Invention Grant
- Patent Title: Support structure for a turbine vane of a gas turbine engine
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Application No.: US16593638Application Date: 2019-10-04
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Publication No.: US11753952B2Publication Date: 2023-09-12
- Inventor: Lawrence A. Binek , David W. Morganson
- 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: Kinney & Lange, P. A.
- Main IPC: F01D9/02
- IPC: F01D9/02 ; F01D9/04 ; F23R3/00 ; F23R3/50 ; B22F10/40 ; B22F10/64 ; B33Y10/00 ; B33Y80/00
Abstract:
A method of manufacturing a turbine vane within an engine case includes additively manufacturing a combustor liner within an engine case, additively manufacturing a support structure attached to the combustor liner at a radially distal position, and additively manufacturing the turbine vane attached to the support structure at an inwardly adjacent position to the radially distal position.
Public/Granted literature
- US20210102704A1 ENGINE TURBINE SUPPORT STRUCTURE Public/Granted day:2021-04-08
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