Unmanned aerial vehicle inclined camera pod for aerial survey and aerial photography

The utility model discloses an unmanned aerial vehicle tilt camera pod for aerial survey and aerial photography, which comprises a pod, a rotating mechanism is arranged at the bottom of the pod, the rotating mechanism comprises a servo motor, a transmission rod and a connecting shaft, the servo moto...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser:	MA YANGANG
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COSMONAUTICS ELECTRIC COMMUNICATION TECHNIQUE ELECTRICITY ENGINEERING ELEMENTS AND UNITS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING LIGHTING MEANS FOR DAMPING VIBRATION MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS PICTORIAL COMMUNICATION, e.g. TELEVISION SHOCK-ABSORBERS SPRINGS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	The utility model discloses an unmanned aerial vehicle tilt camera pod for aerial survey and aerial photography, which comprises a pod, a rotating mechanism is arranged at the bottom of the pod, the rotating mechanism comprises a servo motor, a transmission rod and a connecting shaft, the servo motor is mounted at the bottom of the pod, and the transmission rod is mounted on the connecting shaft. The power output end of the left side of the servo motor is vertically connected with a connecting shaft A through a transmission rod and is connected with a connecting shaft B in parallel, and camera mounting holes are formed in the centers of the bottom ends of the connecting shaft A and the connecting shaft B. According to the camera pod, 360-degree rotation of the camera in the vertical direction and the horizontal direction is achieved through the vertical connecting shaft and the horizontal connecting shaft, and the shooting azimuth range of the unmanned aerial vehicle is large; the damping device is arranged,