Invention Grant
US09206742B2 Passages to facilitate a secondary flow between components 有权
通道以促进组件之间的二次流动

Passages to facilitate a secondary flow between components
Abstract:
An annular mount for a gas turbine engine includes a first flange and a second flange. The first flange has an arcuate shape, and the second flange extends from the first flange. The second flange has an interface surface along at least one side and has a plurality of mounting apertures extending therethrough. The channels extend along a length of the interface surface from a first edge to a second edge.
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