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Cushioned landing gear for rotorcraft UAVs

A technology for unmanned aerial vehicles and landing gear, applied in the field of unmanned aerial vehicles, can solve problems such as damage to airborne equipment, and achieve the effect of prolonging service life, avoiding damage and improving stability

Active Publication Date: 2019-09-10
JIANGSU UNIV OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] In order to solve the problem of damage to the UAV and UAV airborne equipment caused by collision with the ground when the rotor UAV lands in the prior art, the present invention provides a buffer type for the UAV. landing gear

Method used

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  • Cushioned landing gear for rotorcraft UAVs
  • Cushioned landing gear for rotorcraft UAVs
  • Cushioned landing gear for rotorcraft UAVs

Examples

Experimental program
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Embodiment

[0031] like Figure 1-6 As shown, a cushioning landing gear for a rotary-wing unmanned aerial vehicle includes a housing 1 with limiting long slots 11 on both sides, a driving device arranged in the housing 1 and a lifter arranged under the housing 1. The folding frame 3 is provided with a buffer device 5 on both sides of the drive device, and the buffer device 5 includes a spring tube 51, a spring frame 52 slidingly sleeved on the spring tube 51, and a lead screw 53 connected to the drive device for transmission. And the moving nut 54 that cooperates with leading screw 53, described driving device selects through-type linear lead screw motor 2, because of itself both sides have leading screw 53, transmission precision is higher than selecting leading screw 53 and driving device transmission connection in addition, and The cost is low. One end of the spring tube 51 is provided with a spring stop ring 55, and the other end is fixedly connected with the moving nut 54. The spring...

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PUM

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Abstract

The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to a buffer landing gear for a rotor-type unmanned aerial vehicle, which includes a housing with long space-limiting slots on both sides, a driving device arranged in the housing, and a driving device arranged in the housing. For the lifting and folding frame below, buffer devices are provided on both sides of the drive device, and the buffer device includes a spring tube, a spring frame slidingly sleeved on the spring tube, a lead screw connected to the drive device and a lead screw connected to the drive device. A matching moving nut, one end of the spring tube is provided with a spring stop ring, the other end is fixedly connected with the moving nut, the spring tube is covered with a buffer spring, and the buffer spring is located between the spring stop ring and the spring frame, Both the moving nut and the spring blocking ring are outwardly extended with a limiting block matched with the limiting long groove, and the lifting and folding frame includes a folding unit, and the folding unit includes two connecting rods hinged to each other, and the two The top ends of the connecting rods are respectively hinged with the bottom ends of the corresponding spring holders.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to a buffer landing gear for a rotary-wing unmanned aerial vehicle. Background technique [0002] At present, UAVs are used more and more widely, including fixed-wing UAVs and rotary-wing UAVs. The former has strong endurance, fast flight speed, good concealment, and can work at high altitudes. It has been widely used in reconnaissance. Aerial photography, agriculture, weather monitoring and many other military or civilian fields; the latter is a relatively small, stable flight, small UAV that can hover in the air or track slowly, due to its excellent flight performance and good reliability The controllability is deeply loved by civilian amateurs, and it occupies a huge market in many public safety fields such as aerial photography and real-time monitoring, as well as in the field of civilian entertainment. [0003] At present, the landing gear designed...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C25/62B64C25/10
CPCB64C25/10B64C25/62B64U10/10
Inventor 徐旭松刘加南刘梦吴德辉
Owner JIANGSU UNIV OF TECH