Invention Grant
- Patent Title: Integrated fan inlet case and bearing support for a gas turbine engine
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Application No.: US16275477Application Date: 2019-02-14
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Publication No.: US11002152B2Publication Date: 2021-05-11
- Inventor: Adam G. Smedresman , Felicia N. White
- 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: Carlson, Gaskey & Olds, P.C.
- Main IPC: F01D25/24
- IPC: F01D25/24 ; F01D25/16 ; F02C7/04 ; F04D29/056
Abstract:
A unitary fan inlet case and bearing support structure for a gas turbine engine includes an annular body having a radially inward ring connected to a radially outward ring via a plurality of struts. A platform protrudes radially inward from the radially inward ring. The platform includes a radially outward facing surface and a radially inward facing surface. The annular body is a single unitary structure.
Public/Granted literature
- US20200263566A1 INTEGRATED FAN INLET CASE AND BEARING SUPPORT FOR A GAS TURBINE ENGINE Public/Granted day:2020-08-20
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