发明名称 Airplane Status System
摘要 A flight deck display that represents the overall health of the airplane by combining energy state, system state and configuration state into one integrated representation that is triggered by the on-board engine indication and crew alerting system. The computer system for controlling the display unit is configured to display an airplane status indicator in the form of a symbolic representation of the airplane that persists across displays. The status indicator shows the energy state of the airplane and how energy is being added or subtracted from it in terms of altitude, airspeed, thrust, wind, etc. As the airplane gains energy, there is a projection of excess energy shown in front of the airplane. As the airplane loses energy, an alerting indicator will appear around the airplane symbol if the performance of the airplane becomes is too low.
申请公布号 US2017088284(A1) 申请公布日期 2017.03.30
申请号 US201514865794 申请日期 2015.09.25
申请人 The Boeing Company 发明人 Holder Barbara E.
分类号 B64D45/00 主分类号 B64D45/00
代理机构 代理人
主权项 1. A computer-implemented method for displaying airplane status information, comprising: operating an airplane; displaying first symbology representing the airplane on a display screen; monitoring performance of the airplane during operation; and displaying second symbology when a value of a performance parameter of the airplane reaches a first preset threshold, wherein said second symbology surrounds at least a portion of said first symbology and has a first color.
地址 Chicago IL US
您可能感兴趣的专利