ROTOR SPEED INDICATION SYSTEMS FOR ROTORCRAFT

A rotor speed indication system configured to communicate a rotor speed operating range for a twin engine rotorcraft (10) having a rotor (12) during one engine inoperable conditions. The rotor speed indication system includes a governing reference indicator (70) located on a display (40) and configu...

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Bibliographische Detailangaben
Hauptverfasser:	HALVERSON, Aaron Thomas, OLTHETEN, Erik John
Format:	Patent
Sprache:	eng ; fre ; ger
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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