Lookup-type manual-throw miniature fixed-rotor unmanned aerial vehicle body

Abstract

The invention relates to a lookup-type manual-throw miniature fixed-rotor unmanned aerial vehicle body which has good gas flow characteristics and good payload-carrying convenience, has large loadingspace for an equipment chamber and good parachuting safety, and allows body structure and payload to be never damaged during reclaiming. The lookup-type manual-throw miniature fixed-rotor unmanned aerial vehicle body comprises a lookup nose, a middle body and a tail support bar. The middle body tends to look up relative to the middle body so as to exhibit 'lookup' feature; the lookup nose is higher than the middle body; body surface is streamlined. The lookup-type manual-throw miniature fixed-rotor unmanned aerial vehicle body effectively ensures look-down space and practicality for payload and effectively improves pneumatic efficiency of an unmanned aerial vehicle, and therefore, the unmanned aerial vehicle has better endurance and wider curding range. The lookup-type manual-throw miniature fixed-rotor unmanned aerial vehicle body belongs to the field of application of unmanned aerial vehicle design techniques.

Description

technical field [0001] The invention relates to a head-up hand-throwable small fixed-wing unmanned aerial vehicle fuselage, which has good gas flow characteristics, convenient loading of mission loads, large loading space in the equipment compartment, high parachute safety, and is not easy to damage the fuselage structure when it is recovered and landed. And the fuselage of the head-up hand-throwing small fixed-wing UAV with mission load. The invention not only effectively guarantees the downward viewing space and practicability of the task load, but also effectively improves the aerodynamic efficiency of the drone, and realizes a greater flight time and range of the drone. It belongs to the application field of unmanned aerial vehicle design technology. Background technique [0002] The hand-throwable small fixed-wing UAV generally weighs no more than 5kg, carries a mission load of less than 1kg, uses batteries as energy sources, and uses motor-driven propellers to provide...

AI Technical Summary

Problems solved by technology

For small fixed-wing UAVs, most of them use parachuting or stall recovery. This recovery method is generally that the belly first touches the ground, and the task load is directly suspended under the belly and must be damaged. Wheeled or sled landing gear is used for landing. , can protect the load from the danger of touching the ground, but because of its non-retractable characteristics, it will definitely reduce the aerodynamic efficiency of the UAV, and then affect the flight time and range of the UAV

If the mission load is hidden in the belly of the aircraft, which is higher than the belly that touches the ground first when landing, it will inevitably lead to a limited downward viewing angle of the mission load, which will affect the scope of operation and execution effect of the mission.

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