| 摘要 |
<P>PROBLEM TO BE SOLVED: To provide a fire suppression system suitable for use in an aircraft, which takes the place of a halon-based fire suppression system. <P>SOLUTION: A programmable controller (126) for a fire suppression system includes: a rewritable memory module (260); a processor module (262); multiple sensor input parts (210, 212, 214, 216, 218, 222, 272); and multiple control signal output parts (230, 232, 236, 238, 240, 242, 250, 274). <P>COPYRIGHT: (C)2012,JPO&INPIT |
