Invention Grant
- Patent Title: Fan case ice liner for turbofan engine
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Application No.: US15032161Application Date: 2014-05-23
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Publication No.: US10294960B2Publication Date: 2019-05-21
- Inventor: Thomas J. Robertson , Steven Clarkson
- Applicant: UNITED TECHNOLOGIES CORPORATION
- Applicant Address: US CT Farmington
- Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: Cantor Colburn LLP
- International Application: PCT/US2014/039360 WO 20140523
- International Announcement: WO2015/065526 WO 20150507
- Main IPC: F04D29/52
- IPC: F04D29/52 ; F02C7/05 ; F02C7/047 ; F01D25/02 ; F04D29/02

Abstract:
An ice liner assembly for a fan containment case for a turbofan gas turbine engine is disclosed. The disclosed ice liner assembly includes a plurality of arcuate panels arranged end to end to form a cylindrical liner that is disposed within the fan containment case and aft of the fan and abradable strip liner that circumscribes the fan. Because the plurality of arcuate panels are arranged end to end fashion, the ice liner assembly includes a plurality of splice joints, or a joint between two abutting ends of two arcuate panels. The splice joints are reinforced with molded polymeric splice support cores that are substantially lighter and less expensive than currently employed high density aluminum honeycomb core materials.
Public/Granted literature
- US20160258445A1 FAN CASE ICE LINER FOR TURBOFAN ENGINE Public/Granted day:2016-09-08
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