Invention Grant
- Patent Title: Thermal insulation features for gas turbine engines
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Application No.: US16881781Application Date: 2020-05-22
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Publication No.: US11268404B2Publication Date: 2022-03-08
- Inventor: David W. Morganson , Lawrence A. Binek
- Applicant: Raytheon Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: Raytheon Technologies Corporation
- Current Assignee: Raytheon Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Kinney & Lange, P.A.
- Main IPC: F01D25/14
- IPC: F01D25/14 ; F01D9/00 ; F02C7/32 ; B33Y80/00
Abstract:
A hot section of a gas turbine engine includes a stator housing wall and an at least one insulating standoff attached to the stator housing wall, extending radially away from the stator housing wall. The hot section includes an accessory module attached to an opposite end of the at least one insulating standoff away from the stator housing wall.
Public/Granted literature
- US20210363897A1 THERMAL INSULATION FEATURES FOR GAS TURBINE ENGINES Public/Granted day:2021-11-25
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