发明申请
US20110268580A1 Axially segmented guide vane mount for a gas turbine 有权
用于燃气轮机的轴向分段导叶架

Axially segmented guide vane mount for a gas turbine
摘要:
A stator blade carrier for a gas turbine is provided. The stator blade carrier includes a plurality of axial segments. At least one axial segment is designed as a tubular lattice structure. This allows a simpler design technically and a more flexible adaptation to the temperature profile present on the stator blade carrier to maintain operational safety.
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