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公开(公告)号：US11215119B2
公开(公告)日：2022-01-04
申请号：US16814159
申请日：2020-03-10
Applicant: RAYTHEON TECHNOLOGIES CORPORATION
Inventor： Ken F. Blaney , Thomas E. Clark
Abstract: A blade outer air seal assembly includes a support structure arranged about an axis. At least one blade outer air seal segment is mounted in the support structure. A flow guide is arranged between the support structure and the at least one blade outer air seal segment defining a passage between the flow guide and the blade outer air seal segment. The passage extends in a generally axial direction.
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