http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-114865965-A

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filingDate 2022-05-19^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_35ea8c0a3887d5bf8cb9d9d9324ff7a7
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publicationDate 2022-08-05^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber CN-114865965-A
titleOfInvention A three-stage generator power system and design method for aviation low-voltage DC
abstract A three-stage generator power system and design method for aviation low-voltage DC, the system includes a three-stage starter generator and a starter generator controller, and the three-stage starter generator includes a permanent magnet auxiliary exciter, a main exciter, a rotating Rectifier tube, main motor, resolver, starter generator controller include MOS tube three-phase full bridge, AC excitation power supply, voltage regulator, auxiliary power supply, control circuit, current sensor S F and S dc . When starting, make the starting process work in the maximum torque-current ratio mode, and drive the three-stage starter-generator from standstill to the ignition speed of the engine. When generating electricity, the output excitation current of the voltage regulator is used to adjust the output three-phase AC voltage value of the main motor to realize the voltage regulation control of the DC voltage V dc ; on the one hand, the three-phase AC voltage v of the main motor is realized through the three-phase full bridge of the MOS transistor. The synchronous rectification of M to the DC voltage V dc , on the other hand, realizes the boost control when the voltage V dc is too low.
priorityDate 2022-05-19^^<http://www.w3.org/2001/XMLSchema#date>
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isDiscussedBy http://rdf.ncbi.nlm.nih.gov/pubchem/compound/CID20111961
http://rdf.ncbi.nlm.nih.gov/pubchem/substance/SID419501450

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