发明名称 DEVICE TO MEASURE GAS TURBINE BLADE TEMPERATURE
摘要 FIELD: radiation pyrometry. ^ SUBSTANCE: device incorporates a micro processor system and AD converter. The photoelectric converter output is connected to the AD converter input, in its turn, connected to the said micro processor system with a feedback with the AD converter. The eddy-current blade position pickup is also connected, via a rectangular pulse shaper, with the said micro processor system. ^ EFFECT: reducing the errors caused by unburnt fuel particle radiation to tolerable values. ^ 1 dwg
申请公布号 RU2332646(C1) 申请公布日期 2008.08.27
申请号 RU20070110289 申请日期 2007.03.20
申请人 GOSUDARSTVENNOE OBRAZOVATEL'NOE UCHREZHDENIE VYSSHEGO PROFESSIONAL'NOGO OBRAZOVANIJA UFIMSKIJ GOSUDARSTVENNYJ AVIATSIONNYJ TEKHNICHESKIJ UNIVERSITET 发明人 SKUDNOV EVGENIJ MIKHAJLOVICH;TOKAREV VLADIMIR PETROVICH
分类号 G01J5/14 主分类号 G01J5/14
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