发明名称 GAS TURBINE OPTICAL IMAGING SYSTEM
摘要 <p><P>PROBLEM TO BE SOLVED: To provide a method and a system for reproducing a two-dimensional distribution of temperatures in an exhaust plane of a gas turbine engine (10). <P>SOLUTION: Light transmission (52) and detection (54) pairs may be arranged in the annulus of the exhaust (16) of the turbine engine (10) in such a way that individual rays form a two-dimensional mesh (70) of beams across a sector of the exhaust (16). Based on the absorption of the rays, the temperature of the sector of the exhaust (16) through which the ray passes may be determined. Based on the determination, an image that corresponds to the operation of the turbine engine (10) may be generated. <P>COPYRIGHT: (C)2011,JPO&INPIT</p>
申请公布号 JP2010255635(A) 申请公布日期 2010.11.11
申请号 JP20100098360 申请日期 2010.04.22
申请人 GENERAL ELECTRIC CO <GE> 发明人 WOODMANSEE MARK ALLEN;BASU SAMIT KUMAR;YARAM VIJAY KUMAR;CHEN WEIGUO;GU YIKANG;HINCKLEY KEVIN MICHAEL
分类号 F02C9/00;F01D25/00;G01K11/12;G01N21/35;G01N21/61 主分类号 F02C9/00
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