NAVY MS90304 REV E-1979 GENERATOR SYSTEM 20 KVA 400 HERTZ ALTERNATING CURRENT INTEGRALLY EXCITED BRUSHLESS AIRCRAFT SELF-COOLED《20千伏400安赫兹自冷却型整体激振式飞机无刷交流发电机系统》.pdf

《NAVY MS90304 REV E-1979 GENERATOR SYSTEM 20 KVA 400 HERTZ ALTERNATING CURRENT INTEGRALLY EXCITED BRUSHLESS AIRCRAFT SELF-COOLED《20千伏400安赫兹自冷却型整体激振式飞机无刷交流发电机系统》.pdf》由会员分享，可在线阅读，更多相关《NAVY MS90304 REV E-1979 GENERATOR SYSTEM 20 KVA 400 HERTZ ALTERNATING CURRENT INTEGRALLY EXCITED BRUSHLESS AIRCRAFT SELF-COOLED《20千伏400安赫兹自冷却型整体激振式飞机无刷交流发电机系统》.pdf（9页珍藏版）》请在麦多课文档分享上搜索。

1、MS0304 REV E bL m 7997732 0002787 7 I YI fro. SUI CLASS 61 I5 ENTIRE STANDARD REVISED LOAD TERMINALS IN AREA“A“ SIX 5/16-24 UNF-3A STUDS. -_, EACH TO cCOMMATE ONE MS90415-5 NUT. -YwTYKtC CENERAT R. THE CENERATOR AND RECTIFIER ASSEMBLY SHALL BE SUBJECTED TO A VIBRATION TEST IN ACCOdTH MIL-E-81910 FOR

2、 ENGINE-MOUNTED COMPONENTS. AT THE COMPLETION OF THIS TEST THE UNIT SHALL SUCCESSFLZLY DEMONSTRATE ITS BLILDUP CHARACTERISTICS AND THE EFFECT OF APPLICATION AND REMOVAL OF RATED AND 200% LOAD. 4.5.23.1.2 DELETE AND ADD: TROL COMPONE NTS. CONTROL CWONENTS SHALL BE SUBJECTED TO A VIBRATION TEST IN ACC

3、ORDANCE WIT!%IL-E-81910 EXCEPT THAT THE VIBRATION RANGE SHALL BE FROM 5 TO 500 HZ. BUILDUP CHARACTERISTICS, THE EFFECT OF APPLICATION AND REMOVAL OF RATED AND 2008 LOAD. AND PROTECTIVE FUNCTIONS. AT THE COMPLETION OF THIS TEST hE UNIT SHALL SUCCESSFULLY DEMONSTRATE ITS 4.5 24 DELETE AND ADD: u. SYST

4、EM COKPONENTS SHALL BE SUBJECTED T A SHOCK FULLY DEMONSTRATE ITS BUILDUP CHARACTERISTICS, THE EFFECT OF APPLICATIOX AND REIIOVAL OF RATED AND ZOOS LOAD, AND PROTECTIVE. FWCTIONS. THE TEST ITEM SHALL REMAIN IN PLACE AND NOT CREATE A WARD DURING PROCEDURE III. TEST IN CCORDANCE WITH mL-p-81910. AT THE

5、 COMPLETION OF PROCEDVRE I, THE UBTT SHALL SUCCESS- THERE SHALL BE NO FAILURE OF THE MOLTFTING ATTACtMEhTS, AND 4.5.25 DELETE AND ADD: -. SYSTEM COFPONENTS. EXCEPT THOSE TESTED UNDER PARAGRAPH 4.5.20.2 THE COMPLETION OF hIS TEST THE LWIT SHALL SUCCESSFULLY DEMONSTRATE ITS BUILDUP CHARACTERISTICS. TH

6、E EFFECT OF APPLICATION AND REMOVAL OF RATED AND 2007. LOAD, AND PROTECTIVE FUNCTIONS. SHALL BE SUBJECTED TO A HUMIDITY TEST IN ACCORDANCE WITH MIL-E-81910. AT 4 5.30 DELETE FIRST SENTENCE AND ADD: ALL SYSTEM CWONENTS EXCEPT THE CSNERATOR SHALL BE SUBJECTED TO THE ACCELERATION TESTS OF MIL-E-81910.

7、THE WUT SHALL SUCCESSFULLY DEMONSTRATE ITS BUILDLT CHARACTERISTICS, ME EFFECT OF APPLICATION AND REMOVAL OF RATED AND 2002 LOAD, AND PROTECTIVE FUNCTIONS. AT THE COMPLETION OF THE TESTS NOTES : 1. 2. DI!ENSIONS IN INCHES. UNLESS OTHERWISE SPECIFIED, TOLERANCES: LINEAR 0.030. ANGULAR i 1. CENERATOR C

8、ONTROL SUITCHES WARNING LIGHTS, AND LINE CONTACTORS ARE SHOWN FOR IhTER- CONNECTIONS ONLY AND ARE NT FURNISHED UNDER THIS DRAWING. O WIVY-AS TITLE MIL IT ARY STANDARD- GENERATOR SsTM 20 KVA 400 HERTZ ALTERNATING cudm, IGRALLY EXCTED. kui, BRUSHLESS, AIRCRAFT, SELF-COOLED. *. . - IC I Provided by IHS

9、Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-MS0309 REV E b1 W 7977912 0002775 b FIELD-INSTALLED SYSTEM (CONSISTS OF ONE GENERATOR, ONE RECTIFIEF, ONE CONTROL UNIT, ONE BASE, AND ONE JUMPER BOX) IDENTIFICATION OF ITEHS 1590304-10 I ITEM FACTORY-INSTALLED SYSTEH

10、(CONSISTS OF ONE GENE!L4TOR, ONE COi!TXOL UNIT. WREE LOAD END CURRENT TRANSFORMERS, AND ONE GROUND END CURRENT TRANSFORMER) HILITARY PART NLBER W.90304-20 GENERATOR RECTIFIER CONTROL UNIT BASE JWER BOX LOAD END CURRENT TRANSFORMER GROUND END CURRENT TRANSFORMER FS90300-3 t”C90313-3 W90313-4 PS90304-9 FS90304-11 M21480/12-5 P21480/12-6 a9 3 I c In c w LL! I ln W W ln In W c3 z 4 I U O IL a - a E o W a * (D o! =! a n m 4 (u L Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-