Invention Grant
US09441499B2 System and method relating to axial positioning turbine casings and blade tip clearance in gas turbine engines 有权
与涡轮机壳体轴向定位和燃气涡轮发动机叶片间隙相关的系统和方法

System and method relating to axial positioning turbine casings and blade tip clearance in gas turbine engines
Abstract:
A system for passively varying an axial position of an inner casing of a gas turbine pursuant to changing pressure in a flowpath during transient engine operation. The system may include: a connection assembly slidably connecting the inner casing to the outer casing for axial movement of the inner casing between a first position and a second position; means for pressurizing the annulus relative to a flowpath pressure; biasing means for axially preloading the inner casing toward the first position; and an inner casing receiving surface configured to receive a pressure in the annulus for axially loading the inner casing in opposition to the axial preload of the biasing means.
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