Turbine engine exhaust gas temperature sensor

The invention relates to a turbine engine exhaust gas temperature sensor. A gas turbine engine may include a compressor section, a combustor section, and a turbine section in a serial flow arrangement, where the combustor section has a combustion chamber defining an exhaust gas flow path through which combustion exhaust gas flows. An exhaust gas temperature sensor is located at least partially within the exhaust gas flow path. The housing defines an interior, the spring is located within the interior, and the temperature probe extends through the interior and is thermally coupled to the exhaust gas flow path. A spring biases the probe housing of the probe against the housing. 本发明涉及涡轮发动机排出气体温度传感器。一种燃气涡轮发动机可包括成串行流布置的压缩机区段、燃烧器区段和涡轮区段，其中燃烧器区段具有燃烧室，燃烧室限定排出气体流动路径，燃烧排出气体流动通过排出气体流动路径。排出气体温度传感器至少部分地位于排出气体流动路径内。外壳界定内部，弹簧位于内部内，并且温度探头延伸通过内部并热联接到排出气体流动路径。弹簧将探头的探头壳体抵靠外壳偏压。