NASA electrified aircraft propulsion efforts

This paper aims to review national aeronautics and space administration (NASA’s) broad investments in electrified aircraft propulsion (EAP). NASA investments are guided by an assessment of potential market impacts, technical key performance parameters, and technology readiness attained through a combination of studies, enabling fundamental research and flight research.,The impact of EAP varies by market and NASA is considering three markets as follows: national/international, on-demand mobility and short-haul regional air transport. Technical advances in key areas have been made that indicate EAP is a viable technology. Flight research is underway to demonstrate integrated solutions and inform standards and certification processes.,A key finding is that sufficient technical advances in key areas have been made, which indicate EAP is a viable technology for aircraft. Significant progress has been made to reduce EAP adoption barriers and further work is needed to transition the technology to a commercial product and improve the technology, so it is applicable to large transonic aircraft.,Significant progress has been made to reduce EAP adoption barriers and further work is needed to transition the technology to a commercial product and improve the technology, so it is applicable to large transonic aircraft.,This paper will review the activities of the hybrid gas-electric subproject of the Advanced Air Transport Technology Project, the Revolutionary Vertical Lift Technology Project and the X-57 Flight Demonstration Project, and discuss the potential EAP benefits for commercial and military applications. This paper focuses on the vehicle-related activities, however, there are related NASA activities in air space management and vehicle autonomy activities, as well as a breakthrough technology project called the Convergent Aeronautics Solutions Project. The target audience is people interested in EAP.

[1]  Christopher K. Droney,et al.  Subsonic Ultra Green Aircraft Research Phase II: N+4 Advanced Concept Development , 2012 .

[2]  Aamod Samuel,et al.  NASA SCEPTOR electric concept aircraft power system: X-plane electric propulsion system design and qualification for crewed flight testing , 2016, 2016 IEEE Transportation Electrification Conference and Expo (ITEC).

[3]  Gerald V. Brown,et al.  Turboelectric Distributed Propulsion in a Hybrid Wing Body Aircraft , 2011 .

[4]  Kiruba Haran,et al.  System Weight Comparison of Electric Machine Topologies for Electric Aircraft Propulsion , 2018, 2018 AIAA/IEEE Electric Aircraft Technologies Symposium (EATS).

[5]  Wayne Johnson,et al.  VTOL Urban Air Mobility Concept Vehicles for Technology Development , 2018, 2018 Aviation Technology, Integration, and Operations Conference.

[6]  Justin J. Scheidler,et al.  High Efficiency Megawatt Motor Conceptual Design , 2018, 2018 Joint Propulsion Conference.

[7]  Ralph Jansen Overview of NASA Electrified Aircraft Propulsion Activities , 2017 .

[8]  Leon M. Tolbert,et al.  Design of a Single Controller for Multiple Paralleled Inverters , 2019, 2019 IEEE Applied Power Electronics Conference and Exposition (APEC).

[9]  Larry W. Hardin,et al.  Parallel Hybrid Gas-Electric Geared Turbofan Engine Conceptual Design and Benefits Analysis , 2016 .

[10]  Ralph Jansen,et al.  Partially Turboelectric and Hybrid Electric Aircraft Drive Key Performance Parameters , 2018, 2018 AIAA/IEEE Electric Aircraft Technologies Symposium.

[11]  Andrew R. Gibson,et al.  Design and Performance of the NASA SCEPTOR Distributed Electric Propulsion Flight Demonstrator , 2016 .

[12]  James L. Felder,et al.  Turbo- and Hybrid-Electrified Aircraft Propulsion Concepts for Commercial Transport , 2018, 2018 AIAA/IEEE Electric Aircraft Technologies Symposium (EATS).

[13]  Dimitri N. Mavris,et al.  Cycle Selection and Sizing of a Single-Aisle Transport with the Electrically Variable Engine(TM) (EVE) for Fleet Level Fuel Optimization , 2017 .

[14]  Nicholas K. Borer,et al.  A Method for Designing Conforming Folding Propellers , 2017 .

[15]  Sean Clarke Aircraft Electric Propulsion Systems Applied Research at NASA , 2015 .

[16]  Gerald V. Brown,et al.  Turboelectric Aircraft Drive Key Performance Parameters and Functional Requirements , 2015 .

[17]  Wayne Johnson,et al.  Concept Vehicles for VTOL Air Taxi Operations , 2018 .

[18]  Jens Friedrichs,et al.  Conceptual Design of Operation Strategies for Hybrid Electric Aircraft , 2018 .