| 摘要 |
<p>The invention relates to a stator for installation in a rear section of a jet engine, the stator comprising a plurality of guide vanes (104, 204, 304) which extend in the radial direction of the stator and between them define ducts for leading a gas. A first side (105) of the stator in its axial direction defines an inlet for the gas and a second side (107), opposite the first, side defines an outlet for the gas . Said guide vanes (104, 204, 304) have such a shape that together they at least substantially cover said gas inlet (105) viewed in the axial direction of the stator from the outlet side (107) thereof .</p> |
