SAE AS 414B:1996

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Temperature Instruments (Turbine Powered Subsonic Aircraft)

Published By	Publication Date	Number of Pages
SAE	1996-09-01	16

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Categories: 43.040.10 - Electrical and electronic equipment, 49 - Aircraft and space vehicle engineering, SAE

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Description

This SAE Aerospace Standard (AS) covers two basic types of temperature instruments as follows:

Type I:	Ratiometer type, actuated by changes in 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 EMF output of a thermocouple; the varying EMF input to the instrument being obtained by temperature changes of the temperature sensing thermocouple.

Additional information

Published Code	SAE
Published By	SAE International, formerly Society of Automotive Engineers
Publication Date	1996-09-01
Pages Count	16
Language	English
Descriptors	Pressure; Aircraft instruments; Humidity; Electronic equipment; Conductivity; Identification numbers; Drag; Aircraft; Performance tests
File Size	102.4 KB
ICS Codes	43.040.10 - Electrical and electronic equipment 49 - Aircraft and space vehicle engineering

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SAE AS 414B:1996

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