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. These are defined in NBS Monograph 125 as nickel-chromium alloy versus nickel-aluminum alloy thermocouples. AIR46B has been reaffirmed to comply with the SAE five-year review policy.
The Preparation and Use of Chromel-Alumel Thermocouples for Aircraft Gas Turbine Engines
2014-05-01
Aufsatz (Konferenz)
Englisch
THE PREPARATION AND USE OF CHROMEL-ALUMEL THERMOCOUPLES FOR AIRCRAFT GAS TURBINE ENGINES
SAE Technical Papers | 1996
THE PREPARATION AND USE OF CHROMEL-ALUMEL THERMOCOUPLES FOR TURBOJET ENGINES
SAE Technical Papers | 1956
The Preparation and Use of Thermocouples for Aircraft Gas Turbine Engines
SAE Technical Papers | 2022
Engineering Index Backfile | 1948
Control of aircraft turbine engines
Engineering Index Backfile | 1968
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