This report documents the results of Phase I, Study, of this five phase program. The objectives of this program are to develop an FTEPS design for an ATF aircraft and to design and fabricate a low cost FTEPS demonstrator with an integrated load simulator. The primary purpose of the program is to develop an electrical power generation and distribution system that can supply electrical power to the various critical systems on the aircraft with a reliability and power quality level commensurate with the requirements of the loads. In Phase I, the electrical loads and their power requirements were defined for the ATF baseline aircraft model. The loads were also located in the baseline aircraft model.
Fault Tolerant Electrical Power System. Phase I. Study
1986
52 pages
Report
Keine Angabe
Englisch
Aircraft , Aircraft equipment , Electrical equipment , Electric power distribution , Base lines , Distribution , Electric power , Electric power production , Electrical loads , Integrated systems , Low costs , Power , Power levels , Quality , Reliability , Requirements , Simulators , Military aircraft , Aircraft Electrical Systems , Fault tolerance , ATF Aircraft
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