| 摘要 |
The present invention relates to an aircraft (1, 1’, 1’’, 1’’’). The aircraft comprises: front glasses (50, 50’, 50’’, 50’’’) arranged on the front thereof; an edge (55) which limits a visible area (49) that a pilot can see; and a display unit (58) which displays one or more visual information (20, 25) of one or more flying parameters in the visible area (49) when one or more aircrafts (1, 1’, 1’’, 1’’’) are in a normal flying constitution state. |
