Reduced power mode for an aircraft electric brake system
作者： Erik Godo
DOI:
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摘要: An electric brake system for an aircraft as described herein is capable of operating in a normal full power mode, low and sleep mode. The mode supported by the active supply aircraft, while modes are backup (e.g., battery) aircraft. activated response to detection certain conditions or states where braking performance not required. For example, can be utilized connection with towing operations parking adjustment operations. absence commands extended period time. Various parameters and/or settings adjusted, controlled, regulated during achieve reduced consumption relative
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