LEADER 01746nam 2200349 450 001 996280550903316 005 20231208101850.0 010 $a0-7381-4339-1 024 7 $a10.1109/IEEESTD.1976.120244 035 $a(CKB)3780000000092706 035 $a(NjHacI)993780000000092706 035 $a(EXLCZ)993780000000092706 100 $a20231208d1976 uy 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aIEEE Std 128-1976 $eIEEE Guide for Aircraft Electric Systems /$fInstitute of Electrical and Electronics Engineers 210 1$aNew York, New York :$cIEEE,$d1976. 215 $a1 online resource 330 $aThis document provides in compact form recommendations and technical reasons for the selection, design and application of aircraft electric power systems and electrically-actuated load equipment, without going into specific detailed designs. The standard was originally published in 1960 as AIEE 750. Sections of this guide are: introduction; criteria for the electric system; characteristics of alternating-current generators affecting their application; distribution system design; symmetrical components; principal subdivisions of electric system; selection of the system; installation practices; equipment characteristics; and electric system design procedures. 517 $aIEEE Std 128-1976: IEEE Guide for Aircraft Electric Systems 606 $aSwitching power supplies$xStandards 615 0$aSwitching power supplies$xStandards. 676 $a621.381044 801 0$bNjHacI 801 1$bNjHacl 906 $aDOCUMENT 912 $a996280550903316 996 $aIEEE Std 128-1976$92575217 997 $aUNISA