发明名称 ADDITIVELY MANUFACTURED NOZZLE TIP FOR FUEL INJECTOR
摘要 A fuel injector for a gas turbine engine is disclosed that includes a nozzle tip assembly having a nozzle body substantially monolithically formed by additive manufacturing and having at least one fuel circuit defined therein and at least one air circuit defined therein.
申请公布号 US2014367494(A1) 申请公布日期 2014.12.18
申请号 US201313918437 申请日期 2013.06.14
申请人 Delavan Inc 发明人 Donovan Matthew Raymond
分类号 F23R3/36 主分类号 F23R3/36
代理机构 代理人
主权项 1. A fuel injector for a gas turbine engine comprising: a nozzle tip assembly including a nozzle body substantially monolithically formed by additive manufacturing and having at least one fuel circuit defined therein and at least one air circuit defined therein.
地址 West Des Moines IA US