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특허 상세정보

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Controlled pilot oxidizer for a gas turbine combustor

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-009/00   
미국특허분류(USC) 060/794; 060/039.27
출원번호 UP-0173655 (2005-07-01)
등록번호 US-7752850 (2010-08-02)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 91  인용 특허 : 29
초록

A combustor (22) for a gas turbine (10) includes a main burner oxidizer flow path (34) delivering a first portion (32) of an oxidizer flow (e.g., 16) to a main burner (28) of the combustor and a pilot oxidizer flow path (38) delivering a second portion (36) of the oxidizer flow to a pilot (30) of the combustor. The combustor also includes a flow controller (42) disposed in the pilot oxidizer flow path for controlling an amount of the second portion delivered to the pilot.

대표
청구항
▼

We claim: 1. A combustor for a gas turbine comprising: a main burner oxidizer flow path delivering a first portion of an oxidizer flow to a main burner of a gas turbine combustor; a pilot oxidizer flow path delivering a second portion of the oxidizer flow to a pilot of the combustor; a flow controller disposed in the pilot oxidizer flow path for controlling an amount of the second portion delivered to the pilot; a pilot fuel flow for delivering fuel to the pilot; and a flow controller actuator controlling a position of the flow controller responsive to ...

이 특허에 인용된 특허 (29)

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이 특허를 인용한 특허 피인용횟수: 91

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