发明名称 Fiber optic linked flame sensor
摘要 A fiber optic linked flame sensor for continuous optical monitoring of the combustion process within the combustion chamber of a gas turbine engine. The system includes a high temperature optical probe, a fiber optic cable, and electro-optics module. The high temperature probe is mounted on the engine skin and sighted in a manner so as to view the combustion process taking place at its origin just aft to the fuel nozzle. The appropriately constructed fiber optic cable connects the high temperature probe with the electro-optics module. The radiation transmitted via the fiber optic cable is then received by an ultraviolet photodiode located in the electro-optics module and coupled with appropriate electronics.
申请公布号 US5828797(A) 申请公布日期 1998.10.27
申请号 US19960666042 申请日期 1996.06.19
申请人 MEGGITT AVIONICS, INC. 发明人 MINOTT, GEORGE L.;PLIMPTON, JONATHAN C.
分类号 F01D17/02;F01D21/00;F23N5/08;G01J5/00;H05H1/00;(IPC1-7):G02B6/32 主分类号 F01D17/02
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