Invention Application
- Patent Title: FAN CONTAINMENT CASE FOR GAS TURBINE ENGINES
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Application No.: US15686255Application Date: 2017-08-25
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Publication No.: US20190063460A1Publication Date: 2019-02-28
- Inventor: Mark W. Costa
- Applicant: United Technologies Corporation
- Main IPC: F04D29/52
- IPC: F04D29/52 ; F02K3/06 ; F01D21/04 ; F04D29/02 ; F01D11/12

Abstract:
A fan section for a gas turbine engine according to an example of the present disclosure includes, among other things, a fan containment case assembly that has an outer case extending about an axis, and a thermally conforming liner assembly radially inward of the outer case. The liner assembly has a shell, a wrap radially outward of the shell, and a ballistic liner between the outer case and the wrap. The wrap has a first fiber construction, and the ballistic liner has a second fiber construction that differs from the first fiber construction in stiffness.
Public/Granted literature
- US10480530B2 Fan Containment case for gas turbine engines Public/Granted day:2019-11-19
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