NDLI: Turboelectric aircraft drive key performance parameters and functional requirements

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Turboelectric aircraft drive key performance parameters and functional requirements

Content Provider	NASA Technical Reports Server (NTRS)
Author	Felder, James L. Duffy, Kirsten P. Brown, Gerald V. Jansen, Ralph
Copyright Year	2015
Description	The purpose of this presentation is to propose specific power and efficiency as the key performance parameters for a turboelectric aircraft power system and investigate their impact on the overall aircraft. Key functional requirements are identified that impact the power system design. Breguet range equations for a base aircraft and a turboelectric aircraft are found. The benefits and costs that may result from the turboelectric system are enumerated. A break-even analysis is conducted to find the minimum allowable electric drive specific power and efficiency that can preserve the range, initial weight, operating empty weight, and payload weight of the base aircraft.
File Size	407280
Page Count	17
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_20150021285
Archival Resource Key	ark:/13960/t1gj4h45v
Language	English
Publisher Date	2015-07-27
Access Restriction	Open
Subject Keyword	Aircraft Engines Hybrid Propulsion Aircraft Configurations Propulsion System Performance Turbogenerators Propulsive Efficiency Fuel Consumption Functional Design Specifications Systems Engineering Electric Power Mathematical Models Thermal Analysis Power Efficiency Cost Analysis Payloads Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Presentation

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