| 摘要 |
<p>A static wing (1) comprises a ring portion (2) having an aerofoil shaped cross section. Positioned above the centre aperture of the ring portion (2) is a diffuser plate (3), the diffuser plate is optionally arranged to be moveable vertically (as shown by the direction arrow) between a closed operational position and an open operational position. At the outer circumference of the ring portion (2) there are provided a plurality of elevators (4) which are moveable in the directions shown by the arrows. The wing may be connected with a propulsion system by means of a mechanical coupling (5). The wing has potential application in both military platforms and civil aircraft.</p> |
