Disclosed is an unmanned aerial vehicle (UAV) with a pre-defined shape to deploy one or more items. The unmanned aerial vehicle (UAV) includes an upper housing, a lower housing, and a power unit. The upper housing includes plurality of rotors to lift and propel the unmanned aerial vehicle (UAV). Further the unmanned aerial vehicle (UAV) includes various electronic components such as plurality of electronic cards, a processing unit, a Global Positioning System (GPS), a communication unit, an electronic gyroscope, a barometer, engines and flight control system, video camera, a forward looking infrared (FLIR) device, a microphone, and a laser telemeter/designator/range finder. The power unit powers the aforementioned electronic components. The lower housing includes plurality of storage units to stores one or more items. The lower housing is removably attached with the upper housing in a way to deploy the items at a predetermined location through plurality of openings.

A flying device includes: an image capturing unit that captures an image of an object that is moving; a flying unit that flies with the image capturing unit mounted thereat; and a control unit that controls at least one of the flying unit and the image capturing unit with control information based on an output from the image capturing unit so as to engage the image capturing unit, after having captured the image of the object, to capture an image of the object.

A propeller-enclosed airlifting air tube apparatus contains a unique multi air-tube structure that functions as a plurality of air outtakes to produce stable lift force with one or more propellers enclosed in the apparatus. By encapsulating the propellers within the outer shells, the airlifting air tube apparatus is able to reduce potential bodily harm and property damage risks during a flight operation in a densely-populated environment or in another environment involving tight spaces. The airlifting air tube apparatus encapsulates one or more pairs of contra-rotating propellers inside a drone casing to enhance operational safety while minimizing the overall footprint of the apparatus. Furthermore, the airlifting air tube apparatus incorporates a novel airflow control dish-based flight control steering unit configured to change directions and altitudes of the apparatus by dynamically adjusting the airflow to each outtake air tube with the airflow control dish.

A propeller-enclosed airlifting air tube apparatus contains a unique multi air-tube structure that functions as a plurality of air outtakes to produce stable lift force with one or more propellers enclosed in the apparatus. By encapsulating the propellers within the outer shells, the airlifting air tube apparatus is able to reduce potential bodily harm and property damage risks during a flight operation in a densely-populated environment or in another environment involving tight spaces. The airlifting air tube apparatus encapsulates one or more pairs of contra-rotating propellers inside a drone casing to enhance operational safety while minimizing the overall footprint of the apparatus. Furthermore, the airlifting air tube apparatus incorporates a novel airflow control dish-based flight control steering unit configured to change directions and altitudes of the apparatus by dynamically adjusting the airflow to each outtake air tube with the airflow control dish.

A multi-axis amphibious copter for flying and cruising at high speeds. The multi-axis amphibious copter includes six propulsion points i.e., four propellors oriented vertically, a coaxial rotor oriented vertically, and a mini turbine thruster on the rear of the aircraft body and configured to propel the multi-axis amphibious copter forward. The multi-axis amphibious copter can land and take off vertically from congested places and can fly at cruising speeds.

A drone having a deployment device, which is configured such that the same can fly both in a folded mode and in a deployed mode. A platform 300 is arranged in the middle of the drone body 400, a deployment device 200 is arranged on the radial outer side of the platform 300, a fixed support table 230 extends outwardly from the radial outer surface of the platform 300, a rotating support table 210 is coupled to an outer free end of the fixed support table 230, and the rotating support table 210 is rotatably coupled to/supported on the outer free end of the fixed support table 230. Multiple propellers 100 are mounted on the radial outer ends of the rotating support table 210, respectively, a landing structure 600 is coupled to the body 400, and a holder 500 is mounted on the landing structure 600.

A remote controlled aircraft includes an aircraft that may be flown. A plurality of light emitters is coupled to the aircraft. A plurality of fans is coupled to the aircraft. Each of the fans may move air thereby facilitating each of the fans to urge the aircraft to fly. A control unit is coupled to the aircraft and the control unit is electrically coupled to each of the fans. The control unit includes a global positioning system. Thus, the control unit may identify a position of the aircraft with respect to Earth. A remote control is provided and the remote control may be manipulated. The remote control is in electrical communication with the control unit such that the remote control controls directional flight of the aircraft.

An unmanned aerial vehicle (UAV) and a method for controlling the flight of the UAV are provided. The UAV provides a motion feedback corresponding to a user command received and a method for controlling the flight of the UAV. The UAV further provides a magnitude of motion feedback that is varied depending on the distance and/or direction between the user and the UAV and a method for controlling the flight of the UAV.

A UAV and a flying control method thereof that can detect a user grip of the UAV are provided. The UAV and a flying control method thereof can detect a user grip at a first position and can detect release of the user grip at a second position.

There is provided a mono-wing aerial device which includes a housing member having disposed thereon electronic components and a power source, including a controller configured to control a thrust unit; a wing member coupled to the housing member, the wing member configured to produce aerodynamic forces for autorotation of the aerial device, the wing member comprising a first edge portion proximal to the housing member and a second edge portion distal to the housing member, wherein the wing member is coupled to the housing member at the first edge portion; and the thrust unit coupled to the wing member at the second edge portion, wherein the thrust unit is configured to generate thrust in a direction substantially tangential to a rotational plane of the wing member. There is also provided a method of forming the mono-wing aerial device.