Novel flight device

Abstract

The invention discloses a novel flight device, and belongs to the technical field of unmanned aerial vehicles. The novel flight device comprising comprises a device body, a fuel tank, a connecting seat, an internal combustion engine, a generator and a battery, wherein the device body is provided with a first side face, a second side face, a third side face and a hollow body; the fuel tank is fixedly arranged in the hollow body, and the connecting seat is provided with a first fastening surface and a second fastening surface, wherein the connecting seat is detachably connected with the second side face through the first fastening surface; the internal combustion engine is connected with the connecting seat through the second fastening surface, and the generator is fixedly connected with theconnecting seat through the second fastening surface and is connected with the internal combustion engine; the battery is correspondingly connected with the internal combustion engine and the generator; the internal combustion engine further includes an exhaust pipe; and an unmanned aerial vehicle further includes a silencer, wherein the silencer and the exhaust pipe are connected. The novel flight device achieves the technical effect of prolonging the time of endurance of the unmanned aerial vehicle.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to a novel flying device. Background technique [0002] Unmanned UAV, referred to as "UAV", is an unmanned UAV controlled by radio remote control equipment and its own program control device. There is no cockpit on board, but it is equipped with autopilot, program control device, information collection device and other equipment. The personnel on the ground, on the ship, or at the remote control station of the parent aircraft track, locate, remotely control, telemeter and digitally transmit it through radar and other equipment. It can take off like an ordinary UAV under radio remote control or be launched into the air with a booster rocket, or it can be brought into the air by the parent aircraft for flight. [0003] For the multi-rotor UAV, the fuselage of the multi-rotor UAV in the prior art is made of an integrally formed structure. Usually, the ta...

AI Technical Summary

Problems solved by technology

However, since the UAV consumes a lot of power during flight, and the power of the battery is extremely limited, when the power of the battery is exhausted, the UAV will be forced to stop flying, which results in a short battery life of the UAV.

[0004] In summary, in the existing UAV technology, there is a technical problem that the UAV's battery life is short

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