Invention Grant
- Patent Title: Cooling for combustor liners with accelerating channels
- Patent Title (中): 用于具有加速通道的燃烧器衬套的冷却
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Application No.: US13645016Application Date: 2012-10-04
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Publication No.: US09194585B2Publication Date: 2015-11-24
- Inventor: Frank J. Cunha , Timothy S. Snyder , Nurhak Erbas-Sen , Alexander W. Williams , Nicholas Mule , James P. Bangerter
- Applicant: United Technologies Corporation
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Miller, Matthias & Hull LLP
- Main IPC: F23R3/00
- IPC: F23R3/00 ; F23R3/06 ; F23R3/16 ; F02C7/18

Abstract:
A combustor liner which reduces cooling flow to a combustion chamber and augments pressure drop split between impingement holes and effusion holes is disclosed. The combustor liner may further include accelerating channels, trip strips, pedestals, and cone-shaped effusion holes to provide further cooling of the liner. The combustor liner may reduce NOx production and the temperature of the combustion chamber of a gas turbine engine or the like.
Public/Granted literature
- US20140096528A1 Cooling for Combustor Liners with Accelerating Channels Public/Granted day:2014-04-10
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