LEADER 01208nam--2200397---450- 001 990001437270203316 005 20040219103749.0 035 $a000143727 035 $aUSA01000143727 035 $a(ALEPH)000143727USA01 035 $a000143727 100 $a20040219d1972----km-y0itay0103----ba 101 0 $aita 102 $aIT 105 $a||||||||001yy 200 1 $a<> percezione$eun'introduzione alla psicologia della visione$fM. Cesa Bianchi, A. Beretta, R. Luccio$gprefazione di Cesare L. Musatti 210 $aMilano$cAngeli$d1972 215 $a327 p.$d22 cm 225 2 $aCollana di psicologia$v1 410 0$12001$aCollana di psicologia$v1 454 1$12001 461 1$1001-------$12001 606 0 $aPercezione 700 1$aCESA BIANCHI,$bMarcello$0451403 701 1$aBERETTA,$bAngelo$049329 701 1$aLUCCIO,$bRiccardo$0142520 702 1$aMUSATTI,$bCesare Luigi 801 0$aIT$bsalbc$gISBD 912 $a990001437270203316 951 $aVI ps C coll 4/1$b58647 L.M.$cVI ps C coll 959 $aBK 969 $aUMA 979 $aSIAV5$b10$c20040219$lUSA01$h1037 979 $aPATRY$b90$c20040406$lUSA01$h1741 996 $aPercezione$9935982 997 $aUNISA LEADER 02230nam 2200373 450 001 9910136506403321 005 20231206165422.0 010 $a1-5044-0447-5 024 7 $a10.1109/IEEESTD.1960.7438698 035 $a(CKB)3710000000619067 035 $a(NjHacI)993710000000619067 035 $a(EXLCZ)993710000000619067 100 $a20231206d1960 uy 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aAIEE No 806-1960 $eAIEE Proposed Test Procedure for Aircraft Alternating Current Generators /$fIEEE 210 1$a[Place of publication not identified] :$cIEEE,$d1960. 215 $a1 online resource 330 $aThe purpose of this procedure to define uniform acceptable test methods for determining the performance and other characteristics of aircraft alternating-current generators. Rotating electric equipment for aircraft is subjected to requirements and operating conditions not normally encountered by commercial generators. For example, conditions of temperature, altitude, humidity, and vibration vary over much wider ranges. Aircraft requirements dictate minimum weight, and yet utmost reliability is essential. Weight reduction is generally achieved by sacrifice of life expectancy commensurate with aircraft practices. The necessity for accurate design requires that direct measurements to insure reliability and adequate life be an important part of this test procedure. It is recognized that there may be acceptable methods of making tests other than those described. Such other methods may be considered as alternative procedures accepted by agreement between interested parties. The tests outlined herein are not necessarily complete for any specific generator; and likewise the requirements in each case will determine the number of tests to be made. 517 $aAIEE No 806-1960 606 $aElectric generators 606 $aElectric motors 615 0$aElectric generators. 615 0$aElectric motors. 676 $a621.313 801 0$bNjHacI 801 1$bNjHacl 906 $aDOCUMENT 912 $a9910136506403321 996 $aAIEE No 806-1960$93646694 997 $aUNINA