Burner
本发明涉及一种燃烧器(100),它带有一燃烧空气通道(104),其中按这样的方式设置一个由一定数量涡流发生器元件(108)构成的涡流发生器(109),即,通过涡流发生器(109)可使流过涡流发生器(109)的燃烧空气(112)的平均流速提高到至少0.4个马赫数。由此实现燃烧区与燃烧空气输入区的流动声学去耦。 The gas turbine burner (100) has a combustion air duct (104) in which are several spin-generating elements (108) forming spin-generators (109) in...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | 本发明涉及一种燃烧器(100),它带有一燃烧空气通道(104),其中按这样的方式设置一个由一定数量涡流发生器元件(108)构成的涡流发生器(109),即,通过涡流发生器(109)可使流过涡流发生器(109)的燃烧空气(112)的平均流速提高到至少0.4个马赫数。由此实现燃烧区与燃烧空气输入区的流动声学去耦。
The gas turbine burner (100) has a combustion air duct (104) in which are several spin-generating elements (108) forming spin-generators (109) in the form of spin blade rings. The ring consists of first (108A) and second (108B) blades. An extra pilot burner (106) stabilizes the mixture of fuel and combustion air emerging from the combustion air duct. |
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