Invention Grant
- Patent Title: Gas turbine engine combustor liner panel
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Application No.: US14896576Application Date: 2014-04-14
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Publication No.: US10352566B2Publication Date: 2019-07-16
- Inventor: Christopher Drake , Stanislav Kostka, Jr. , Frank J. Cunha
- 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: O'Shea Getz, P.C.
- International Application: PCT/US2014/034009 WO 20140414
- International Announcement: WO2015/002686 WO 20150108
- Main IPC: F23R3/00
- IPC: F23R3/00 ; F23R3/06
Abstract:
A liner panel for a combustor of a gas turbine engine includes a multiple of heat transfer augmentors. At least one of the multiple of heat transfer augmentors includes a hemi-spherical protuberance.
Public/Granted literature
- US20160116166A1 GAS TURBINE ENGINE COMBUSTOR LINER PANEL Public/Granted day:2016-04-28
Information query
