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公开(公告)号：US10927851B2
公开(公告)日：2021-02-23
申请号：US16367673
申请日：2019-03-28
Applicant: Raytheon Technologies Corporation
Inventor： JinQuan Xu , Frederic Tisdall Tenney
Abstract: A stage of a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a row of flow directing components circumferentially disposed about a centerline axis and at least one flow directing component of the row having at least one design characteristic that is dissimilar from a corresponding design characteristic of at least one other flow directing component of the row.
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