Aerial releasing type high-altitude gliding drone aircraft

The utility model discloses an aerial releasing type high-altitude gliding drone aircraft. The overall structure of a drone aircraft body is a conical rectification body, the front section of the drone aircraft body is an oval rectification body, the middle of the drone aircraft body is a cylinder,...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	CUI JINJIE, SUN XIAOFANG, CHANG TIEZHENG
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING BULLET CATCHERS COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HEATING HELICOPTERS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TARGET RANGES TARGETS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	The utility model discloses an aerial releasing type high-altitude gliding drone aircraft. The overall structure of a drone aircraft body is a conical rectification body, the front section of the drone aircraft body is an oval rectification body, the middle of the drone aircraft body is a cylinder, a folding wing and a wing unfolding driver module are arranged in the drone aircraft body, and a launch power module is located below the wing unfolding driver module inside the drone aircraft body. A drag parachute and a parachute-opening structure of the drag parachute are arranged inside the drone aircraft body. The parachute-opening structure is located between the wing unfolding driver module and the launch power module, and a thermal insulation layer is arranged behind the launch power module. A control system antenna is installed on the lower surface of the drone aircraft body. The aerial releasing type high-altitude gliding drone aircraft is low in manufacturing cost, collision between the drone aircraft an