Invention Grant
- Patent Title: Gas turbine combustor
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Application No.: US14577719Application Date: 2014-12-19
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Publication No.: US10197284B2Publication Date: 2019-02-05
- Inventor: Shinji Akamatsu , Hiroaki Kishida , Kenji Sato , Kentaro Tokuyama , Keisuke Matsuyama , Takayoshi Takashima
- Applicant: MITSUBISHI HEAVY INDUSTRIES, LTD.
- Applicant Address: JP Yokohama-shi
- Assignee: MITSUBISHI HITACHI POWER SYSTEMS, LTD.
- Current Assignee: MITSUBISHI HITACHI POWER SYSTEMS, LTD.
- Current Assignee Address: JP Yokohama-shi
- Agency: Westerman, Hattori, Daniels & Adrian, LLP
- Priority: JP2011-151310 20110707
- Main IPC: F23R3/42
- IPC: F23R3/42 ; F23R3/00 ; F23M20/00 ; F02C7/24

Abstract:
A gas turbine combustor is provided with a combustor basket where combustion gas flows, the combustion gas being produced by combustion of fuel injected from a nozzle, and a first resonance device and a second resonance device mounted on an outer surface of the combustor basket. The second resonance device is disposed on a downstream side from the first resonance device in a flow of the combustion gas and damps combustion oscillation of a frequency higher than the first resonance device. The first and second resonance devices are acoustic liners each having a housing mounted to the outer surface of the combustor basket. A resonance space surrounded by the housing and the outer surface of the combustor basket communicates with an interior space of the combustor basket via a plurality of acoustic holes formed in the combustor basket.
Public/Granted literature
- US20150101343A1 GAS TURBINE COMBUSTOR Public/Granted day:2015-04-16
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