发明名称 一体の共振器を持つ噴射器
摘要 <p>The system may include a turbine engine. The turbine engine may include a fuel nozzle. The fuel nozzle may include an air path. The fuel nozzle may also include a fuel path such that the fuel nozzle is in communication with a combustion zone of the turbine engine. Furthermore, the fuel nozzle may include a resonator. The resonator may be disposed in the fuel nozzle directly adjacent to the combustion zone.</p>
申请公布号 JP5709401(B2) 申请公布日期 2015.04.30
申请号 JP20100106063 申请日期 2010.05.06
申请人 发明人
分类号 F23R3/20;F02C7/22;F23R3/28 主分类号 F23R3/20
代理机构 代理人
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