Invention Grant
- Patent Title: Fuel injector assembly for a turbine engine
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Application No.: US17108606Application Date: 2020-12-01
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Publication No.: US11649964B2Publication Date: 2023-05-16
- Inventor: Lawrence A. Binek , Timothy S. Snyder
- 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: Getz Balich LLC
- Main IPC: F23R3/60
- IPC: F23R3/60 ; F23R3/28 ; F23D14/58 ; F23D14/64
Abstract:
An apparatus is provided for a turbine engine. This turbine engine apparatus includes a monolithic body. The monolithic body includes a splash plate and a fuel nozzle. The splash plate includes a splash plate surface. The fuel nozzle includes a nozzle orifice. The fuel nozzle is configured to direct fuel out of the nozzle orifice to impinge against the splash plate surface.
Public/Granted literature
- US20220170636A1 FUEL INJECTOR ASSEMBLY FOR A TURBINE ENGINE Public/Granted day:2022-06-02
Information query
