Invention Application
- Patent Title: GAS TURBINE ENGINE COMBUSTOR LINER PANEL
- Patent Title (中): 燃气轮机发动机衬板
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Application No.: US14897725Application Date: 2014-06-12
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Publication No.: US20160123592A1Publication Date: 2016-05-05
- Inventor: Christopher Drake , Frank J Cunha , Stanislav Kostka
- Applicant: UNITED TECHNOLOGIES CORPORATION
- International Application: PCT/US2014/042130 WO 20140612
- Main IPC: F23R3/00
- IPC: F23R3/00 ; F23R3/06
Abstract:
A liner panel is provided for a combustor of a gas turbine engine. The liner panel includes a multiple of heat transfer augmentors. At least one of the multiple of heat transfer augmentors includes a depression, where the depression includes an entrance to at least one passage through the liner panel.
Information query
