Dual gain digital engine control

An engine control system (101) having an engine (105), a digital engine control (103), and a gain logic (115) disposed within the digital engine control (0103) for use with an aircraft. The digital engine control (103) is configured to receive and process inputs from systems within the aircraft. Gai...

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Bibliographische Detailangaben
1. Verfasser:	MCCOLLOUGH, JAMES M
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES CONTROLLING CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	An engine control system (101) having an engine (105), a digital engine control (103), and a gain logic (115) disposed within the digital engine control (0103) for use with an aircraft. The digital engine control (103) is configured to receive and process inputs from systems within the aircraft. Gain logic (115) uses the inputs to generate command data to regulate the performance of the engine (105) so as to allow rotor speed deviations from a set point.