Temperature and pressure measurement techniques for an advanced turbine test facility
Abstract
A high pressure, high-temperature turbine test facility constructed for use in turbine cooling research is described. Several recently developed temperature and pressure measuring techniques are used in this facility. The measurement techniques, their status, previous applications and some results are discussed. Noncontact surface temperature measurements are made by optical methods. Radiation pyrometry principles combined with photoelectric scanning are used for rotating components and infrared photography for stationary components. Contact (direct) temperature and pressure measurements on rotating components are expected to be handled with an 80 channel rotary data package which mounts on and rotates with the turbine shaft at speeds up to 17,500 rpm. The data channels are time-division multiplexed and converted to digital words in the data package. A rotary transformer couples power and digital data to and from the shaft.
- Publication:
-
NASA STI/Recon Technical Report N
- Pub Date:
- 1980
- Bibcode:
- 1980STIN...8014374P
- Keywords:
-
- Gas Turbine Engines;
- Pressure;
- Rotating Bodies;
- Temperature Measurement;
- Test Facilities;
- Digital Data;
- Infrared Photography;
- Optical Measurement;
- Pyrometers;
- Time Division Multiplexing;
- Instrumentation and Photography