Invention Grant
- Patent Title: Turbine engine conduit interface
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Application No.: US15479750Application Date: 2017-04-05
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Publication No.: US10697372B2Publication Date: 2020-06-30
- 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
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Hanley, Flight and Zimmerman, LLC
- Main IPC: F02C7/00
- 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.
Public/Granted literature
- US20180291812A1 TURBINE ENGINE CONDUIT INTERFACE Public/Granted day:2018-10-11
Information query
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