发明名称 METHOD AND APPARATUS FOR A FAULT TOLERANT CLOCK WITH DYNAMIC RECONFIGURATION
摘要 A fail-operational/fail-operational fault tolerant clock includes a voting core comprised of triple redundant clock modules (30, 40, 50) and a floating hot spare module (60). Each module includes a voter (84) and fault detection, identification and reconfiguration circuitry (82) which operates to substitute the floating hot spare module produced clock signal for a failed voting core module signal without the introduction of transients or an asynchronous voted output. The modules (30, 40, 50, 60) are all preferably formed on a single semiconductor chip which includes isolation guard rings (32, 42, 52, 62) and independent power leads (34, 44, 54, 64) in addition to isolation buffering and point-to-point wiring to enhance fault torelance.
申请公布号 WO9611439(A1) 申请公布日期 1996.04.18
申请号 WO1995US09321 申请日期 1995.07.20
申请人 THE BOEING COMPANY 发明人 TRUONG, TUONG, KIEN
分类号 G06F11/18;G06F11/20;(IPC1-7):G06F11/18;G06F11/16 主分类号 G06F11/18
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