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A Hybrid Economy Bleed, Electric Drive Adaptive Power and Thermal Management System for More Electric Aircraft
Journal Article
2010-01-1786
ISSN: 1946-3855, e-ISSN: 1946-3901
Sector:
Topic:
Event:
Power Systems Conference
Citation:
O'Connell, T., Lui, C., Walia, P., and Tschantz, J., "A Hybrid Economy Bleed, Electric Drive Adaptive Power and Thermal Management System for More Electric Aircraft," SAE Int. J. Aerosp. 3(1):168-172, 2010, https://doi.org/10.4271/2010-01-1786.
Language:
English
Abstract:
Minimizing energy use on more electric aircraft (MEA) requires
examining in detail the important decision of whether and when to
use engine bleed air, ram air, electric, hydraulic, or other
sources of power. Further, due to the large variance in mission
segments, it is unlikely that a single energy source is the most
efficient over an entire mission. Thus, hybrid combinations of
sources must be considered.
An important system in an advanced MEA is the adaptive power and
thermal management system (APTMS), which is designed to provide
main engine start, auxiliary and emergency power, and vehicle
thermal management including environmental cooling. Additionally,
peak and regenerative power management capabilities can be achieved
with appropriate control. The APTMS is intended to be adaptive,
adjusting its operation in order to serve its function in the most
efficient and least costly way to the aircraft as a whole.
This paper presents a hybrid APTMS, which balances the use of
economy bleed air and electric drive in a single architecture that
automatically adapts to changing aircraft conditions to optimally
regulate its function. Bleed air is used when it is relatively
"cheap" (i.e., requires the lowest fuel consumption
compared to other available power sources), but is reduced and
supplemented with electric power from the main engine generator
when bleed air becomes more expensive and electric power becomes
cheaper. Through proper control, this strategy can find the most
efficient balance of bleed air and electric power, increasing
aircraft range and capability. This architecture, abbreviated
"e₂", is presented, describing its components,
functionality, and features. Comparisons to more traditional
systems highlight the potential for energy savings afforded by the
e₂ system. The analysis shows that the e₂ architecture has the
potential to significantly reduce energy use compared to previous
systems, without upsizing the primary generating system (PGS).
Additional anticipated benefits include the ability to provide both
cooling and supplemental power growth without upsizing the
turbomachinery.
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