发明公开
EP2072394A2 Aircraft flight control user interface fluid linkage system 审中-公开
Fluidverbindung vonFlugzeugsteuerungsbenutzeroberflächen

Aircraft flight control user interface fluid linkage system
摘要:
A user interface fluid linkage system includes first (102) and second (104) user interfaces that are linked by a single, constant volume fluid line (110). The system includes identically configured, but oppositely mounted hydraulic fluid chambers (106) to link motion between the first and second user interfaces.
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