| 摘要 |
<p>A turbo-jet thrust reverser comprising movable elements (7) which, when closed, are incorporated into the outer wall of the turbo-jet pipe, and, when open, may deflect the flow in said pipe. Blade-shaped elements (23) are arranged within each movable element (7) on the upstream side thereof and evenly spread out over the width thereof in a direction which is generally parallel to the geometrical thrust reverser axis, whereby deflecting walls for controlling reversed-flow layers are formed.</p> |
