AIR46B: The Preparation and Use of Chromel-Alumel Thermocouples for Aircraft Gas Turbine Engines - Information Report

Features

Issuing Committee: E-32 Aerospace Propulsion Systems Health Management

Scope

Content: 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.

Meta Tags

Topics: Aircraft propulsion systems
Vehicle health management (VHM)
Gas turbines
Jet engines
Turbojet engines
Turboprop engines

Details

DOI: https://doi.org/10.4271/AIR46B

Pages: 54

Citation: SAE International Information Report, The Preparation and Use of Chromel-Alumel Thermocouples for Aircraft Gas Turbine Engines, SAE Standard AIR46B, Reaffirmed May 2014, Revised November 1996, Issued March 1956, https://doi.org/10.4271/AIR46B.

Additional Details

Publisher: SAE International

Published: May 1, 2014

Product Code: AIR46B

Content Type: Information Report

Status: Reaffirmed

Language: English

Historical