发明名称 Fuel regulator for gas turbines - has environmental temperature dependant fuel rate flow correcture valve to move fuel line throttle
摘要 <p>Fuel is fed to the jects from a pump via a pipe system. The flow rate is determined by a regulator cross bore and fuel opening sizes of the fuel correcture slide valve as well as the pressure drop on the regulator and slide valves. The fuel pressure drop is held constant by the correcture valve. A temp. sensor responds to changes in the atmosphere air by displacing by a bellow, a sprung slide valve which correspondingly increases or decreases the slide valve opening cross sections to adjust the fuel flow rate to the jets.</p>
申请公布号 DE2552042(A1) 申请公布日期 1977.05.26
申请号 DE19752552042 申请日期 1975.11.20
申请人 DMITRIEV,VASILIJ PETROVITSCH;LUSCHIN,ANDREJ ALEXANDROVITSCH;POLYAKOV,ANATOLIJ MICHAILOVITSCH;TOMILIN,ALEXANDR GRIGORIEVITSCH;SCHUSCHPAN,STANISLAV MICHAILOVITSCH 发明人 PETROVITSCH DMITRIEV,VASILIJ;ALEXANDROVITSCH LUSCHIN,ANDREJ;MICHAILOVITSCH POLYAKOV,ANATOLIJ;GRIGORIEVITSCH TOMILIN,ALEXANDR;MICHAILOVITSCH SCHUSCHPAN,STANISLAV
分类号 F02C9/32;(IPC1-7):02C9/04 主分类号 F02C9/32
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