发明名称 Thermocouple for measuring the temperature of an aircraft braking component incorporates a temperature compensation thermistor in the thermocouple housing thus reducing the overall weight of the temperature sensor
摘要 Thermocouple for an aircraft braking system has first and second temperature elements (20, 22) in chromel and alumel and a protective housing (16) for the thermocouple (14). The housing has a connector (18) with terminals (34, 36) to which copper connectors are connected. A temperature compensation thermistor (40) is arranged between one of the thermocouple elements and its corresponding connector and is contained within the housing. The invention also relates to a corresponding temperature measurement device and an aircraft braking system.
申请公布号 FR2831268(A1) 申请公布日期 2003.04.25
申请号 FR20010013467 申请日期 2001.10.18
申请人 LABINAL 发明人 BALLARINI PIERRE
分类号 G01K7/10;G01K7/13;(IPC1-7):G01K7/10;B64C25/42 主分类号 G01K7/10
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