公开(公告)号：WO1993018494A1

公开(公告)日：1993-09-16

申请号：PCT/US1993002137

申请日：1993-03-10

Applicant: THE BOEING COMPANY

Inventor： THE BOEING COMPANY ,  BROUDY, Robert, Malcolm ,  GOLDSTICK, Edward, Charles ,  HOLM, David, Allen ,  HOLT, Federick, B. ,  IVERSON, Alan, Neil ,  RIEMER, Dietrich, E. ,  TYLEE, James, Louis

IPC: G08B17/12

CPC classification number: G01J5/02 ,  G01J5/0205 ,  G01J5/025 ,  G01J5/026 ,  G01J5/08 ,  G01J5/0815 ,  G01J5/0821 ,  G01J5/0834 ,  G01J5/0862 ,  G01J5/0893 ,  G01J5/60 ,  G01J5/62 ,  G01J2005/068 ,  G08B17/12

Abstract: A thermal condition sensor system monitors equipment such as aircraft engines. The thermal condition sensor system includes a collector which collects radiation from the equipment and a detector assembly which detects collected radiation over a discriminating spectral band region in at least three spectral bands and generates signals representative of detected radiation in each spectral band. A processor receives the signals and generates a report of the thermal conditions of the equipment using interband comparison of the at least three spectral bands.

Abstract translation: 热状态传感器系统监视飞机发动机等设备。 热条件传感器系统包括收集来自设备的辐射的收集器和检测器组件，该检测器组件在至少三个光谱带中的识别光谱带区域上检测所收集的辐射，并产生表示每个光谱带中检测到的辐射的信号。 处理器接收信号并使用至少三个光谱带的区间比较来生成设备的热条件的报告。