Invention Grant
- Patent Title: Flow exchange baffle insert for a gas turbine engine component
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Application No.: US14997992Application Date: 2016-01-18
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Publication No.: US10253636B2Publication Date: 2019-04-09
- Inventor: Matthew A. Devore , Eleanor D. Kaufman
- 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: F01D5/18
- IPC: F01D5/18 ; F01D25/12 ; F01D9/02 ; F01D9/06

Abstract:
A baffle insert for a component of a gas turbine engine is provided. The baffle insert having: a first fluid conduit having a first interior cavity extending therethrough; a second fluid conduit having a second interior cavity extending therethrough; and a member located between the first fluid conduit and the second fluid conduit, wherein the member fluidly couples the first interior cavity to an exterior of the second fluid conduit, and wherein the member fluidly couples the second interior cavity to an exterior of the first fluid conduit and wherein the first interior cavity is isolated from the second interior cavity.
Public/Granted literature
- US20170204731A1 FLOW EXCHANGE BAFFLE INSERT FOR A GAS TURBINE ENGINE COMPONENT Public/Granted day:2017-07-20
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