Skip to main content Accessibility help
×
Hostname: page-component-78c5997874-g7gxr Total loading time: 0 Render date: 2024-11-18T05:46:52.515Z Has data issue: false hasContentIssue false

9 - Performance Assessment of Electrified Aircraft

Published online by Cambridge University Press:  11 May 2022

Kiruba Haran
Affiliation:
University of Illinois, Urbana-Champaign
Nateri Madavan
Affiliation:
NASA Aeronautics Mission Directorate, NASA
Tim C. O'Connell
Affiliation:
P.C. Krause & Associates
Get access

Summary

Most electrified aircraft propulsion (EAP) studies define a concept architecture and compute its potential benefits and key dependencies while attempting to answer the question: Can this architecture “buy its way” onto an aircraft? An important follow-on question is when will the architecture become physically and economically viable? Answering these two questions is the goal of the performance assessment process, a systematic method of analyzing the trade-offs when choosing an EAP system over a traditional one. Its methodologies and assumptions must be reasonable, and detailed comparisons to an appropriate baseline architecture must be included. This chapter outlines a systematic performance assessment process for EAP concept architectures, providing a means of deriving system-level figures of merit. Key steps in the process are identified and details are given for how they might reasonably be performed. Concepts and conclusions from earlier chapters are incorporated as needed. This serves as a guide to aircraft designers – new and old – who are beginning to delve into this exciting field and starting to explore the large design space enabled by EAP configurations.

Type
Chapter
Information
Electrified Aircraft Propulsion
Powering the Future of Air Transportation
, pp. 256 - 293
Publisher: Cambridge University Press
Print publication year: 2022

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

Federal Aviation Administration, “Extended Operations (ETOPS and Polar Operations),” Washington DC, 2008, FAA AC 120-42B.Google Scholar
National Academies of Sciences, Engineering, and Medicine, Commercial Aircraft Propulsion and Energy Systems Research: Reducing Global Carbon Emissions, Washington, DC: National Academies Press, 2016.Google Scholar
Code of Federal Regulations, “Title 14 – Aeronautics and Space, Chapter 1 – Federal Aviation Administration Department of Transportation, Subchapter C – Aircraft, Part 25 – Airworthiness Standards: Transport Category Airplanes.”Google Scholar
International Civil Aviation Organization, “ICAO Aircraft Engine Emissions Databank,” 2019. [Online]. Available: www.easa.europa.eu/easa-and-you/environment/icao-aircraft-engine-emissions-databankGoogle Scholar
Mankins, J. C., “Technology readiness and risk assessments: A new approach,” Acta Astronaut., vol. 65, pp. 12081215, November 2009.CrossRefGoogle Scholar
Lents, C. E., Hardin, L. W., Rheaume, J., and Kohlman, L., “Parallel hybrid gas-electric geared turbofan engine conceptual design and benefits analysis,” presented at the 52nd AIAA/SAE/ASEE Joint Propulsion Conference, Salt Lake City, UT, July 2016, Paper AIAA 2016-4610.Google Scholar
Hall, D. et al., “Boundary layer ingestion propulsion benefit for transport aircraft,” J. Prop. Power, vol. 33, No. 5, pp. 11181129, September 2017.CrossRefGoogle Scholar
de Vries, R., Hoogreef, M., and Vos, R.., “Preliminary sizing of a hybrid-electric passenger aircraft featuring over-the-wing distributed-propulsion,” presented at the 57th AIAA Aerospace Sciences Meeting, San Diego, CA, January 2019, Paper AIAA 2019-1811.Google Scholar
Bradley, M. et al., “Subsonic ultra green aircraft research: Phase II – Volume II – Hybrid electric design exploration,” NASA, Cleveland, OH, Tech. Rep. NASA/CR–2015-218704/Volume II, 2015.Google Scholar
Perullo, C. et al., “Cycle selection and sizing of a single-aisle transport with the electrically variable engine (EVE) for fleet level fuel optimization,” presented at the 55th AIAA Aerospace Sciences Meeting, Grapevine, TX, January 2017, Paper AIAA 2017-1923.CrossRefGoogle Scholar
Felder, J. L., Brown, G. V., Hyun, D., and Chu, J., “Turboelectric distributed propulsion in a hybrid wing body aircraft,” presented at the 20th International Society for Airbreathing Engines Meeting, Gothenburg, Sweden, September 2011, Paper ISABE-2011-1340.Google Scholar
Welstead, J. R. and Felder, J. L., “Conceptual design of a single-aisle turboelectric commercial transport with fuselage boundary layer ingestion,” presented at the 54th AIAA Aerospace Sciences Meeting, San Diego, CA, January 2016, Paper AIAA 2016-1027.Google Scholar
Borer, N. K. et al., “Design and performance of the NASA SCEPTOR distributed electric propulsion flight demonstrator,” presented at the 16th AIAA Aviation Technology, Integration, and Operations Conference, Washington, DC, June 2016, Paper AIAA 2016-3920.CrossRefGoogle Scholar
Kratz, J. L., Culley, D. E., and Thomas, G. L., “A control strategy for turbine electrified energy management,” presented at the 2nd AIAA/IEEE Electric Aircraft Technologies Symposium, Indianapolis, IN, August 2019, Paper AIAA 2019-4499.Google Scholar
Trawick, D., Milios, K., Gladin, J. C., and Mavris, D. N., “A method for determining optimal power management schedules for hybrid electric airplanes,” presented at the 2nd AIAA/IEEE Electric Aircraft Technologies Symposium, Indianapolis, IN, August 2019, Paper AIAA 2019-4500.Google Scholar
Gladin, J. C., Perullo, C., Tai, J. C., and Mavris, D. N., “A parametric study of hybrid electric gas turbine propulsion as a function of aircraft size class and technology level,” presented at the 55th AIAA Aerospace Sciences Meeting, Grapevine, TX, January 2017, Paper AIAA 2017-0338.CrossRefGoogle Scholar
RITA/BTS, Office of Airline Information, “Air Carrier Statistics Database (T-100),” [Online]. Available: www.transtats.bts.gov.Google Scholar

Save book to Kindle

To save this book to your Kindle, first ensure coreplatform@cambridge.org is added to your Approved Personal Document E-mail List under your Personal Document Settings on the Manage Your Content and Devices page of your Amazon account. Then enter the ‘name’ part of your Kindle email address below. Find out more about saving to your Kindle.

Note you can select to save to either the @free.kindle.com or @kindle.com variations. ‘@free.kindle.com’ emails are free but can only be saved to your device when it is connected to wi-fi. ‘@kindle.com’ emails can be delivered even when you are not connected to wi-fi, but note that service fees apply.

Find out more about the Kindle Personal Document Service.

Available formats
×

Save book to Dropbox

To save content items to your account, please confirm that you agree to abide by our usage policies. If this is the first time you use this feature, you will be asked to authorise Cambridge Core to connect with your account. Find out more about saving content to Dropbox.

Available formats
×

Save book to Google Drive

To save content items to your account, please confirm that you agree to abide by our usage policies. If this is the first time you use this feature, you will be asked to authorise Cambridge Core to connect with your account. Find out more about saving content to Google Drive.

Available formats
×