Invention Grant
- Patent Title: Gas turbine combustor fuel injector flow device including vanes
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Application No.: US16808443Application Date: 2020-03-04
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Publication No.: US11280495B2Publication Date: 2022-03-22
- Inventor: Gurunath Gandikota , Steven Clayton Vise , Perumallu Vukanti , Mayank Krisna Amble , Clayton Stuart Cooper , Nicholas Ryan Overman , Karthikeyan Sampath , Allen Michael Danis , Craig Douglas Young
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Venable LLP
- Agent Jacqueline A. DiRamio; Michele V. Frank
- Main IPC: F23R3/14
- IPC: F23R3/14 ; F23R3/28 ; F23R3/00 ; F02C7/22

Abstract:
A flow device for a combustor assembly defining a longitudinal axis around which the flow device is positioned is provided. The flow device includes a body extended around the longitudinal axis. The body includes a first wall and a second wall separated longitudinally from one another along the longitudinal axis. A fuel injector passage is defined through the body coaxial to the longitudinal axis. A plurality of vane walls is extended radially between the first wall and the second wall relative to the longitudinal axis. A radial flow passage is extended between the plurality of vane walls and the fuel injector passage.
Public/Granted literature
- US20210278085A1 Fuel Injector Flow Device Public/Granted day:2021-09-09
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