FAULT DETECTION ASSEMBLY

A fault detection assembly (70) for an aircraft system (62) according to an example of the present disclosure includes, among other things, a transmitter (72) that communicates an electrical input signal to a first portion (82) of an electrical connector (80), the first portion (82) moveable between...

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Bibliographische Detailangaben
Hauptverfasser:	DARDONA, Sameh, TOKGOZ, Cagatay
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING FUNCTIONAL ELEMENTS OF SUCH SYSTEMS MEASURING MEASURING ELECTRIC VARIABLES MEASURING MAGNETIC VARIABLES MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PHYSICS REGULATING TESTING
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Beschreibung
Zusammenfassung:	A fault detection assembly (70) for an aircraft system (62) according to an example of the present disclosure includes, among other things, a transmitter (72) that communicates an electrical input signal to a first portion (82) of an electrical connector (80), the first portion (82) moveable between a fully seated position and a fully unseated position relative to a second portion (84) of the electrical connector (80) to define a range of insertion depths, a receiver (74) that senses an electrical output signal relating to the electrical input signal, and a comparison module (76) that determines an insertion depth (D) in the range of insertion depths based on a change in a resonant frequency of the electrical output signal with respect to the electrical input signal.