INTELLIGENT INTEGRATED PROPULSION CONTROL SYSTEM AND METHOD

Control systems and methods for an aircraft propulsion system are disclosed in which the propulsion control system (140) is integrated to intelligently control aircraft propulsion and minimize transient effects from the power demands of other aircraft subsystems (120, 130, 152) La présente invention...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	BURNS, DONALD, W, ZELLER, ROBERT, J
Format:	Patent
Sprache:	eng ; fre
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
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	Control systems and methods for an aircraft propulsion system are disclosed in which the propulsion control system (140) is integrated to intelligently control aircraft propulsion and minimize transient effects from the power demands of other aircraft subsystems (120, 130, 152) La présente invention se rapporte à des systèmes et à des procédés de commande destinés à un système de propulsion d'aéronef dans lesquels le système de commande de propulsion (140) est intégré pour commander intelligemment la propulsion de l'aéronef et pour réduire au minimum les effets de transition issues des demandes d'énergie d'autres sous-systèmes d'aéronef (120, 130, 152).