Invention Grant
- Patent Title: Multiple source impingement baffles for gas turbine engine components
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Application No.: US15982163Application Date: 2018-05-17
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Publication No.: US10697310B2Publication Date: 2020-06-30
- Inventor: Corey D. Anderson , Jeremy Styborski
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: RAYTHEON TECHNOLOGIES CORPORATION
- Current Assignee: RAYTHEON TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: Cantor Colburn LLP
- Main IPC: F01D5/18
- IPC: F01D5/18 ; F01D9/06

Abstract:
Partitioned baffles and components for installation within gas turbine engines are provided. The partitioned baffles include a baffle body defining a first cavity, the baffle body having a first inlet and at least one first impingement hole arranged for flow to pass through the first cavity from the first inlet to the at least one first impingement hole and a partitioned channel installed within the baffle body and defining a second cavity, wherein the partitioned channel has a second inlet and at least one second impingement hole, wherein a flow through the second cavity flows from the second inlet to the at least one second impingement hole. The baffle body is configured to receive cooling air from a first source and the partitioned channel is configured to receive cooling air from a second source, wherein the first source is different from the second source.
Public/Granted literature
- US20190353038A1 MULTIPLE SOURCE IMPINGEMENT BAFFLES FOR GAS TURBINE ENGINE COMPONENTS Public/Granted day:2019-11-21
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