TY - JOUR
T1 - Effect of Endogenous Failure Events on the Survivability of Turboelectric Distributed Propulsion System
AU - Guddanti, Balaji
AU - Choi, Jongchan
AU - Illindala, Mahesh S.
AU - Roychowdhury, Rajarshi
N1 - Publisher Copyright:
© 1972-2012 IEEE.
PY - 2022
Y1 - 2022
N2 - Recent advancements in aircraft electrification have led to the introduction of turboelectric distributed propulsion (TeDP). For instance, NASA's N3X airplane aims to curb jet fuel emissions with the aid of TeDP. However, it is crucial to analyze the survivability of the TeDP system during extreme conditions. The endogenous failure events are of specific interest as they were found to cause a significant number of accidents for commercial aircraft. While the distribution reconfiguration is necessary to meet the critical load demands under extreme failure events, it can also create a transient overload condition in the turboshaft engine. The power system survivability is further deteriorated in the presence of constant power loads. In this article, a mathematical analysis of the survivability of the system is presented to make the aircraft power system highly resilient to endogenous failure events. A power system collapse mitigation strategy is proposed by adding an energy storage system. Moreover, the analytical expressions are formulated to size the energy storage unit to prevent the system collapse. Various failure conditions are modeled using PSCAD/EMTDC to study the minimum energy storage required to prevent system collapse.
AB - Recent advancements in aircraft electrification have led to the introduction of turboelectric distributed propulsion (TeDP). For instance, NASA's N3X airplane aims to curb jet fuel emissions with the aid of TeDP. However, it is crucial to analyze the survivability of the TeDP system during extreme conditions. The endogenous failure events are of specific interest as they were found to cause a significant number of accidents for commercial aircraft. While the distribution reconfiguration is necessary to meet the critical load demands under extreme failure events, it can also create a transient overload condition in the turboshaft engine. The power system survivability is further deteriorated in the presence of constant power loads. In this article, a mathematical analysis of the survivability of the system is presented to make the aircraft power system highly resilient to endogenous failure events. A power system collapse mitigation strategy is proposed by adding an energy storage system. Moreover, the analytical expressions are formulated to size the energy storage unit to prevent the system collapse. Various failure conditions are modeled using PSCAD/EMTDC to study the minimum energy storage required to prevent system collapse.
KW - Constant power loads (CPLs)
KW - PSCAD/EMTDC
KW - distributed energy resources
KW - distribution system
KW - energy storage system (ESS)
KW - fuel map
KW - microgrid
KW - more electric aircraft (MEA)
KW - prime mover
KW - stability
KW - synchronous generator
KW - voltage collapse
UR - http://www.scopus.com/inward/record.url?scp=85118639107&partnerID=8YFLogxK
U2 - 10.1109/TIA.2021.3124739
DO - 10.1109/TIA.2021.3124739
M3 - Article
AN - SCOPUS:85118639107
SN - 0093-9994
VL - 58
SP - 224
EP - 232
JO - IEEE Transactions on Industry Applications
JF - IEEE Transactions on Industry Applications
IS - 1
ER -