公开(公告)号：US10697372B2

公开(公告)日：2020-06-30

申请号：US15479750

申请日：2017-04-05

Applicant: General Electric Company

Inventor： Jeremy Kevin Payne ,  John Wilbur Acree ,  Anthony James Bailey ,  Satyambabu Kalyani ,  Thomas Alan Wall ,  Michael Alan Zupancic ,  Jonathan Russell Ratzlaff ,  Anthony Paul Greenwood ,  Kevin William Caldwell ,  Christophe Jude Day

IPC: F02C7/00 ,  F02C7/20 ,  F02C3/04 ,  F02C7/18 ,  F02C6/08

Abstract: An apparatus and method for a turbine engine having an engine core. A casing can contain a compressor section, a combustor section and a turbine section in axial flow arrangement. An air conduit can extend at least partially between the compressor section and the turbine section. A compliant interface can include a nut and a biasing device mount the air conduit to the casing.

公开(公告)号：US20180291812A1

公开(公告)日：2018-10-11

申请号：US15479750

申请日：2017-04-05

Applicant: General Electric Company

Inventor： Jeremy Kevin Payne ,  John Wilbur Acree ,  Anthony James Bailey ,  Satyambabu Kalyani ,  Thomas Alan Wall ,  Michael Alan Zupancic ,  Jonathan Russell Ratzlaff ,  Anthony Paul Greenwood ,  Kevin William Caldwell ,  Christophe Jude Day

IPC: F02C7/20 ,  F02C3/04

Abstract: An apparatus and method for a turbine engine having an engine core. A casing can contain a compressor section, a combustor section and a turbine section in axial flow arrangement. An air conduit can extend at least partially between the compressor section and the turbine section. A compliant interface can include a nut and a biasing device mount the air conduit to the casing.