Inverter prototype development for HLFC compressor applications

نویسندگان

چکیده

Abstract A key component in Hybrid Laminar Flow Control (HLFC) is a turbo-compressor, which requires an inverter. However, harsh environment combination with restrictive boundary conditions make the inverter design very challenging. Moreover, aviation certification standards have to be considered. By reason of its growing significance, Model-Based Systems Engineering (MBSE) approach described break HLFC system requirements down lower level Using acquired set requirements, prototype was initiated. For this, compressor motor, Permanent Magnet Synchronous Motor (PMSM) running up 150,000 $$\text {min}^{\text {-1}}$$ min -1 at power more than 5 kW, characterized by measurements. Thereafter, control concept elaborated and implemented on preliminary electronics. In end, feasibility tests were conducted testbed, whose results match well theory.

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ژورنال

عنوان ژورنال: CEAS Aeronautical Journal

سال: 2022

ISSN: ['1869-5582', '1869-5590']

DOI: https://doi.org/10.1007/s13272-022-00611-4