Architecture, Voltage and Components for a Turboelectric Distributed Propulsion Electric Grid
Armstrong, Michael J. and Blackwelder, Mark and Bollman, Andrew and Ross, Christine and Campbell, Angela and Jones, Catherine and Norman, Patrick (2015) Architecture, Voltage and Components for a Turboelectric Distributed Propulsion Electric Grid. NASA, US.
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Abstract
The development of a wholly superconducting turboelectric distributed propulsion system presents hide unique opportunities for the aerospace industry. However, this transition from normally conducting systems to superconducting systems significantly increases the equipment complexity necessary to manage the electrical power systems. Due to the low technology readiness level (TRL) nature of all components and systems, current Turboelectric Distributed Propulsion (TeDP) technology developments are driven by an ambiguous set of system-level electrical integration standards for an airborne microgrid system (Figure 1). While multiple decades' worth of advancements are still required for concept realization, current system-level studies are necessary to focus the technology development, target specific technological shortcomings, and enable accurate prediction of concept feasibility and viability. An understanding of the performance sensitivity to operating voltages and an early definition of advantageous voltage regulation standards for unconventional airborne microgrids will allow for more accurate targeting of technology development. Propulsive power-rated microgrid systems necessitate the introduction of new aircraft distribution system voltage standards. All protection, distribution, control, power conversion, generation, and cryocooling equipment are affected by voltage regulation standards. Information on the desired operating voltage and voltage regulation is required to determine nominal and maximum currents for sizing distribution and fault isolation equipment, developing machine topologies and machine controls, and the physical attributes of all component shielding and insulation. Voltage impacts many components and system performance.
ORCID iDs
Armstrong, Michael J., Blackwelder, Mark, Bollman, Andrew, Ross, Christine, Campbell, Angela, Jones, Catherine ORCID: https://orcid.org/0000-0001-7524-5756 and Norman, Patrick ORCID: https://orcid.org/0000-0001-5577-1281;-
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Item type: Report ID code: 54548 Dates: DateEvent1 July 2015PublishedSubjects: Technology > Motor vehicles. Aeronautics. Astronautics
Technology > Electrical engineering. Electronics Nuclear engineeringDepartment: Faculty of Engineering > Electronic and Electrical Engineering Depositing user: Pure Administrator Date deposited: 13 Oct 2015 09:43 Last modified: 28 Nov 2024 01:34 Related URLs: URI: https://strathprints.strath.ac.uk/id/eprint/54548