Invention Grant
- Patent Title: Combustion liner seal with heat transfer augmentation
- Patent Title (中): 具有传热增强的燃烧衬套密封
-
Application No.: US10856592Application Date: 2004-05-28
-
Publication No.: US07007482B2Publication Date: 2006-03-07
- Inventor: Andrew Green , Peter Stuttaford , Jeffrey Arthur Benoit , Vamsi Duraibabu , Hany Rizkalla
- Applicant: Andrew Green , Peter Stuttaford , Jeffrey Arthur Benoit , Vamsi Duraibabu , Hany Rizkalla
- Applicant Address: US FL Jupiter
- Assignee: Power Systems Mfg., LLC
- Current Assignee: Power Systems Mfg., LLC
- Current Assignee Address: US FL Jupiter
- Agent Brian R. Mack; Christopher Hayes
- Main IPC: F02C7/12
- IPC: F02C7/12

Abstract:
A gas turbine combustion liner is disclosed having an alternate interface region between it and a transition duct where the cooling effectiveness and heat transfer along the aft end of the combustion liner is improved, resulting in extended component life. The region of the combustion liner proximate its second end comprises a plurality of first feed holes, a plurality of spring seals that seal against a transition duct, a cooling ring having a plurality of second feed holes, that with the first feed holes pass a cooling fluid into an annulus formed between the cooling ring and combustion liner. The cooling fluid passes over a means for augmenting the heat transfer proximate the combustion liner second end, wherein the heat transfer augmentation preferably comprises a plurality of raised ridges that increases the surface area of the outer liner wall to turbulate the cooling fluid and maximize the cooling effectiveness.
Public/Granted literature
- US20050262844A1 COMBUSTION LINER SEAL WITH HEAT TRANSFER AUGMENTATION Public/Granted day:2005-12-01
Information query
IPC分类: