| 摘要 |
<p>An aircraft system for control of the application of power to a plurality of devices (390, 391, 400, 401)in the aircraft comprises a plurality of local control modules (35, 36). Each local control module (35, 36) controls the application of the power to the group of at least one device (390, 391, 400, 401). A central control system (38) communicates with and controls the local control modules (35, 36). The system is particularly applicable to an ice protection system.</p> |
