发明名称 Oxygen sensor heater regulation unit for aircraft engine
摘要 The heater regulation device, for an oxygen sensor, has an oxygen sensor (26) with a sensor element (34) which yields the oxygen concentration in the fluid flow. This has a heater (33) for warming the sensor element. The impedance of the sensor element (34) is received by a holding device. A heater regulation device (105), which is based on a negative feedback circuit, maintains the impedance of the sensor (33) at a nominal value by regulation of the energy supplied to the heater element. A further device detects any variation of the sensor (33) which leads to an increase of its internal impedance, and this is coupled with a device that modifies the nominal impedance value maintained by the feedback circuit.
申请公布号 DE19729350(A1) 申请公布日期 1998.01.15
申请号 DE19971029350 申请日期 1997.07.09
申请人 DENSO CORP., KARIYA, AICHI, JP 发明人 YAMASHITA, YUKIHIRO, KARIYA, AICHI, JP;IIDA, HISASHI, KARIYA, AICHI, JP;HASEGAWA, JUN, KARIYA, AICHI, JP
分类号 F02D41/14;G01N27/406;(IPC1-7):G01N27/02;F02D45/00 主分类号 F02D41/14
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