A collision-resistant quadrotor spherical UAV system
A technology of drones and quadrotors, applied in the field of drones, can solve problems such as being vulnerable to collisions, the inability of drones to enter the scene, and crashes, so as to improve collision resistance, reduce the possibility of damage and fall, and reduce Effects of impact or disturbance of flight attitude
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Embodiment 1
[0057] A collision-resistant four-rotor spherical UAV system, such as Picture 10 As shown, it includes a flight platform 001 for performing flight tasks, a task load 002 carried on the flight platform 001 for detection, and ground equipment for remote control, telemetry, and data transmission of the flight platform 001 or the task load 002.
[0058] Such as Figure 1-Figure 5 As shown, the flying platform 001 includes a spherical frame mechanism 1, an aircraft body 3 completely located inside the spherical frame mechanism 1, and a supporting mechanism 2 that connects the spherical frame mechanism 1 and the aircraft body 3 into an integral body.
[0059] The spherical frame mechanism 1 as a whole is in the structure of the latitude and longitude frame of the globe. The supporting mechanism 2 includes an annular connecting piece located in the center of the spherical frame mechanism 1 and two supporting tubes 204 respectively arranged along the rotation axis of the globe. The annular...
Embodiment 2
[0064] In this embodiment, the structure of the flight platform 001 is further optimized on the basis of embodiment 1, such as Figure 1-Figure 4 As shown, the flying platform 001 is mainly composed of a spherical frame mechanism 1, an aircraft body 3, and a supporting mechanism 2 that connects the spherical frame mechanism 1 and the aircraft body as a whole. The spherical frame mechanism 1 and the supporting mechanism 2 together form a spherical protective structure that protects the aircraft body 3, improves the collision resistance of the entire flying platform 001, and effectively protects the aircraft body 3 to fly safely in a complex environment. The mission load 002 is integrated on the aircraft body 3 for easy disassembly and maintenance.
[0065] In this embodiment, the specific structure of the spherical frame mechanism 1 and the supporting mechanism 2 is emphasized, and the principle that the spherical protective mechanism makes the aircraft body 3 resistant to collisi...
Embodiment 3
[0084] In this embodiment, on the basis of Embodiment 2, the material of the spherical frame mechanism 1 is further optimized. Such as Figure 5 As shown, the latitude ring frame 101 is a complete ring-shaped carbon fiber sheet; the longitude ring frame 102 is composed of four fan-ring carbon fiber sheets spliced together; the longitude tube 103 is a glass fiber stringer; the bearing seat 104, The bearings 105 are all lightweight plastics; the end faces of the bearing housing 104 are respectively fixed with the glass fiber stringers passing through the annular carbon fiber sheet and the fan-ring carbon fiber sheet fixed on the annular carbon fiber sheet at one end. Each additional circular latitude circle is composed of four fan-ring carbon fiber sheets, or each additional circular latitude circle uses one end-to-end looped glass fiber stringer, or the additional circular latitude circle part uses four fan-ring carbon fiber It is composed of splicing thin slices and partly co...
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