INTEGRATED CAPACITIVE DISCHARGE ELECTRICAL BONDING ASSURANCE SYSTEM

In one embodiment, an aircraft electronics system (300) includes a hardware processor (304), a charge collection circuit (402) to collect charge; a switching circuit (404) controlled by the hardware processor (304) to discharge the charge collected on the charge collection circuit (402) through a bo...

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Bibliographische Detailangaben
1. Verfasser:	FROMAN, Gary S
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CONVERSION OR DISTRIBUTION OF ELECTRIC POWER COSMONAUTICS ELECTRICITY EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERATION MEASURING MEASURING ELECTRIC VARIABLES MEASURING MAGNETIC VARIABLES PARACHUTES PERFORMING OPERATIONS PHYSICS TESTING TRANSPORTING
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Beschreibung
Zusammenfassung:	In one embodiment, an aircraft electronics system (300) includes a hardware processor (304), a charge collection circuit (402) to collect charge; a switching circuit (404) controlled by the hardware processor (304) to discharge the charge collected on the charge collection circuit (402) through a bonding circuit (310) formed from a chassis (302) and a bonding surface; and a voltage measurement circuit (408) to measure a voltage difference between measurement terminals (406) across the chassis (302) and the bonding surface.