发明名称 FUEL-FEED REGULATOR OF GAS-TURBINE ENGINE
摘要 A fuel-feed regulator of gas-turbine engine includes centrifugal tachometer connected to air bleed valve installed in channel of air supply downstream of compressor, corrector separated by spring-loaded membrane into two cavities, Venturi tube connected to corrector, and dozing needle. Besides that there are included connected in sequence pressure sensor, amplification device and electric magnet, input of pressure sensor is connected to output of corrector, and output of electric magnet is connected to input of dozing needle.
申请公布号 UA35597(U) 申请公布日期 2008.09.25
申请号 UA20080005647U 申请日期 2008.04.30
申请人 M. ZHUKOVSKYI NATIONAL AERO-SPACE UNIVERSITY “KHARKIV AVIATION INSTITUTE” 发明人 PASICHNYK SERHII MYKOLAIOVYCH;BANDURA IVAN MYKOLAIOVYCH;CHUMAK TETIANA SERGIIVNA
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