Invention Grant
US07673454B2 Combustor of gas turbine and combustion control method for gas turbine
有权
燃气轮机燃烧器及燃气轮机燃烧控制方法
- Patent Title: Combustor of gas turbine and combustion control method for gas turbine
- Patent Title (中): 燃气轮机燃烧器及燃气轮机燃烧控制方法
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Application No.: US11700214Application Date: 2007-01-31
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Publication No.: US07673454B2Publication Date: 2010-03-09
- Inventor: Keijiro Saito , Satoshi Tanimura , Atsushi Yuasa , Toshihiko Saito
- Applicant: Keijiro Saito , Satoshi Tanimura , Atsushi Yuasa , Toshihiko Saito
- Applicant Address: JP Tokyo
- Assignee: Mitsubishi Heavy Industries, Ltd.
- Current Assignee: Mitsubishi Heavy Industries, Ltd.
- Current Assignee Address: JP Tokyo
- Agency: Birch, Stewart, Kolasch & Birch, LLP
- Priority: JP2006-093166 20060330
- Main IPC: F02C3/00
- IPC: F02C3/00

Abstract:
In a combustor, divisional fluid passages of a first group, and divisional fluid passages of a second group are present on an inner peripheral side, and divisional fluid passages are also present on an outer peripheral side, and swirl air flows are gushed from the divisional fluid passages. When the total amount of fuel supplied to the combustor is small as in a speed increasing state or in a low load state, fuel is injected only into the divisional fluid passages of the first group. Since a fuel injection region is limited to a position on the inner peripheral side, particularly, a specific position, the concentration of a fuel gas comprising a mixture of fuel and air is lean, but is higher than a flammability limit concentration, even when the total amount of fuel is small.
Public/Granted literature
- US20070227156A1 Combustor of gas turbine and combustion control method for gas turbine Public/Granted day:2007-10-04
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