| 摘要 |
<p>The invention concerns an adjustable control surface (3) comprising two surface elements (4, 5) mobile relative to each other whereof one (5) is fixed relative to the craft body (1). One (4) of the elements has an internally positioned part adjacent to the body (1), relative to another part externally positioned adjacent to the other element (5). The adjustable element can be fixed to an axis of rotation (14) The fixed element (5) external part (9) can comprise a rear part (10) acting as its support pylon on the body (1). The invention is applicable to adjustable control surfaces of missiles.</p> |
