POWER DEMAND ANTICIPATION SYSTEMS FOR ROTORCRAFT

A power demand anticipation system (100) for a rotorcraft (102) includes an engine subsystem (112) having an engine (116) with a power output. The power demand anticipation system (100) also includes one or more sensors (108) including a cyclic control sensor (130). The one or more sensors (108) are...

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Bibliographische Detailangaben
Hauptverfasser:	COVINGTON, Charles Eric, SCHAEFFER, Joseph M, WORSHAM II, Robert Earl
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS FUNCTIONAL ELEMENTS OF SUCH SYSTEMS GAS-TURBINE PLANTS HEATING HELICOPTERS HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PARACHUTES PERFORMING OPERATIONS PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A power demand anticipation system (100) for a rotorcraft (102) includes an engine subsystem (112) having an engine (116) with a power output. The power demand anticipation system (100) also includes one or more sensors (108) including a cyclic control sensor (130). The one or more sensors (108) are operable to detect one or more flight parameters of the rotorcraft (102) to form sensor data (122) including a cyclic control position. A power demand anticipation module (104) is in data communication with the engine subsystem (112) and the one or more sensors (108). The power demand anticipation module (104) is operable to anticipate a power demand of the engine (116) using the sensor data (122) to form a power demand anticipation signal (126). The engine subsystem (112) is operable to adjust the power output of the engine (116) based on the power demand anticipation signal (126) received from the power demand anticipation module (104).