Guide blade sealing device for gas turbo group, has compressor and turbine guide blades and axially limiting hot spot segments, which are connected among each other in gas-tight manner using temperature-resistant skeletal laminations
摘要
<p>The device has a guide blade row with compressor guide blades and/or turbine guide blades (18), which are fastened at a set of separate ring segments. The ring segments are detachably fastened at a carrier structure in such a manner that the ring segments with the guide blades are individually detachable from the carrier structure under retention of the carrier structure. The guide blades and axially limiting hot spot segments (22) are connected among each other in a gas-tight manner using temperature-resistant flexible skeletal laminations (30).</p>
