Invention Publication
- Patent Title: GAS TURBINE ENGINE COMBUSTOR WITH INTEGRAL FUEL CONDUIT(S)
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Application No.: US17535133Application Date: 2021-11-24
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Publication No.: US20230160574A1Publication Date: 2023-05-25
- Inventor: Lawrence A. Binek , Timothy S. Snyder , Sean R. Jackson
- Applicant: Raytheon Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: Raytheon Technologies Corporation
- Current Assignee: Raytheon Technologies Corporation
- Current Assignee Address: US CT Farmington
- Main IPC: F23R3/28
- IPC: F23R3/28 ; F23R3/00
Abstract:
An assembly is provided for a gas turbine engine. This assembly includes a combustor and a fuel conduit. The combustor includes a combustor wall that forms a peripheral boundary of a combustion chamber within the combustor. The fuel conduit extends along and is formed integral with the combustor wall. The fuel conduit is disposed outside of the combustion chamber.
Public/Granted literature
- US11808455B2 Gas turbine engine combustor with integral fuel conduit(s) Public/Granted day:2023-11-07
Information query
