Invention Grant
US07640743B2 Aircraft flight control user interface linkage system 失效
飞机飞行控制用户界面联动系统

Aircraft flight control user interface linkage system
Abstract:
A user interface linkage system includes first and second user interfaces that are linked by a single hydraulic circuit. The system is configured to provide compensation for relatively slow changes in hydraulic fluid pressure due, for example, to temperature variations. The system is also configured to allow the user interfaces to be selectively unlinked from each other.
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