Invention Grant
- 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.: US11808455B2Publication Date: 2023-11-07
- Inventor: Lawrence A. Binek , Timothy S. Snyder , Sean R. Jackson
- Applicant: Raytheon Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: RTX CORPORATION
- Current Assignee: RTX CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: GETZ BALICH LLC
- Main IPC: F23R3/00
- IPC: F23R3/00 ; F23R3/28
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
- US20230160574A1 GAS TURBINE ENGINE COMBUSTOR WITH INTEGRAL FUEL CONDUIT(S) Public/Granted day:2023-05-25
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