VORTEX GENERATOR ARRANGEMENT FOR AN AIRCRAFT, and aircraft

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

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Bibliographische Detailangaben
1. Verfasser: STEFES BRUNO
Format: Patent
Sprache:chi ; eng
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung: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 device (301). The invention also relates to an aircraft having the vortex generator arrangement. 本申请涉及一种旋涡发生器结构。该旋涡发生器结构(115)包括限定通向对应的腔室(423)的开口(421)的部分(405)、布置在腔室(423)内的飞行器气流改变装置(301)以及联接至气流改变装置(301)的至少一个流体肌肉致动器结构(801)。本申请还涉及一种包括所述涡旋发生器结构的飞行器。