发明名称 Gas turbine fuel regulator system - has electromagnetic valve excited by combined outputs of two compressors
摘要 <p>The fuel feed is varied by an air pressure signal taken from a first and a second compressor connection (21, 22). The connections are joined by a restrictor (23) and a venturi (24) in series. A bellows (18) is subjected to pressure from the second compressor connection (P3) and a second bellows (19) is subject to a vacuum. A second venturi (25) is connected between the first venturi and the restrictor on its outlet side. The electro magnetic valve is excited by the compressor values to decrease the fuel flow. Stops (29, 30) form upper and lower (acceleration and retard) fuel flow limit values.</p>
申请公布号 FR2349737(A1) 申请公布日期 1977.11.25
申请号 FR19770012033 申请日期 1977.04.21
申请人 LUCAS INDUSTRIES LTD 发明人
分类号 F02C9/38;F02C9/32;(IPC1-7):02C9/04 主分类号 F02C9/38
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