公开(公告)号：US10801342B2

公开(公告)日：2020-10-13

申请号：US14644596

申请日：2015-03-11

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Mark David Ring ,  Scot A Webb ,  Mark J Rogers ,  Gerald D Cassella ,  Charles H Warner ,  Eric A Kuehne ,  Jonathan J Earl ,  Matthew M Zietala ,  Neil L Tatman ,  Randall J Butcher ,  Matthew R Willett ,  Nicholas R Leslie

IPC: F01D9/04 ,  F01D25/24

Abstract: A vane cluster for a gas turbine engine includes a first end-of-cluster vane, a second end-of-cluster vane, a neighbor vane adjacent to the second end-of-cluster vane at an interface that includes an angled load interface therebetween; and a multiple of base vanes between the first end-of-cluster vane and the neighbor vane, the angled load interface different than an interface between each of the multiple of base vane.