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Utilizing a diluent to lower combustion instabilities in a gas turbine engine

机译：利用稀释剂降低燃气涡轮发动机的燃烧不稳定性

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摘要

A method of influencing combustion dynamics, including measuring a combustion dynamics parameter, and controlling a diluent flow (26) delivered to a fuel flow (32) upstream of a pilot burner fuel outlet (40) in response to the measured combustion dynamics parameter.

机译：一种影响燃烧动力学的方法，包括测量燃烧动力学参数和控制在引燃燃烧器燃料上游输送到燃料流（ 32 ）的稀释剂流（ 26 ）出口（ 40 ）响应测量的燃烧动力学参数。 展开▼

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公开/公告号US9017064B2

专利类型

公开/公告日2015-04-28

原文格式PDF

申请/专利权人 SAMER P. WASIF;
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申请/专利号US20100795786

发明设计人 SAMER P. WASIF;
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申请日2010-06-08

分类号F02C3/30;F23R3/28;F23N1/08;F23N5/16;

国家 US

入库时间 2022-08-21 15:18:20

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1. 降低燃气涡轮发动机的风扇不稳定性的装置及方法 [P] . 中国专利： CN104011362B . 2017.10.20

2. 具有风扇可变面积喷嘴以降低风扇不稳定性的燃气涡轮发动机 [P] . 中国专利： CN104011362A . 2014-08-27

3. UTILIZING A DILUENT TO LOWER COMBUSTION INSTABILITIES IN A GAS TURBINE ENGINE [P] . 美国专利： US2011300491A1 . 2011-12-08

机译：利用稀释剂降低燃气轮机发动机的燃烧不稳定性

4. instabilities to the combustion in a combustion chamber; the combustion chamber of a gas turbine engine according to this [P] . 法国专利： FR2961292B1 . 2014-01-31

机译：燃烧室内燃烧的不稳定性;根据此的燃气涡轮发动机的燃烧室

5. Method for reducing instabilities of combustion in combustion chamber in gas turbine engine, involves adjusting distance of wall to create phase difference between acoustic wave and aerodynamic oscillation generated through spin part [P] . 法国专利： FR2961292A1 . 2011-12-16

机译：减少燃气涡轮发动机燃烧室中燃烧不稳定性的方法，包括调节壁的距离以在声波和通过旋转部分产生的空气动力学振荡之间产生相位差。

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