HUBSCHRAUBER

A helicopter includes missile supporting means movable from an operational position to a stowed position in which the missiles 17 are located within the confines of the helicopter fuselage. In one embodiment the missile supporting means is pivotally attached to the fuselage about a generally horizon...

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Bibliographische Detailangaben
Hauptverfasser:	ERNEST NORTH,HORACE, LEWIS COWDERY,ROY, VINCENT SMITH,RONALD
Format:	Patent
Sprache:	ger
Schlagworte:	AEROPLANES AIRCRAFT APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS ANDORDNANCE, e.g. CANNONS HARPOON GUNS HEATING HELICOPTERS LAUNCHERS FOR ROCKETS OR TORPEDOES LIGHTING MECHANICAL ENGINEERING MOUNTINGS FOR SMALLARMS OR ORDNANCE PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A helicopter includes missile supporting means movable from an operational position to a stowed position in which the missiles 17 are located within the confines of the helicopter fuselage. In one embodiment the missile supporting means is pivotally attached to the fuselage about a generally horizontal longitudinally extending hinge for movement through an opening in the fuselage between the operational and stowed positions. A closure member 16 is provided to automatically close the opening when the missile supporting means is in the closed position and conveniently the missile supporting means may be integral with the closure member.