Invention Grant
- Patent Title: Helmholtz resonator for a gas turbine combustion chamber
- Patent Title (中): 用于燃气轮机燃烧室的亥姆霍兹共振器
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Application No.: US13497091Application Date: 2010-09-14
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Publication No.: US08689933B2Publication Date: 2014-04-08
- Inventor: Ghenadie Bulat
- Applicant: Ghenadie Bulat
- Applicant Address: DE München
- Assignee: Siemens Aktiengesellschaft
- Current Assignee: Siemens Aktiengesellschaft
- Current Assignee Address: DE München
- Priority: EP09012116 20090923
- International Application: PCT/EP2010/063487 WO 20100914
- International Announcement: WO2011/036073 WO 20110331
- Main IPC: F01N1/12
- IPC: F01N1/12 ; F02C7/24 ; F02K1/00 ; F02K1/82

Abstract:
A resonator is provided, having an adaptable resonator frequency for absorbing sound generated by a gas stream of a gas turbine. The resonator includes a neck section, a chamber and a deformable element being deformable under influence of a change of a gas turbine temperature of the gas stream. The shape of the deformable element is predetermined with respect to a respective gas turbine temperature. The neck section and the chamber form a volume of the resonator. The neck section forms a passage coupling the volume with the gas turbine. The deformable element is thermally coupled to the gas turbine in such a way that the shape of the deformable element depends on the respective gas turbine temperature. The deformable element forms a spiral and is installed to the neck section in such a way that an effective diameter of the neck section depends on the gas turbine temperature.
Public/Granted literature
- US20120228050A1 HELMHOLTZ RESONATOR FOR A GAS TURBINE COMBUSTION CHAMBER Public/Granted day:2012-09-13
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