1、KS W 5092KSKSKSKSSKSKSKS KSKSKS SKSKS KSKS SKS KS KS W 5092 : 2003 (2008 ) 2003 6 27 http:/www.kats.go.kr : ( ) ( ) ( ) ( ) : (http:/www.standard.go.kr) ： : 2003 6 27 : 2008 6 27 2008-0304 : ( 02-509-7294) . (http:/www.kats.go.kr) 10 5 , . ICS 49.060 KS W 5092： 2003(2008 ) AC generators and associat
2、ed regulators for aircraft 1. 1.1 ( .) . ( ) . 1.2 120/208 V( 110/220 V), 400 Hz, 3 , Y . (brush) (brushless) . 2. . . RTCA/DO 160D Environmental conditions and test procedures for airborne equipment MIL STD 461 Requirements for the control of electromagnetic interference characteristics of subsyste
3、ms and equipment MIL STD 810 Environmental engineering considerations and laboratory tests 3. . 3.1 / (exciter/regulator) 3.2 (phase balance) 3 . 100333.3 3.4 (full rating) (per phase current) . ) (30001kVA 4. 4.1 . . 4.1.1 a) b) (kVA) c) ( ) W 5092： 2003 2 d) e) (400 Hz ) f) g) h) (overspeed) i) j)
4、 ( 1 ) k) ( ) l) m) n) o) 4.1.2 a) b) c) d) e) f) ( ) 4.2 . , . 4.3 a) , , , . b) . 4.4 a) . b) . 5. 5.1 6.3.1 . 5.1.1 . 5.1.1.1 a) , . b) ( 5 % ) , . 5.1.1.2 . W 5092： 2003 3 . a) (rated lagging power factor) 150 % 2 b) (rated lagging power factor) 200 % 5 5.1.2 5.1.2.1 ( ) a) 3 % . b) ( 1 ). 5.1.2
5、.2 0 , 0 200 3 % . 5.1.2.3 5.1.1.1 5.1.1.2 1 . 5.1.3 (excitation) (self excited) . 5.1.4 (slip rings) , , (pin point) . . 5.1.5 (unity power factor load) , (terminal) . 5.1.5.1 (phase) 0.5 % , 1200.6 . 5.1.5.2 (phase) 1/6, 1/3, 2/3 ( , ) 1 %, 2 %, 4 % , 1201, 1202, 1204 . 5.1.6 5.1.6.1 3.5 V . / (pe
6、ak to valley) 1 . 5.1.6.2 2 . 5.1.7 (line to neutral) (crest factor) 1.41410 % , 3 % 4 % RMS(Root Mean Square) . a) 100 % 50 % (unity power factor) b) (rated power factor) a) c) 10 % . 5.1.8 (dielectric strength) 60 Hz . / . , , , . a) 50 V 500 V RMS 1 600 V RMS 1 W 5092： 2003 4 b) 50 V 2 1 000 V RM
7、S 1 1 120 % 1 5.1.9 (flexible drive) (damper) . . 20 . , . a) ( ) 1(0.5) 100 . 5(4) . b) 2 40 c.p.s 2(1) 50 . 7(5) . c) 2(1) 15 . 7(5) . d) “ (dead band)” “ (clearance) , 1/2 . 5.1.10 a) ( ) . b) (10 %) . c) . d) . 5.1.11 a) 3 300 % , 5 115 % . b) 1 (line to line) 300 % . c) . d) . e) . 5.1.12 (bear
8、ing failure) 4 . . a) , (cage), (seal) . b) 4 . . 5.1.13 (overspeed) a) 115 % 5 . b) . W 5092： 2003 5 c) . d) 5.1.2 . 5.1.14 (operating position) . 5.2 RTCA/DO 160D / . 5.2.1 (fluid resistance) RTCA/DO 160D 10.0 . RTCA/DO 160D A . 5.2.2 53.9 ( 65F) 8 (warm up) 5.1.2 . 5.2.3 (radio frequency) RTCA/DO
9、 160D 21.0 . . 5.2.4 . RTCA/DO 160D 4.0 . 5.1.2 5.1.5 . 5.2.5 a) 6 360 . 2 5 2 5 1 50 3 5 (120 6 ) b) RTCA/DO 160D 3.5 4.3 , , . c) 120 . d) . . 5.2.6 RTCA/DO 160D 6.3.1 A . . 5.2.7 RTCA/DO 160D 7.0 . a) 1) 5.1.2.1 5.1.5 . 2) . b) , W 5092： 2003 6 . . 5.2.8 a) RTCA/DO 160D 8.0 . 5.1.2.1 . b) 5.1.8 .
10、 c) RTCA/DO 160D 8.0 . (inactive) (brinelling) . 5.2.9 3 0.5 % . 5.2.10 a) MIL STD 461 . b) . c) / . d) MIL STD 461, Class No. B . 5.3 RTCA/DO 160D . 5.3.1 RTCA/DO 160D 10.0 . 5.1.2.1 5.1.5 . 5.3.2 / a) RTCA/DO 160D 12.0 / . b) . c) 2 6 . d) . e) 5.1.2.1 . 5.3.3 a) RTCA/DO 160D 13.0 . b) 28 , 5.1.2.
11、1 5.1.5 . c) . 5.3.4 RTCA/DO 160D 14.0 . 5.1.2.1 5.1.5 . 5.3.5 RTCA/DO 160D 9.0 . . 6. 6.1 , . W 5092： 2003 7 RTCA/DO 160D . 6.1.1 5.1 5.2 , 2 . 5.3 5.1 5.2 . 6.1.2 5.1 5.2 , . 6.2 . . 6.3 6.3.1 6.3.1.1 . 6.3.1.2 3010 . 6.3.1.3 . 6.3.1.4 . 6.3.1.5 . 6.3.1.6 , , . 10 ( ) 555 5 . 6.3.1.7 (instrumen ta
12、tion and test equipment) . W 5092： 2003 8 1 2 A B C 0.8 2 ： (L N) 115 . . ( ) 5 V . /() ( ) ( ) /(Vpv) (CPS) RMS X (Vpv)0 .04 .08 .12 .16 .20 .24 .28.4.5.6.7.8.91.01.11.21.31.361.41.51.571.61.7A B 118.5V L N 111.5V L N 115V L N 120V L N 69V L N 4.0 3.0 2.0 1.0 0.5 0.0 Vp v CPS 0.5 0.5 3.5 3.5 0.5 0.
13、5 0.5 1.01.710.025.070.0100.0200.0W 5092： 2003 9 1 (ft) (kVA) (%) ( ) 120 120 40 140 0 100 80 120 40 40 100 0 0.5 70 40 120 40 40 100 40 70 40 135513 7017 (02)60094867 (02)600948878 http:/ KS W 5092 : 2003 KSKSKS SKSKS KSKS SKS KS SKS KSKS SKSKS KSKSKS AC generators and associated regulators for aircraft ICS 49.060 Korean Agency for Technology and Standards http:/www.kats.go.kr
