| 摘要 |
<p>A stator vane (4) for a gas turbine engine having a varying chordal length (52, 54) is disclosed. The chordal length reaches a maximum (52) at a point intermediate the ends (40, 44) of the vane for defining a radially varying nozzle throat (58, 56) between adjacent vanes (4, 4a) in a stator vane stage.</p> |
