Patent ID: 11946811
Assignee: PRATT & WHITNEY CANADA CORP.
Field: Measurement (Instruments)
Classification: CPC G  F | IPC F  G

Claim 0:
1. An assembly for a turbine engine, comprising:
a turbine engine structure; and
a sensor system including a probe and an optical sensor;
the probe connected to the turbine engine structure and projecting into a gas path of the turbine engine, the probe including a tubular sidewall and an endwall, the tubular sidewall projecting into the gas path from the turbine engine structure to the endwall, the endwall connected to the tubular sidewall, and the endwall comprising an opaque material; and
the sensor system configured to measure a temperature of the opaque material using the optical sensor;
wherein the optical sensor has a straight line-of-sight from the optical sensor to the opaque material.