SYSTEM FOR REAL-TIME SIMULATION OF THE ENVIRONMENT OF AN AIRCRAFT ENGINE

The disclosed system (SYS1) comprises a digital computer (FAD1), the inputs of which a selection module (MSEL1) directs to a sensor (CAPi) or to a substitute digital bus (BSU1) on which substitute digital data (DSUi) generated by a real-time simulator (SIM) can transit. Ce système (SYS1) comporte un...

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Bibliographische Detailangaben
Hauptverfasser:	EVRA, YANNICK, PY, JEAN MICHEL, RUPERT, PASCAL
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AEROPLANES AIRCRAFT AVIATION CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR FUNCTIONAL ELEMENTS OF SUCH SYSTEMS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HELICOPTERS MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PERFORMING OPERATIONS PHYSICS REGULATING TRANSPORTING
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Beschreibung
Zusammenfassung:	The disclosed system (SYS1) comprises a digital computer (FAD1), the inputs of which a selection module (MSEL1) directs to a sensor (CAPi) or to a substitute digital bus (BSU1) on which substitute digital data (DSUi) generated by a real-time simulator (SIM) can transit. Ce système (SYS1) comporte un calculateur numérique (FAD1) dont les entrées sont aiguillées par un module de sélection (MSEL1) embarqué dans le calculateur (FAD1) soit vers un capteur (CAPi) soit vers un bus numérique de substitution (BSU1) sur lequel peuvent transiter des données numériques (DSUi) de substitution générées par un simulateur temps réel (SIM).