Gas turbine for use in aircraft, has sealing device to seal gap between pre-guiding units and pre-guiding vanes, where vanes and units are integrated in turbine and/or compressor of turbine
摘要
<p>The turbine has a number of pre-guiding vanes (15) and pre-guiding units (25) arranged in an axial direction. The pre-guiding vanes and pre-guiding units are integrated in the turbine and/or a compressor of the turbine. A sealing device (34) seals the gap (33) between the pre-guiding units and the pre-guiding vanes. An adjusting device is positioned at a radial external end of the pre-guiding vanes.</p>
