Abstract
The impact of the onboard electrical power system on the operation of the mechanical prime mover, for example an aircraft gas-engine, is examined through experimental testing on a 100kW aircraft power system facility. Hardware-in-the-loop techniques are used to control two motor drives such that they emulate the dynamic characteristics of the shafts in an aircraft engine. Electrical generators are driven by the shafts and loaded with representative, highly dynamic, power system load profiles, including actuators, landing gear and avionics. The effects of electrical transients on the shaft torques are examined to demonstrate how an electrical energy storage system can mitigate load transients on the engine. Also, the use of generator power sharing algorithms is assessed. © 2011 IEEE.
Original language | English |
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Title of host publication | IEEE Energy Conversion Congress and Exposition: Energy Conversion Innovation for a Clean Energy Future, ECCE 2011, Proceedings|IEEE Energy Conver. Congr. Expo.: Energy Conv. Innov. Clean Energy Future, ECCE, Proc. |
Pages | 1476-1482 |
DOIs | |
Publication status | Published - 2011 |
Event | 3rd Annual IEEE Energy Conversion Congress and Exposition, ECCE 2011 - Phoenix, AZ Duration: 1 Jul 2011 → … |
Conference
Conference | 3rd Annual IEEE Energy Conversion Congress and Exposition, ECCE 2011 |
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City | Phoenix, AZ |
Period | 1/07/11 → … |
Keywords
- aerospace control
- aerospace engines
- aircraft power systems
- electric generators
- energy storage
- machine control
- motor drives
- shafts
- actuators
- aircraft gas-engine
- aircraft power system facility
- avionics
- electrical energy storage system
- electrical generators
- electrical transients
- finite inertia mechanical systems
- generator power sharing algorithms
- hardware-in-the-loop techniques
- landing gear
- load transients
- mechanical prime mover
- onboard electrical power system
- power 100 kW
- shaft torques