Abstract
A centralised smart supervisor (CSS) controller with enhanced electrical energy management (E2-EM) capability has been developed for an Iron Bird Electrical Power Generation and Distribution System (EPGDS) within the Clean Sky 2 ENhanced electrical energy MAnagement (ENIGMA) project. The E2-EM strategy considers the potential for eliminating the 5 min overload capability of the generators to achieve a substantial reduction in the mass of the EPGDS. It ensures optimal power and energy sharing within the EPGDS by interfacing the CSS with the smart grid network (SGN), the energy storage and regeneration system (ESRS), and the programmable load bank 1 secondary distribution board (PLB1 SDU) during power overloads and failure conditions. The CSS has been developed by formalizing E2-EM logic as an algorithm operating in real time and by following safety and reliability rules. The CSS undergoes initial verification using model-in-the-loop (MIL) testing. This paper describes the EPGDS simulated for the MIL testing and details the E2-EM strategy, the algorithms, and logic developed for the ENIGMA CSS design. The CSS was subjected to two test cases using MIL demonstration, and based on the test results, the performance of the ENIGMA CSS is verified and validated.
Highlights
Recent trends in aircraft development and related research and development (R&D) programs show the increasing role and importance of electrically powered onboard equipment that was traditionally powered by hydraulic or pneumatic systems
This paper aims to verify and validate the performance of the ENIGMA centralised smart supervisor (CSS) through MIL demonstration
Through the two test cases presented the MIL demonstration has verified and validated the behaviour and performance of the ENIGMA CSS
Summary
Recent trends in aircraft development and related research and development (R&D) programs show the increasing role and importance of electrically powered onboard equipment that was traditionally powered by hydraulic or pneumatic systems. This has resulted in an increased onboard power generation capacity, exceeding 1 MW in civil aircraft programs in some cases. The trend is clearly a move toward a more-electric aircraft (MEA) or even an eventual all-electric Aircraft.
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