design a subscale system to emulate the TeDP power grid, which would enable rapid analysis and ...
openaire   +1 more source

Trends in Military Aircraft Propulsion

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 1989
The major factors determining the choice of engine cycle for a combat aircraft are the requirements of the design mission and those of aircraft speed and agility. The requirement for jet-borne flight in short take-off vertical landing (STOVL) aircraft imposes further demands on cycle and configuration.
R M Denning, N A Mitchell
openaire   +1 more source

An Advanced Propulsion Motor With Enhanced Winding Cooling System for a Solar-Powered Aircraft

IEEE Transactions on Transportation Electrification
Solar-powered aircraft are being upsized and required to carry more payloads, which poses great challenges for propulsion motors, especially for their cooling considering extreme lightweight. Due to remarkable thermal performance, heat pipes (HPs) become
H. Zhao   +5 more
semanticscholar   +1 more source

Hypersonic flight [scramjet aircraft propulsion]

IEEE Spectrum, 2004
Current turbojet engines cannot propel an aircraft to hypersonic speeds -their spinning shafts and compressors would simply collapse. To solve this problem, groups in the United States, Japan, Australia, and other countries are working on a propulsion system that burns fuel combined with air flowing at supersonic speeds through the engine, which is ...
openaire   +1 more source

The future of aircraft propulsion

Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, 2000
The next century offers many challenges to the aero-engine industry in both the civil and the military markets. The primary driver in both markets will be to reduce the cost of acquiring, operating and supporting the product throughout its life. Reducing the environmental impact will be an additional challenge for the civil sector.
openaire   +1 more source

Lightweight Design of Fully Superconducting Motors for Electrical Aircraft Propulsion Systems

IEEE transactions on applied superconductivity, 2019
This paper describes and discusses fully superconducting motors (FSCMs) for electrical aircraft propulsion systems. The FSCM structures have a potential to reach over 20 kW/kg, thanks to air cored structure and higher current density coils while ...
Y. Terao   +4 more
semanticscholar   +1 more source

Higher thrust-to-power with large electrode gap spacing electroaerodynamic devices for aircraft propulsion

Journal of Physics D: Applied Physics, 2019
Electroaerodynamic (EAD) devices, which produce a propulsive force in air by electrostatic acceleration, have been demonstrated as a method of propulsion for airplanes.
Haofeng Xu   +3 more
semanticscholar   +1 more source

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