发明名称 FUEL NOZZLE
摘要 <p><P>PROBLEM TO BE SOLVED: To provide a fuel nozzle preventing decline in combustion efficiency due to adhesion of fuel to a pilot flare of a staging type fuel nozzle, generation of smoke, deterioration of a dilution limit and decline in combustion efficiency due to mixing of air fuel mixture of fuel and air of a pilot fuel injection part and air passed through a main fuel injection part. <P>SOLUTION: In the fuel nozzle, a gas flow passage annuarly surrounding the fuel injection part is formed by a throat part and a flow passage area expansion part located downstream of the throat part. A space between the throat part and the flare is formed to have a recessed shape like a step in which the flow passage area is rapidly expanded, and a recirculating air flow is formed in the recessed region. <P>COPYRIGHT: (C)2011,JPO&INPIT</p>
申请公布号 JP2010281513(A) 申请公布日期 2010.12.16
申请号 JP20090135645 申请日期 2009.06.05
申请人 JAPAN AEROSPACE EXPLORATION AGENCY 发明人 YAMAMOTO TAKESHI;SHIMODAIRA KAZUO;MATSUURA KAZUAKI;KUROSAWA YOJI;YOSHIDA SEIJI
分类号 F23R3/16;F02C7/00;F02C7/22;F23R3/14;F23R3/20 主分类号 F23R3/16
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