VORTEX GENERATOR ARRANGEMENT FOR AN AIRCRAFT, and aircraft

A vortex generator arrangement (115) comprises a section (405) that defines an opening (421) to a corresponding cavity (423), an aircraft airflow modification device (301) disposed within the cavity (423), and at least one fluidic muscle actuator arrangement (801) coupled to the airflow modification...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	STEFES BRUNO
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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