发明名称 Gas turbine jet engine.
摘要 <p>Normal high load operation automatically varies nozzle area to maintain an optimum engine pressure ratio (EPR). An error signal representing fan damage is established by comparing the actual EPR to the predicted EPR. Compressor stalls are also monitored. In response to these signals a minimum nozzle area is set and modified. Automatic operation to hold EPR and afterburning is inhibited. Further signals representing satisfactory operation may reset the inhibiting action.</p>
申请公布号 EP0385912(A2) 申请公布日期 1990.09.05
申请号 EP19900630019 申请日期 1990.01.18
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 PATTERSON, GREGORY S.;KELLY, JAMES B.
分类号 F02K1/16 主分类号 F02K1/16
代理机构 代理人
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