SYSTEME POUR LA FOURNITURE D'ESTIMATIONS DE PARAMETRES DE VOL D'UN AERONEF INDEPENDANTES ET DISSIMILAIRES ET AERONEF ASSOCIE

The system has multiple measurement probes including an aerial part (24) to provide physical size that is correlated to flight parameters and different from static pressure. The measurement probes and static pressure taps (281-1, 281-2, 282-1, 282-2, 283-1, 283-2) are connected with each other to fo...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	COLLIAU FLORENT, FLAVEN CEDRIC, JAULAIN YVES
Format:	Patent
Sprache:	fre
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT MEASURING MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION,OR SHOCK PARACHUTES PERFORMING OPERATIONS PHYSICS TESTING TRANSPORTING
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	The system has multiple measurement probes including an aerial part (24) to provide physical size that is correlated to flight parameters and different from static pressure. The measurement probes and static pressure taps (281-1, 281-2, 282-1, 282-2, 283-1, 283-2) are connected with each other to form three data systems (SA-SC) that are connected with the static pressure taps. The static pressure tap of each data system is separated from the static pressure tap of the other data systems.