Invention Grant
- Patent Title: Baffle insert for a gas turbine engine component
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Application No.: US14961644Application Date: 2015-12-07
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Publication No.: US10577947B2Publication Date: 2020-03-03
- Inventor: Brandon W. Spangler , Atul Kohli
- 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: Cantor Colburn LLP
- Main IPC: F02C1/00
- IPC: F02C1/00 ; F01D5/18 ; F01D9/02 ; F01D11/08 ; F01D25/12 ; F23R3/00
Abstract:
A baffle insert for a component of a gas turbine engine is provided. The baffle insert having: a plurality of trip strips extending upwardly from an exterior surface of the baffle insert; and at least one rib extending upwardly from the exterior surface of the baffle insert.
Public/Granted literature
- US20170159455A1 BAFFLE INSERT FOR A GAS TURBINE ENGINE COMPONENT Public/Granted day:2017-06-08
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