Fixed-wing aircraft cockpit

The invention relates to structural design of aircraft cockpits, in particular to a fixed-wing aircraft cockpit. The fixed-wing aircraft cockpit comprises mounting openings, mounting opening frames and emergency escape windows; the mounting openings are formed over a driver seat in the cockpit; the...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: GENG JIANZHONG, TAN YUTING, DUAN ZHUOYI, WANG BIN
Format: Patent
Sprache:chi ; eng
Schlagworte:
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Beschreibung
Zusammenfassung:The invention relates to structural design of aircraft cockpits, in particular to a fixed-wing aircraft cockpit. The fixed-wing aircraft cockpit comprises mounting openings, mounting opening frames and emergency escape windows; the mounting openings are formed over a driver seat in the cockpit; the mounting opening frames are matched with the mounting openings in shape and size and detachably and fixedly arranged in the mounting openings; and the emergency escape windows are matched with the mounting opening frames in shape and size and fixedly arranged in the mounting opening frames. According to the fixed-wing aircraft cockpit, the emergency escape windows are detachably arranged over the driver seat in the cockpit, thus on one hand, a driver can climb out of an escape outlet rapidly for escape through the seat, the required emergency evacuation time of the driver of a fixed-wing aircraft is shortened greatly, design difficulty can be also reduced, and the requirement for the internal space of the aircraft