Invention Grant
- Patent Title: Gas turbine engine component cooling passage turbulator
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Application No.: US15036833Application Date: 2014-11-05
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Publication No.: US10364683B2Publication Date: 2019-07-30
- Inventor: Brooks E. Snyder , Thomas N. Slavens , Nicholas M. LoRicco , James T. Auxier
- 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.
- International Application: PCT/US2014/064011 WO 20141105
- International Announcement: WO2015/077017 WO 20150528
- Main IPC: F01D5/18
- IPC: F01D5/18
Abstract:
A gas turbine engine component includes opposing walls that provide an interior cooling passage. One of the walls has a turbulator with a hook that is enclosed within the walls.
Public/Granted literature
- US20160290139A1 GAS TURBINE ENGINE COMPONENT COOLING PASSAGE TURBULATOR Public/Granted day:2016-10-06
Information query
