Aerodynamische Verkleidung für ein Flugzeugfahrwerk

The device (1) has a housing closing unit (4) adapted to occupy, under action of actuating cylinders, a position of masking, with respect to streamlined flow, a part of a landing gear in released position. The closing unit has two front flaps (4a, 4b) movable under the action of the cylinders, betwe...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	FORT, FREDERIC
Format:	Patent
Sprache:	ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
Online-Zugang:	Volltext bestellen
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