Composite ceramic/metal cylinder for gas turbine engine
AssigneeAvco Corporation
InventorsEdward O. Hartel, Zoltan L. Libertini, Joseph C. Manente, Jr., Donald E. Wilson
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AssigneeAvco Corporation
InventorsEdward O. Hartel, Zoltan L. Libertini, Joseph C. Manente, Jr., Donald E. Wilson
Estimating the term…
A cylinder of a gas turbine engine is formed of a multilayered construction including a radially inner ceramic ring, the inner surface of which is juxtaposed to the tips of a turbine rotor, an intermediate arrangement of two annular ceramic rings that are substantially L-shaped in cross-section and are disposed in mirror image so as to entrap the radially inner ceramic ring, and a radially outer metallic support means which envelopes the intermediate ceramic rings for maintaining the composite ceramic structure during different operating modes of the turbine engine. The composite ceramic portion of the cylinder enables the engine to operate at higher temperatures, and offers the potential for improved turbine tip clearance control, since the ceramic material is less sensitive to thermal distortion.
A gas turbine engine cylinder forming a portion of the turbine assembly surrounding the tips of a plurality of blades of a rotor, said cylinder comprising:
Dependencies are inferred from the claim text.