A New Autocalibration Procedure in Intelligent Temperature Transducer

2019 ◽  
Vol 68 (3) ◽  
pp. 895-902
Author(s):  
Wieslaw Miczulski ◽  
Mariusz Krajewski ◽  
Sergiusz Sienkowski
Keyword(s):  
Temperature Transducer

Comments on “Development of an Intelligent Temperature Transducer”

2019 ◽  
Vol 19 (12) ◽  
pp. 4734-4736 ◽  
Author(s):  
Tapan Prasad ◽  
Kanwar Pal Singh Rana ◽  
Vineet Kumar
Keyword(s):  
Temperature Transducer

Calculation of the characteristics of an electromagnetic temperature transducer

1997 ◽  
Vol 40 (1) ◽  
pp. 79-84
Author(s):  
V. V. Sebko ◽  
I. V. Mashneva ◽  
O. L. Bagmet ◽  
I. I. Moskalenko
Keyword(s):  
Temperature Transducer

Sapphire high-Q low temperature transducer for resonant bar gravitational wave antennas

1996 ◽  
Vol 211 (3) ◽  
pp. 139-142 ◽  
Author(s):  
I.A. Bilenko ◽  
E.N. Ivanov ◽  
M.E. Tobar ◽  
D.G. Blair
Keyword(s):  
Low Temperature ◽  
Gravitational Wave ◽  
Temperature Transducer ◽  
High Q

scholarly journals Characteristic Curves of Iridium-Rhodium Sensing Elements in High-Temperature Transducer Applications

2021 ◽  
Vol 7 (1) ◽  
pp. 62-67
Author(s):  
Vasyl Fedynets ◽  
◽  
Yaroslav Yusyk ◽  
Ihor Vasylkivskyi
Keyword(s):  
High Temperature ◽  
Gas Turbines ◽  
Internal Combustion Engines ◽  
High Reliability ◽  
Characteristic Curve ◽  
Individual Characteristic ◽  
General View ◽  
Temperature Transducer ◽  
Oxidizing Atmosphere ◽  
The Individual

In order to increase the capacity and efficiency factor of gas turbines and internal combustion engines while preserving their high reliability, the gas temperature and its distribution need to be measured in combustion chambers. Values of these temperatures can exceed 1800°С in an oxidizing atmosphere. Therefore, designing temperature transducers for measurements in such severe environments, special attention should be paid to the selection of thermometric materials. The requirements of the necessary accuracy and temperature range over 1800°С in an oxidizing atmosphere are fulfilled only by the temperature transducer based on iridium-rhodium alloys. The characteristic curve of such sensing elements is individual and each temperature transducer is to be calibrated. The paper discusses a technique of determining the individual characteristic curve of iridium-rhodium sensing elements of high-temperature transducers. The preparation steps to be taken prior to the calibration and the main stages of determining the characteristic curve are described. The general view of the experimental set for calibrating the sensing elements is presented. Based on the calibration results, the form of approximating polynomial of the individual characteristic curve is proposed.

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