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基本信息

【范围】

This SAE Aerospace Recommended Practice (ARP) provides technical and application information needed by the designers of aircraft electric systems and support equipment for the selection of overcurrent protective devices. It provides definitions to permit comparisons of various electric circui protective devices. Included also are recommended procedures for periodic visual and mechanical inspection criteria.strRefField

【与前一版的变化】

替代标准

ARP1199A

引用文件/被引文件

DC 20005

Aircraft Industries of America (AIA) Publications: Available from Aerospace Industries Association

PA 19111-5097

Naval Air System Command Publications: Available from Naval Air Technical Services Facility

NAVAIR 01-1A-514

Design of Electric Systems for Naval Aircraft and Missiles

包含图表

Comparison of Very F	Typical Current-Limi	Effect of Temperatur
Effect of Temperatur	A Method of Protecti	Another Method of Pr
Coordination of Fuse	Melting and Total-Cl	MS25244-5 Trip Chara
Coordination Misappl	Coordination Misappl	ICEA Wire Damage Cha
Typical Current Limi	FIGURE 5	FIGURE 5 (Continued)
FIGURE 5 (Continued)	FIGURE 5 (Continued)	FIGURE 5 (Continued)
Typical Coordination	Time-Current Charact	Aircraft Limiters Ap
Aircraft Limiters Ap	formula 1	formula 2
formula 3	formula 4	FIGURE A1
formula 5	formula 6	formula 7
formula 8	formula 9	Wire Resistance
Circuit Breaker Maxi	formula 10	formula 11
formula 12	Circuit Breaker Sele	TABLE B1-Continued
TABLE B1 - Continued	TABLE B1 - Continued	TABLE B1-Continued