PULSE MODULATION TECHNIQUE FOR GAS TURBINE ENGINES

Various implementations described herein are related to an aircraft (100) having a multi-engine configuration with multiple engines. The aircraft (100) may have a flight control system (210) coupled to the multiple engines (224A, 224B) with a multi-engine interface (220). The flight control system (...

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Bibliographische Detailangaben
Hauptverfasser:	Parson, Thomas, Emrich, Joshua
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 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 TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	Various implementations described herein are related to an aircraft (100) having a multi-engine configuration with multiple engines. The aircraft (100) may have a flight control system (210) coupled to the multiple engines (224A, 224B) with a multi-engine interface (220). The flight control system (210) may be configured to reduce fuel consumption of at least one engine of the multiple engines (224A, 224B) during reduced-engine operation by pulse modulating fuel delivery to the at least one engine of the multiple engines.