MONITORING DEVICE FOR DIFFERENTIAL TRANSFORMER SENSORS IN AN AIRCRAFT AND METHOD

A monitoring device for differential transformer sensors in an aircraft includes a first sensor interface which can be coupled with a first differential transformer sensor, a second sensor interface which can be coupled with a second differential transformer sensor, a calculation apparatus which is...

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Bibliographische Detailangaben
Hauptverfasser:	LUECKER JAN, GALINSKI MIKE
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVEREDIN A SINGLE OTHER SUBCLASS ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS MEASURING MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR PARACHUTES PERFORMING OPERATIONS PHYSICS TARIFF METERING APPARATUS TESTING TRANSPORTING
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Beschreibung
Zusammenfassung:	A monitoring device for differential transformer sensors in an aircraft includes a first sensor interface which can be coupled with a first differential transformer sensor, a second sensor interface which can be coupled with a second differential transformer sensor, a calculation apparatus which is coupled with the first sensor interface and the second sensor interface and is designed to detect and output first measurement values from a first differential transformer sensor which is coupled with the first sensor interface and second measurement values from a second differential transformer sensor which is coupled with the second sensor interface, and having a display device which is designed to display the detected first measurement values and the detected second measurement values separately or together.