| 摘要 |
<p>The present invention relates to a flying submarine probe, comprising: airplane-type wings arranged at the left and right sides of an enclosed hull, such that the wings are adjustable in the horizontal and vertical directions by up to 180 degrees; and propeller-type propulsion body integrally installed on the wings so as to provide power in the forward/backward and upward/downward directions according to the angle of the wings.</p> |
