| 摘要 |
<p>The invention relates to a vane (1) for use in a fluid flow of a turbine engine comprising a thin-walled radially extending aerodynamic vane body (2) having axially spaced leading and trailing edges (3, 4), the wall (5) of said vane body (2) comprising an outer shell (6) and an inner shell (7), the wall (5) of said vane body (2) defining an interior cavity (8) therein for flowing a cooling medium, and an radially outer platform (9), whereby a radially extending load strut (10) is arranged at the inner shell (7) of the wall (5) of the leading edge (3) of the vane body (2). The invention further relates to a turbine engine comprising at least one rotating wheel with a plurality of rotating vanes and at least one guide wheel with a plurality of guide vanes, whereby the rotating vanes and/or the guide vanes are built like the aforementioned vane.</p> |
