초록 ▼

A hot gas turbine wheel shroud ring, for hot gas turbine engines, is adapted to be concentrically positioned around the periphery of a row of buckets or blades on the circumference of a turbine wheel to provide a predetermined small sealing and running clearance between the tips of the turbine blade

A hot gas turbine wheel shroud ring, for hot gas turbine engines, is adapted to be concentrically positioned around the periphery of a row of buckets or blades on the circumference of a turbine wheel to provide a predetermined small sealing and running clearance between the tips of the turbine blades and the ring. The shroud ring is characterized as incorporating certain opposite warping or deflection characteristics from those found in shroud rings under normal high temperature operating conditions.

대표청구항 ▼

A shroud ring for a hot gas turbine engine having a casing, a turbine wheel concentrically mounted in said casing and a combustion chamber to supply hot gases to said turbine wheel, (a) said casing having a radially tapering wall therein along which said hot gases flow, (b) said shroud ring being fi

A shroud ring for a hot gas turbine engine having a casing, a turbine wheel concentrically mounted in said casing and a combustion chamber to supply hot gases to said turbine wheel, (a) said casing having a radially tapering wall therein along which said hot gases flow, (b) said shroud ring being fixedly positioned in said casing concentrically about said turbine wheel, (c) said shroud ring having a cross-section illustrating a generally U shape or channel member having a bottom wall and a pair of opposite upstanding walls with oppositely directed faces, (d) said channel member being formed in an annular or ring configuration with said sidewalls being in a radially outward and upstanding relationship with respect to said bottom wall, (e) said bottom wall having a radially outwardly directed curve or bow therein between said sidewalls.