Invention Grant
- Patent Title: Splitter for air bleed manifold
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Application No.: US14762092Application Date: 2013-12-18
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Publication No.: US10018118B2Publication Date: 2018-07-10
- Inventor: Philip Robert Rioux , Rishon Saftler
- 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
- International Application: PCT/US2013/076111 WO 20131218
- International Announcement: WO2014/143296 WO 20140918
- Main IPC: F02C7/18
- IPC: F02C7/18 ; F01D25/24 ; F02C6/08

Abstract:
A splitter for protecting parts of a gas turbine engine is provided. The splitter segregates the flow of hot and cold gases into the air bleed manifold around the high compressor section to reduce maximum temperatures and minimize the temperature gradients of engine parts, especially inner case flanges The splitter divides the air bleed manifold into an annular inner cavity and an outer cavity. The splitter directs relatively cold air from the high compressor bleed ducts into the inner cavity and relatively hot air from the aft hub into the outer cavity, away from the inner case flanges.
Public/Granted literature
- US20150354457A1 Splitter for Air Bleed Manifold Public/Granted day:2015-12-10
Information query
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