Invention Grant
- Patent Title: Gas turbine engine noise reducing nose cone
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Application No.: US14766825Application Date: 2014-02-13
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Publication No.: US10371051B2Publication Date: 2019-08-06
- Inventor: Jonathan Gilson , Nigel David Sawyers-Abbott
- 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.
- International Application: PCT/US2014/016196 WO 20140213
- International Announcement: WO2014/133770 WO 20140904
- Main IPC: F01D5/02
- IPC: F01D5/02 ; F01D25/24 ; F02C7/045
Abstract:
A fan section for a gas turbine engine includes a fan hub and a nose cone section operatively mounted to the fan hub. The nose cone section includes a noise attenuation feature.
Public/Granted literature
- US20160032832A1 GAS TURBINE ENGINE NOISE REDUCING NOSE CONE Public/Granted day:2016-02-04
Information query
