发明名称 Apparatus for fuel injection in a turbine engine
摘要 <p>In one embodiment, a system (10) includes a fuel nozzle (12) that includes a fuel injector (61, 70) configured to output a fuel flow and a premixer tube (52) disposed about the fuel flow output from the fuel injector (61, 70). The premixer tube (52) includes a perforated portion (74) and a non-perforated portion (76), and the non-perforated portion (76) is downstream of the perforated portion (74).</p>
申请公布号 EP2213944(A2) 申请公布日期 2010.08.04
申请号 EP20100152191 申请日期 2010.01.29
申请人 GENERAL ELECTRIC COMPANY 发明人 BOARDMAN, GREGORY ALLEN;MELTON, PATRICK BENEDICT;SIMU, CHRISTINE ELAINE
分类号 F23R3/28 主分类号 F23R3/28
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