Zobrazeno 1 - 10
of 15
pro vyhledávání: '"Michael James Armstrong"'
Publikováno v:
IEEE Transactions on Applied Superconductivity. 26:1-9
Turbine engine driven distributed electrical aircraft power systems (also referred to as Turboelectric Distributed Propulsion (TeDP)) are proposed for providing thrust for future aircraft with superconducting components operating at 77K in order for
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6a37aa1fa410448af68a3bffc37d872b
https://doi.org/10.1109/tasc.2016.2530696
https://doi.org/10.1109/tasc.2016.2530696
Autor:
Dwayne Bevis, David Trawick, Dimitri N. Mavris, Jonathan C. Gladin, Michael James Armstrong, Kyle Klein
Publikováno v:
2018 AIAA/IEEE Electric Aircraft Technologies Symposium.
This paper describes a basic analysis for mission performance of parallel hybrid turbofan systems. A series of equations is derived to illustrate the concept of parallel hybrid performance showing that there is an optimum range for a given battery si
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::60e7d40f6b707381ce2a412c4bfc91e4
https://doi.org/10.2514/6.2018-5024
https://doi.org/10.2514/6.2018-5024
Publikováno v:
2018 IEEE Transportation Electrification Conference and Expo (ITEC).
This work describes the architecture and evaluation of a turbo-electric distributed propulsion microgrid for ECO-150, a NASA funded 154 passenger subsonic fixed wing commercial transport aircraft concept for entry into service by 2035. Three differen
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2dabde24324c7b756da414157e6813f6
https://doi.org/10.1109/itec.2018.8450180
https://doi.org/10.1109/itec.2018.8450180
Autor:
David Trawick, Douglas J. Snyder, Dimitri N. Mavris, Christopher Perullo, Michael James Armstrong, Jimmy C. Tai
Publikováno v:
55th AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::de44f8ce6223f4fc99abc4b8518b6602
https://doi.org/10.2514/6.2017-1922
https://doi.org/10.2514/6.2017-1922
Publikováno v:
55th AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c15e3098bf978b1683e0db5d172e3950
https://doi.org/10.2514/6.2017-1923
https://doi.org/10.2514/6.2017-1923
Publikováno v:
Aircraft Engineering and Aerospace Technology. 86:509-514
Purpose – The purpose of this paper is to highlight and discuss the unique safety and protection requirements for the electrical microgrid system in a turboelectric distributed propulsion aircraft. Design/methodology/approach – The NASA N3-X conc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7b65e4d93488b3f8cde5ac9824dbcb82
https://doi.org/10.1108/aeat-04-2014-0049
https://doi.org/10.1108/aeat-04-2014-0049
Publikováno v:
SAE International Journal of Aerospace. 5:325-336
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::78c6d534344a444faa2bc96286f810b9
https://doi.org/10.4271/2012-01-2163
https://doi.org/10.4271/2012-01-2163
Propulsion System Component Considerations for NASA N3-X Turboelectric Distributed Propulsion System
Publikováno v:
SAE International Journal of Aerospace. 5:344-353
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6074bce55d58b99cbcf661fa954a4061
https://doi.org/10.4271/2012-01-2165
https://doi.org/10.4271/2012-01-2165
Autor:
Graeme Burt, Catherine E. Jones, Andrew Bollman, Michael James Armstrong, Stuart Galloway, Karen Davies, Patrick Norman
Publikováno v:
SAE Aerotech Congress and Exhibition
Distributed electrical propulsion for aircraft, also known as turbo-electric distributed propulsion (TeDP), will require a complex electrical power system which can deliver power to multiple propulsor motors from gas turbine driven generators. To ens
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9478550f0efc44ef1cce44b2608822ae
https://strathprints.strath.ac.uk/55041/1/Jones_etal_SAE2015_protection_system_considerations_DC_distributed_electrical_propulsion_systems.pdf
https://strathprints.strath.ac.uk/55041/1/Jones_etal_SAE2015_protection_system_considerations_DC_distributed_electrical_propulsion_systems.pdf
Autor:
Stuart Galloway, Michael James Armstrong, Catherine E. Jones, Andrew Bollman, Graeme Burt, Patrick Norman
Turbo-electric distributed power (TeDP) systems proposed for hybrid wing body (HWB) N3-X aircraft are complex, superconducting electrical networks, which must be developed to meet challenging weight, efficiency and propulsor power requirements. An in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a647c5610487c228f62c25a5db22dab1
https://strathprints.strath.ac.uk/54931/1/Jones_etal_ESARS2015_sensitivity_analysis_tool_for_consideration_of_full_electric_aircraft.pdf
https://strathprints.strath.ac.uk/54931/1/Jones_etal_ESARS2015_sensitivity_analysis_tool_for_consideration_of_full_electric_aircraft.pdf