Invention Grant
- Patent Title: Fan spacer for a gas turbine engine
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Application No.: US15915379Application Date: 2018-03-08
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Publication No.: US10781702B2Publication Date: 2020-09-22
- Inventor: Arun K. Theertham , Peter Karkos
- 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: Carlson, Gaskey & Olds, P.C.
- Main IPC: F01D5/30
- IPC: F01D5/30 ; F01D5/02 ; F02K3/06 ; F04D19/00 ; F01D11/00
Abstract:
A multi-piece fan spacer for a gas turbine engine includes at least one lug comprising a platform portion, a connection portion radially inward of the platform portion, and a support connecting the platform portion to the connection portion. The multi-piece fan spacer includes a plurality of platforms. Each of the platforms is connected to at least one axially adjacent platform portion.
Public/Granted literature
- US20190277145A1 FAN SPACER FOR A GAS TURBINE ENGINE Public/Granted day:2019-09-12
Information query
