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公开(公告)号：US10935240B2
公开(公告)日：2021-03-02
申请号：US14694086
申请日：2015-04-23
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Hoyt Y Chang , Brooks E Snyder , Thomas N Slavens
Abstract: A heat shield for use in a combustor of a gas turbine engine including a plurality of standoff pins that extend from a cold side, the plurality of standoff pins at least partially surround an attachment stud, the cold side including at least one film cooling hole adjacent to the plurality of standoff pins and the attachment stud.
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