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특허 상세정보

Modular resonators for suppressing combustion instabilities in gas turbine power plants

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-007/24   
미국특허분류(USC) 060/725; 431/114; 181/213
출원번호 US-0667409 (2000-09-21)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 54  인용 특허 : 7
초록

A resonator module for a combustion turbine power plant, where the combustion turbine power plant defines a flow path. The resonator module includes a first member, an a second member. The first member has a size substantially smaller than the diameter of said flow path and a plurality of openings therethrough. The openings are in fluid communication with the flow path. The second member has a size generally equal to said first member. The second member is in a generally spaced relation to the first member and encloses a volume of gas between the first a...

대표
청구항

1. A resonator module in combination with a combustion turbine power plant, wherein said combustion turbine power plant has a compressor assembly, a combustor assembly, a turbine assembly, and a transition section between said combustor assembly and said turbine assembly which define a flow path, said resonator module comprising: a first member having a size substantially smaller than the diameter of said flow path and a plurality of openings therethrough; a second member maintained in a generally spaced relation to said first member and defining a v...

이 특허를 인용한 특허 피인용횟수: 54

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