Stationary vane model aeroplane and model ship
The utility model discloses a stationary vane model aeroplane and model ship, including fuselage, aircraft nose and two fins, the long 68.5cm of fuselage, span 50cm, two fins install in the rear of fuselage, the external diameter distance of being close to between two fins of tail one end be 11.53cm...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | The utility model discloses a stationary vane model aeroplane and model ship, including fuselage, aircraft nose and two fins, the long 68.5cm of fuselage, span 50cm, two fins install in the rear of fuselage, the external diameter distance of being close to between two fins of tail one end be 11.53cm, the external diameter distance of being close to between two fins of aircraft nose one end is 12.27cm, fin width 1cm, fuselage and aircraft nose between install the connecting plate, the angle of connecting plate and fuselage bottom be 8 degrees. The utility model discloses an optimize the width of fuselage and abdominal streamline, the two vertical tail front and back installations of adjustment, improved the lift when model aeroplane and model ship take off, reduced relative energy consumption to make the ability reinforcing that aircraft automatic correction flight gesture is unusual, flight performance is more stable.
本实用新型公开了种固定翼航模,包括机身、机头和两个尾翼,所述的机身长68.5cm,翼展50cm,所述的两个尾翼安装于机身的后方,靠近机尾端的两个尾翼之间的外径距离为11.53cm,靠近 |
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