An aircraft with a fuselage, wings, horizontal stabilizers and a vertical stabilizer, wherein on a front portion of the vertical stabilizer an elongated one-piece nose element is mounted which forms lateral air guide surfaces. To the front end of the nose element a perforated metal plate nose member is attached. The front end of the nose element being closed and between this closed front end and the nose member an elongated air channel is formed.
LEADING EDGE NOSE STRUCTURE ON THE VERTICAL STABILIZER OF AN AIRCRAFT
2015-12-17
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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