Thermally compliant liner
AssigneeUnited Technologies Corporation
InventorsKeith S. Brewer, Gary F. Chaplin, David R. Olsen
Life of this patent
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Abstract
The present invention relates to a thermally compliant liner for a gas turbine engine. The liner includes an outer wall, an inner wall spaced radially inwardly from the outer wall leaving a duct therebetween. A plurality of stiffeners are disposed in the duct. The stiffeners include a flexible medial portion which accommodates differential rates of thermal growth between the outer and inner walls. The stiffeners also include radially extending portions which in conjunction with the medial portion, minimize buckling of the liner due to pressure differentials.
Claims2
A liner for an augmentor of a gas turbine engine, comprising:
- an outer wall;
- an inner wall, spaced radially inwardly from the outer wall defining a duct therebetween;
- and
- a plurality of stiffeners disposed in the duct, each of said stiffeners including radially extending, inner and outer end portions attached to said inner and outer walls respectively, and a medial portion between said end portions, said medial portion having a pliant section
- wherein the pliant medial section of the stiffeners accommodates differential rates of thermal growth between the outer and inner wall and said inner and outer radially extending, end portions resist buckling of the walls due to pressure gradients.
Dependencies are inferred from the claim text.