Invention Grant
- Patent Title: Gas turbine engine dilution chute geometry
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Application No.: US16791499Application Date: 2020-02-14
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Publication No.: US11543127B2Publication Date: 2023-01-03
- Inventor: Lawrence A. Binek , Brendan T. Gustafson
- 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: F23R3/06
- IPC: F23R3/06 ; F23R3/00 ; B33Y80/00
Abstract:
A combustor for a gas turbine engine includes a combustor liner and a dilution chute integral and conformal with the combustor liner to provide an outlet into the combustor for fuel, wherein the dilution chute has at least one wall with a tapered edge extending into an interior of the combustor.
Public/Granted literature
- US20210254831A1 GAS TURBINE ENGINE DILUTION CHUTE GEOMETRY Public/Granted day:2021-08-19
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