Indicator bars of dynamic graphical user interface of aircraft cockpit display panel

Abstract

1. Name of the product of this design: Indicator bar of a dynamic graphical user interface of an aircraft cockpit display panel. 2. Purpose of the product of this design: The part for which protection is sought in this design is the area in the main view that is not covered by the gray translucent layer. This part is the portion of the aircraft cockpit display panel that is used to display the folding status and dynamic folding process of the aircraft's folding wingtips, providing the pilot with a clear visual display of the folding wingtip status. 3. The design highlights of this appearance design product are only located in the local part of the graphical user interface, including the design of the wingtip indicator icon in the indicator bar, the text label design, and the dynamic change process. 4. The picture or photo that best illustrates the key points of the design: main view. 5. Explanation of other reference figures for situations that require explanation: Partial design enlarged change state Figure 1 to partial design enlarged change state Figure 8 are enlarged views of the area requiring protection in the main view. Figure 1 shows the state of the aircraft wing tip expansion. As the wingtips of the aircraft are gradually folded, the main view jumps to the local design enlarged change state diagram 2, the local design enlarged change state diagram 2 jumps to the local design enlarged change state diagram 3, and the local design enlarged change state diagram 3 jumps to the local design enlarged change state diagram 4, which are used to represent the folding process of the aircraft wingtips. FIG4 shows the state where the aircraft wingtips are fully retracted. As the wingtip of the aircraft gradually unfolds, the local design enlarged change state diagram 4 jumps to the local design enlarged change state diagram 5, from the local design enlarged change state diagram 5 jumps to the local design enlarged change state diagram 6, from the local design enlarged change state diagram 6 jumps to the local design enlarged change state diagram 7, and from the local design enlarged change state diagram 7 jumps to the local design enlarged change state diagram 8, to represent the unfolding process of the aircraft wingtip. The partial design enlarged change state Figure 8 shows the state of the aircraft wing tip fully extended. 6. Other situations that require explanation: The aircraft cockpit display panel is of conventional design, omitting the rear view, left view, right view, top view and bottom view.