公开(公告)号：US10190425B2

公开(公告)日：2019-01-29

申请号：US14916291

申请日：2014-09-03

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Christopher Drake ,  Christopher B Lyons

IPC: F01D9/06 ,  F01D9/04 ,  F01D25/24 ,  F01D5/18 ,  F01D11/00 ,  F01D25/12 ,  F23R3/04

Abstract: A gas turbine engine includes an engine static structure that has a fluid port. A turbine vane is supported relative to the engine static structure and includes a cooling passage. A flow splitter is provided between the engine static structure and the turbine vane. The flow splitter is configured to divide a flow upstream from the flow splitter into a first fluid flow provided to the fluid port and a second fluid flow provided to the cooling passage.