发明名称 SYSTEM FOR SUPPLYING FUEL TO THE INJECTORS OF A TURBOSHAFT ENGINE
摘要 <p>A system for supplying fuel to a plurality of fuel injectors of a gas turbine engine is disclosed having first and second fuel distributors and a fuel transfer device which enables fuel to flow from the fuel source to the first and second fuel distributors as a function of the fuel flow rate. The fuel transfer device enables fuel to flow through the first fuel distributor under low fuel flow conditions. The first fuel distributor sequentially supplies fuel to each of a plurality of groups of fuel injectors when the fuel flow rate is below a predetermined threshold value. When the fuel flow exceeds a high threshold value, the fuel transfer device enables fuel to flow through the second fuel distributor which supplies fuel to all of the fuel injectors of the engine.</p>
申请公布号 GB9226298(D0) 申请公布日期 1993.02.10
申请号 GB19920026298 申请日期 1992.12.17
申请人 SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION S N E C M A 发明人
分类号 F02C7/22;F02C7/228;F02C9/26 主分类号 F02C7/22
代理机构 代理人
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