NAVY MS90313 REV E-1978 GENERATOR SYSTEM 20 KVA 400 HERTZ ALTERNATING CURRENT INTEGRALLY EXCITED BRUSHLESS TYPE AIRCRAFT BLAST COOLED《20千伏400安赫兹风冷却型整体激振式飞机无刷交流发电机系统》.pdf

《NAVY MS90313 REV E-1978 GENERATOR SYSTEM 20 KVA 400 HERTZ ALTERNATING CURRENT INTEGRALLY EXCITED BRUSHLESS TYPE AIRCRAFT BLAST COOLED《20千伏400安赫兹风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 MS90313 REV E-1978 GENERATOR SYSTEM 20 KVA 400 HERTZ ALTERNATING CURRENT INTEGRALLY EXCITED BRUSHLESS TYPE AIRCRAFT BLAST COOLED《20千伏400安赫兹风冷却型整体激振式飞机无刷交流发电机系统》.pdf（7页珍藏版）》请在麦多课文档分享上搜索。

1、-MS903L3 REV E 61 9999932 0002796 PI FEO. SUC CLASS 6115 6- 224 UNF-JA X -875 LONG STEEL STUDS, Re34 MIN. HARDNESS,AND 6-MS90415-5 NUfS. SPLINE PER MS14169 FORJ 314 INCH SIZE. PLASTIC SPLINE ADAPTER SHALL BE FURNISHED WITH GENERATOR. MS90313-2, GENERATOR, MAX. WT.-SB LBS ENTIRE STANDARD REVISED - MI

2、LITARY STANDARD NAVIAS. TRLC kcr, GENERATOR SYSTEM EOKVA 400 HERTZ, ALTFDNATIUC P#lDDcuI( *u-e-A* I s Y CY-*- -. 1 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-flS703L3 REV E b1 W 7777712 0002 T m- I f ED. HIC CLASS 10-32 POSTS, 3 REO. (TERMINAL C

3、OVER REOUIREDI.3 MS3376-3 NUTS SHALL BE FURNISHED -RU WITH RECTIFIER - O h- 4 I MOUNTING BAND SHALL - BE SUITABLE FOR MOUNTING THE RECTIFIER ON THE 6.500 DIAMETER OF MS90313-2 GENERATOR. PLUG MS3126E- 10-6s MS90313- 3, RECTIFIER ASSEMBLY, MAX. WT. - 1.3 LBS .?BE MAX. -H b- -+ k.249 MAX. RECEPTACLE T

4、O MATE WITH MS31 I6P-16-265 RECEPTACLE TO MATE WITH MSJII6P-I6-BS L J6 DIA. 4 HOLES .3B MAX. A40 RD. MIN. CLEARANCE AROUND EACH HOLE L.200 MAX. 4 MOUNTING TABS MS90313-4, GENERATOR CONTROL UNIT, MAX. WT.-3 L8S O C I E 1 MILITARY STANDARD- MS90313 (AS) TITLE t4lacri GENERATOR SYSTEM, 20 KVA, 400 HERZ

5、, . ALTERNATING CURRENT, INTEGRALLY EXCITED, .- BRUSHLESS TYPE, AIRCRAFT, BLAST COOLED i Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,- L MS90333 REV E 61 9979932 0002798 3 W *li MAVI -AS *cum KICLIREUENT SPECIFUIKIW MIL- G - 2 14 8 O I FEO. W? ELM

6、S TITLC GENERATOR SYSTEM,2O KVA, 400 HERTZ, ALTERNATING CURRENT, INTEGRALLY EXCITED, BRUSHLESS TYPE, AIRCRAFT, BLAST COOLED -%!E F%?%LED EQUIUEN. CONTROL COM- PONENTS SHAU lEET THE TEMPERATURE-ALTITUDE REQUIREMENTS OF MIL-E-81910 FOR SELF-COOLED EQUIPMENT. NAVY A.S. mu RGi M Il IT AIY ST Al DA I I G

7、ENERATOR SYSTEM, M KVA, 400 HERTZ. , i Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-.MS03L3 REV E bL M 979L2 0002800 b M I 6115 3.4.0 QUNCE “FIGURE 3“ To “FICURE 1“ OF IS SPECIFICATION. 3.4.0.2 CHANCE “5 MNmS“ fo “2 III#vTES“. 3.4.9.3 ADD: THE CEN

8、ERATOR SYSTEM SHALL BE DESIGNED SO lWAT UPON RMOVAL OF ANY CON- HECTOR PLUG THE CWERATOR AND GCU SHALL BE DE-ENERGIZED. 3.4.9.6.1.1 CHANCE :10,000 HOUR LIFICC AND THE EFFECT OF APPLICATION AND REMOVAL OF RATED AND 2007. LOAD. THE COHPLETION OF THIS TEST THE UNIT SHALL 4.5.23.1.1 DELETE AND ADD: GENE

9、RATOR. THE GENERATOR AND RECTIFIER ASSEMBLY SHALL BE SUBJECTED TO A VIBRATION TEST IN ACCOmT3 MIL-E-81910, EXCEPT THAT THE AMPLITUDE OF VIBRA- TlOZ MONITORED AT THE ANTI-DRIVE END OF THE GENERATOR DURING THE MAIN BENDING MODE SHALL BE I.TMTTED Tn 25 Cs BUT THE VXBRATIOI INPUT SHALL NOT BE LWERED BEL

