发明名称 |
CONTROL METHOD OF GAS-TURBINE ENGINE WITH AFTERBURNER, AND SYSTEM USED FOR ITS IMPLEMENTATION |
摘要 |
FIELD: engines and pumps. ^ SUBSTANCE: control of gas-turbine engine (GTE) with afterburner is performed as per one of three control loops; individual control programme is specified on each loop and corrected as per certain group of sensors the readings of which are the most essential for operation exactly in that mode. ^ EFFECT: invention allows improving operating reliability and safety of GTE with afterburner of airborne vehicle due to reducing the time of augmented and full acceleration of GTE and expansion of safe startup area of afterburner, and providing GTE operation in wide range in optimum modes. ^ 2 cl, 1 dwg |
申请公布号 |
RU2466287(C1) |
申请公布日期 |
2012.11.10 |
申请号 |
RU20110119911 |
申请日期 |
2011.05.19 |
申请人 |
OTKRYTOE AKTSIONERNOE OBSHCHESTVO "NAUCHNO-PROIZVODSTVENNOE OB"EDINENIE "SATURN" (OAO "NPO "SATURN") |
发明人 |
BONDAREV LEONID JAKOVLEVICH;ZELIKIN JURIJ MARKOVICH;KONDRATOV ALEKSANDR ANATOL'EVICH;KOROLEV VIKTOR VLADIMIROVICH;MARCHUKOV EVGENIJ JUVENAL'EVICH;FEDJUKIN VLADIMIR IVANOVICH |
分类号 |
F02C9/28 |
主分类号 |
F02C9/28 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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