发明名称 Hole liners for repair of vane counterbore holes
摘要 A variable vane shroud (36) for a gas turbine engine (10) comprises a cylindrically shaped body, a hole (55B) arranged at a circumference of the body, and a counterbore (56B) arranged concentrically around the hole on a radially inward facing surface of the body. The hole (55B) is for receiving a trunnion (43) from a variable vane (32B) and the counterbore is for receiving a hub (45) from the variable vane (32B). A liner (52) is inserted into the hole (55B) and counterbore (56B) such that the trunnion (43) and hub (45) are provided with a contact surface. The invention also provides a method for repairing a damaged counterbore (54B) in a variable vane shroud (36). A liner (52) having a shape corresponding to a layer of material removed from the shroud is inserted into the void left by removing damaged material such that the counterbore is restored to pre-damaged dimensions.
申请公布号 EP1959094(A3) 申请公布日期 2010.06.16
申请号 EP20080250529 申请日期 2008.02.13
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 ADDIS, MARK E.
分类号 F01D5/00;B23P6/00;F01D9/04 主分类号 F01D5/00
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