摘要 |
A combustion system for an engine, such as a gas turbine engine is provided. The combustion system has a ceramic component (24), such as ceramic combustor liner, and at least one metal support component, such as a metal ring (20) or a plurality of metal cones (110,114, FIG. 7), for providing radial and axial support to the ceramic component. The at least one metal support component (20) includes a structure, such as axial slots (23) or radial slots, for minimizing stress and for increasing compliance of the metal support component (20) with respect to the ceramic component (24).
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申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SHI, JUN;LAWRENCE, JASON;BOMBARA, DAVID J.;TUTHILL, RICHARD S.;MELMAN, JEFFREY D. |