Invention Grant
- Patent Title: Gas turbine engine with integral combustion liner and turbine nozzle
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Application No.: US16212879Application Date: 2018-12-07
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Publication No.: US11248789B2Publication Date: 2022-02-15
- Inventor: Lawrence Binek , Jesse R. Boyer , Dmytro Mykolayovych Voytovych
- Applicant: UNITED TECHNOLOGIES CORPORATION
- Applicant Address: US CT Farmington
- Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F23R3/00
- IPC: F23R3/00 ; F23R3/16 ; F23R3/26 ; F23R3/04 ; F23R3/06

Abstract:
A core engine article includes a combustor liner defining a combustion chamber therein and a turbine nozzle. The combustor liner includes a plurality of injector ports, and the plurality of injector ports have a shape that tapers to a corner on a forward side of the injector ports. The turbine nozzle includes a plurality of airfoils. The combustor liner and turbine nozzle are integral with one another. A method of making a core engine article is also disclosed.
Public/Granted literature
- US20200182467A1 ENGINE ARTICLE WITH INTEGRAL LINER AND NOZZLE Public/Granted day:2020-06-11
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