Invention Grant
- Patent Title: Flow sleeve impingement cooling baffles
- Patent Title (中): 流动套筒冲击冷却挡板
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Application No.: US13553076Application Date: 2012-07-19
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Publication No.: US08794006B2Publication Date: 2014-08-05
- Inventor: Jaisukhlal V. Chokshi , Craig F. Smith , Carlos G. Figueroa , Larry C. George
- Applicant: Jaisukhlal V. Chokshi , Craig F. Smith , Carlos G. Figueroa , Larry C. George
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Kinney & Lange, P.A.
- Main IPC: F02C1/00
- IPC: F02C1/00
Abstract:
A combustor assembly for a turbine engine includes a combustor liner, a flow sleeve and a baffle ring. The flow sleeve surrounds the combustor liner. An annulus is formed between the flow sleeve and the combustor liner. A plurality of row of cooling holes are formed in the flow sleeve. The baffle ring radially surrounds the combustor liner and is located in the annulus.
Public/Granted literature
- US20130000310A1 FLOW SLEEVE IMPINGEMENT COOLING BAFFLES Public/Granted day:2013-01-03
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