公开(公告)号：US10655502B2

公开(公告)日：2020-05-19

申请号：US15606005

申请日：2017-05-26

Applicant: United Technologies Corporation

Inventor： Brian Barainca ,  Gary F. Fowler

IPC: F01D1/02 ,  F01D25/24 ,  F01D9/04

Abstract: A stator assembly of a gas turbine engine according to an example of the present disclosure includes, among other things, a first shroud extending about an axis to bound a flow path. The first shroud defines a first shroud opening. An airfoil has an airfoil body extending from a first end portion. The first end portion is received in the first shroud opening and defines at least one airfoil opening. At least one retention clip has an arcuate portion extending from a first elongated leg portion. The first elongated leg portion and the arcuate portion are received through the at least one airfoil opening such that the at least one retention clip limits movement of the airfoil relative to the first shroud.