タイトル | Temperature and pressure measurement techniques for an advanced turbine test facility |
本文(外部サイト) | http://hdl.handle.net/2060/19800006117 |
著者(英) | Pollack, F. G.; Cochran, R. P. |
著者所属(英) | NASA Lewis Research Center |
発行日 | 1980-01-01 |
言語 | eng |
内容記述 | 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. |
NASA分類 | INSTRUMENTATION AND PHOTOGRAPHY |
レポートNO | 80N14374 E-212 NASA-TM-79278 |
権利 | No Copyright |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/173842 |