| 摘要 |
A fire suppression system for a plurality of enclosures (17) in an aircraft comprises a plurality of bottles (1a, 1b) containing fire suppression agent, a temperature sensor and a pressure sensor on each bottle for measuring temperature and pressure data of the bottle contents, an addressable bottle valve (2a) on each bottle and a control unit (12). The control unit is configured to analyse the temperature and pressure data for each bottle to determine adequacy of fire suppression agent content for extinguishing a fire in a particular enclosure of the aircraft. The control unit is further configured to control the bottle valves independently by using the bottle valves' addresses, in order to manage the release of fire suppression agent. |
