AS413A: TEMPERATURE INDICATOR - Technical Standard

Features

Issuing Committee: A-4 Aircraft Instruments Committee

Scope

Content

This Aeronautical Standard covers two basic types of temperature indicators as follows:

TYPE I	-	Ratiometer type actuated by changes of electrical resistance of a temperature sensing electrical resistance element; the resistance changes being obtained by temperature changes of the temperature sensing resistance element.
TYPE II	-	Millivoltmeter type, operated and actuated by varying e.m.f. output of a thermocouple, the varying e.m.f. input to the instrument being obtained by temperature changes of the temperature sensing thermocouple.

Meta Tags

Topics: Aircraft instruments
Conductivity
Humidity
Identification numbers
Drag
Pressure
Aircraft
Performance tests
Suppliers
Vehicle acceleration

Details

DOI: https://doi.org/10.4271/AS413A

Pages: 7

Citation: SAE International Technical Standard, TEMPERATURE INDICATOR, SAE Standard AS413A, Revised December 1954, Issued November 1948, https://doi.org/10.4271/AS413A.

Additional Details

Publisher: SAE International

Published: Dec 1, 1954

Product Code: AS413A

Content Type: Technical Standard

Status: Revised

Language: English

Historical