Invention Grant
- Patent Title: Gas turbine gaseous fuel injection system
- Patent Title (中): 燃气轮机气体燃料喷射系统
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Application No.: US13358227Application Date: 2012-01-25
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Publication No.: US09027349B2Publication Date: 2015-05-12
- Inventor: Keisuke Miura , Tomomi Koganezawa , Satoshi Dodo , Takeo Saito
- Applicant: Keisuke Miura , Tomomi Koganezawa , Satoshi Dodo , Takeo Saito
- Applicant Address: JP Kanagawa
- Assignee: Mitsubishi Hitachi Power Systems, Ltd.
- Current Assignee: Mitsubishi Hitachi Power Systems, Ltd.
- Current Assignee Address: JP Kanagawa
- Agency: Crowell & Moring LLP
- Priority: JP2011-014682 20110127
- Main IPC: F02C1/00
- IPC: F02C1/00 ; F23R3/28

Abstract:
A combustor of the prior art that defines the outlet position and direction of an air hole and suppresses adhesion of flame to an air hole outlet can reduce a discharge amount of NOx by increasing a distance over which fuel and air are mixed with each other. However, such a combustor is not sufficiently discussed for measures to suppress the occurrence of combustion oscillation resulting from the variation of a flame surface.A combustor 2 according to the present invention includes a combustion chamber 5 to which fuel and air are supplied; air holes 32 adapted to supply air to the combustion chamber 5; fuel nozzles 25 adapted to supply gaseous fuel to the air holes 32; and orifices 24 adapted to allow the gaseous fuel supplied to the air holes 32 to cause a pressure drop.
Public/Granted literature
- US20120192568A1 Gas Turbine Combustor Public/Granted day:2012-08-02
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