SAE AIR 46C:2022-09-14

SAE AIR 46C:2022-09-14

The Preparation and Use of Thermocouples for Aircraft Gas Turbine Engines

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Details

This SAE Aerospace Information Report (AIR) reviews the precautions that must be taken and the corrections which must be evaluated and applied if the experimental error in measuring the temperature of a hot gas stream with a thermocouple is to be kept to a practicable minimum. Discussions will focus on Type K thermocouples, as defined in National Institute of Standards and Technology (NIST) Monograph 175 as Type K, nickel-chromium (Kp) alloy versus nickel-aluminium (Kn) alloy (or nickel-silicon alloy) thermocouples. However, the majority of the content is relevant to any thermocouple type used in gas turbine applications.

Additional Info

Author Society of Automotive Engineers International (SAE)
Committee E-32 Aerospace Propulsion Systems Health Management
Published by SAE
Document type Standard
ICS 49.050 : Aerospace engines and propulsion systems
Number of pages 49
Replace SAE AIR 46B:2014-05-01
Document history SAE AIR 46B:2014-05-01,SAE AIR 46A:1996-11-01,SAE AIR 46:1956-03-01
Keyword SAE 46,SAE AIR46C,SAE AIR46C,SAE AIR 46