10、OW 5 GIs. AT THE COWLETION ID THE APPLICA- TION AND REHOVAL OF RAED AND 200% WAU. LIMITED TO GIs, VIBRATIOI Gs. OF THIS TEST, THE UNIT SHALL SUCCESSFULLY DEHONSTRATE ITS BUILDUP CHARACTERISTICS AND RATED MAD. 4.5.23.1.2 DELETE AND ADD: CONTROL COMPONENTS. CONTROL COKPONENTS SHALL BE SUBJECTED TO A V

11、IBRATION TEST IN ACCORDANCE WITH M - - 5 TO 500 Hi AT THE COMPLETION OF THik hi:% =HALL SUCCESSFULLY D!CIONSTRATE ITS BUILDUP CHARACTERISTICS, THE EFFECT OF APPLICATION AND REHOVAL OF RATED AND 2002 LOAD, AND PROTECTIVE FUNCTIONS. THAT THE VIBRATION RANGE SHALL BE FROM 4.5.24 DELETE AND ADD: SHOCK.

12、SYSTEM COMPONENTS SHALL BE SUBJECTED TO A SHOCK TEST IN ACCORDANCE WITH MIL-E-81910. DEMONSTRATE ITS BUILDUP CHARACT?2RISTICS AT !PL!XION OF PROCEDURE 1. THE UNIT SHALL SUCCESSFULLY THE EFFECT OF APPLICATION AND RMOVAL OF RATED AND 200% LOAD AND PROTECTIVE FUNCTIONS. THERE SHALL BE NO FAILURE OF THE

13、 MOLWTING AITACIDENTS AND THE TEST IGS-GLL-EN-IN PUCE AND NOT CREATE A HAZARD DURING PROCEDURE III. L.5.25 DELETE AND ADD: HUMIDITY. SYSTEM COMPONENTS, EXCEPT THOSE TESTED UNDER PAM- GRAPH 4.5.20.2, SHALL BE SUBJECTED TomIn TEST IR ACCORDANCE WITH FIL-E-81910. COMPLETION OF THIS TEST THE UNIT SHALL

14、SUCCESSFULLY DEONSTRATE ITS BUILDUP CHARACTERISTICS, THE EFFECT OF APPLICATION AND REHOVAL OF RATED AND 200% LOAD, AND PROTECTIVE FUNCTIONS. AT THE 4.5.30 DELETE FIRST SENTENCE AND ADD: ALL SYSTEM COHPONEWS EXCEPT THE GENERATOR SHALL BE SUBJECTED TO THE ACCELERATION TESTS OF MIL-E-81910. UNIT SHALL

15、SUCCESSFULLY DEMONSTRATE ITS BUILDUP CHARACTERISTICS. REHOVAL OF RATED AND 200% LOAD, AND PROTECTIVE FUNCTIONS. AT THE COMPLETION OF RIE TESTS THE THE EFFECT OF APPLICATION AND NOTES : 1. PINS B AND C FOR CONSTANT SPEED DRIVE INTERLOCK. THE SYSTEM. PINS D AND E FOR GROUND POWER INTERLOCK. OPENING TH

16、IS CIRCUIT SHALL DEENERGIZE 2. OPENING THIS CIRCUIT SHALL =ENERGIZE THE SYSTM. 3. GENERATOR CONTROL SWITCH AND LINE CONTACTOR SHWN FOR INTERC6“ECTIONS ONLY AND ARE NOT FURNISHED UNDER THIS DRAWING. 4. DMNSIONS IN INCHES. UHLESS OTHERUISE SPECIFIED, TOLERANCES: LINFAR +- .030; ANGULAR 5 1. 5. ALL OUT

17、LINE DIMENSIONS ARE LImTING DIZIENSIONS ONLY. 1 ITEM PART “BER COMPLETE SYSTEM (CONSISTS OF ONE GENERATOR ONE RECTIFIER, ONE BASE AND ONE GCU) HS90313-1 GENERATOR M90313-2 RECTIFIER ASSMBLY HS90313-3 rsm HS90313-4 r - I BASE nC90313-5 I FOR DESIGN FUTURE PURPOSES MREIN. lHIC STANDARD TAKES PRECEDENC

18、E OVER PROCUREMENT DOCUMENTS REnRENCED REFERENCED DOCWNk SHALL BE OF THE ISSUE IN EFFECT ON DATE OF INVITATION FOR BIDS. A MAW-AS TITLE MILITARY STANDAI hhb GENERATOR SYSTEM, 20 KVA, 400 HERTZ, ALTERNATING CURRENT. INTEGRALLY EXCITED, BRUSHLESS TYPE, AIRCRAFT, BLAST COOLED MS90313 (AS) 7 0 6 -EWW YC

19、CWUIIQ( oIEIy#S WET MIL-G-21480 .utr DO tZn672-1 (wrr. ddurlr) -mrmmu-rr Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-i I o o 8 VIME I# SECWDS FIGURE 1. SYSTEM VOLTAGE LIMITS. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-