Invention Grant
- Patent Title: Fan case assembly for gas turbine engine
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Application No.: US16036513Application Date: 2018-07-16
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Publication No.: US10724403B2Publication Date: 2020-07-28
- Inventor: Mark W. Costa
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: RAYTHEON TECHNOLOGIES CORPORATION
- Current Assignee: RAYTHEON TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: Cantor Colburn LLP
- Main IPC: F01D11/12
- IPC: F01D11/12 ; F01D25/24 ; F04D29/52 ; F01D11/08 ; F01D21/04
Abstract:
A fan case assembly for a gas turbine engine includes a honeycomb structure. The fan case assembly also includes a septum operatively coupled to the honeycomb structure and located radially inward of the honeycomb structure. The fan case assembly further includes a rubstrip in contact with the septum and located radially inward of the septum.
Public/Granted literature
- US20200018185A1 FAN CASE ASSEMBLY FOR GAS TURBINE ENGINE Public/Granted day:2020-01-16
Information query
