Solid state flight deck panels and components thereof

The present invention provides for a systems control panel comprising: a front plate; a front PWA spaced a predetermined uniform distance from the front plate; and a plurality of systems control devices including one or more of switches, rheostats and annunciators mounted on the front plate and fron...

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Bibliographische Detailangaben
Hauptverfasser:	BOHLANDER, RICHARD A, FRASER, CHARLES R, METZGER, ROBERT W, LE, TOAN D, SCHATZ, RICHARD M, HUGHLOCK, BARRIE W, EDWARDS, WAYNE A, OKAMOTO, MARSHALL T, SCHAEFFER, DWIGHT R
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BASIC ELECTRIC ELEMENTS BASIC ELECTRONIC CIRCUITRY CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS COSMONAUTICS ELECTRIC SWITCHES ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR ELECTRICITY EMERGENCY PROTECTIVE DEVICES EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS PARACHUTES PERFORMING OPERATIONS PRINTED CIRCUITS PULSE TECHNIQUE RELAYS SELECTORS TRANSPORTING
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Beschreibung
Zusammenfassung:	The present invention provides for a systems control panel comprising: a front plate; a front PWA spaced a predetermined uniform distance from the front plate; and a plurality of systems control devices including one or more of switches, rheostats and annunciators mounted on the front plate and front PWA, the front PWA having circuitry for the systems control devices, and each of the systems control devices having solid state elements mounted on the PWA and interacting with the circuitry thereof.