25TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES COMPARISON OF POWER QUALITY SOLUTIONS USING ACTIVE AND PASSIVE RECTIFICATION FOR MORE ELECTRIC AIRCRAFT Bulent Sarlioglu, Ph.D. Honeywell Aerospace, Electric Power Systems Torrance, California USA
[email protected] Abstract The introduction of variable frequency distribution system on commercial aircraft This paper presents various three phase active results in the elimination of a mechanical and passive rectification schemes and compares interface device for variable ratio transmission them for more electric aircraft applications. that is positioned between the main engine and The passive topologies involve multi-pulse the ac electric generator. The ac electric transformer rectification systems while the generator can now be directly coupled to the active topologies look into active rectification. main engine output shaft via a gearbox. The Passive rectification systems are to be used for effect of such direct coupling is an ac bus the ac-to-dc conversion that comprises the first frequency proportional to the engine speed stage of the ac-to-ac conversion for applications (which can vary over a 2:1 range depending on such as motor drives in aircraft systems. application), while the magnitude of the ac bus Particular emphases are given to comparison of voltage is regulated to a constant value via a dc bus regulation, electromagnetic interface generator control unit (GCU) for the generation (EMI) filtering, current harmonic cancellation, system. power factor, size, weight, cost and reliability With such a distribution system, it is still among the schemes. Results are summarized possible to connect induction motors directly to qualitatively in a table.