Design of portable performance parameter test system for aviation DC generator

Author

Zhang, Shutuan ; Lu, Fang ; Jiang, Zhongshan ; Zhang, Kai

Author_Institution

Naval Aeronaut. & Astronaut. Univ., Yantai, China

fYear

2009

Abstract

Aimed at the requirement of fast test for aviation DC generator, a portable performance parameters test system is introduced in this paper. According to the requirement of GJB181 and GJB181A, the hardware structure and software of test system are analyzed, and the design and implementation of the test system software with LabVIEW is completed. The system has the functions including auto setup load, steady state and transient parameters test with different loads, rotor speed test, and so on. The result shows that the system has good and reliable performance of parameter test and achieves the design requirement.

Keywords

DC generators; aircraft power systems; automatic test software; computerised instrumentation; data acquisition; electric machine analysis computing; machine testing; GJB181; GJB181A; LabVIEW; auto setup load; aviation DC generator; hardware structure; portable performance parameter test system; rotor speed test; software structure; steady state parameter; test system software; transient parameters test; Control systems; DC generators; Data acquisition; Electronic equipment testing; Feedback; Hardware; Software systems; Software testing; System testing; Voltage; Aviation DC generator; LabVIEW; auto setup load; test;

fLanguage

English

Publisher

ieee

Conference_Titel

Electronic Measurement & Instruments, 2009. ICEMI '09. 9th International Conference on

Conference_Location

Beijing

Print_ISBN

978-1-4244-3863-1

Electronic_ISBN

978-1-4244-3864-8

Type

conf

DOI

10.1109/ICEMI.2009.5274872

Filename

5274872