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Skid-type landing gear of an unmanned helicopter

An unmanned helicopter and landing gear technology, applied in landing gear, unmanned aerial vehicles, motor vehicles, etc., can solve the problems of complexity, limited ability to absorb shock and impact energy, and large number of parts, and achieve a simple structure. , good craftsmanship, easy to produce effect

Active Publication Date: 2022-05-17
BEIJING ZHZ TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In view of the above-mentioned analysis, the present invention aims to provide a skid-type landing gear of an unmanned helicopter, which solves the problem of heavy structure, large and complex parts, and the limitation of the deformation of the bow beam of the landing gear in the prior art, which leads to its shock absorption and Problem with limited ability to absorb impact energy

Method used

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  • Skid-type landing gear of an unmanned helicopter
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  • Skid-type landing gear of an unmanned helicopter

Examples

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Embodiment 1

[0038] This embodiment provides a skid type landing gear of an unmanned helicopter, see Figure 1 to Figure 4 , including two sets of skid tube assemblies and two sets of arched beam assemblies, the skid tube assembly includes a skid tube 1, the arched beam assembly includes a sleeve 2 and two half-arched beams 3, one end of one half-arched beam 3 passes through The sleeve 2 is slidingly connected to one end of another half-arch beam 3, and the other end of the half-arch beam 3 is fixedly connected to the skid tube 1 by means of bolts, welding or riveting; along the direction gradually away from the sleeve 2, the half-arch beam The beam 3 is divided into successively connected horizontal sections, arc sections and inclined sections; the side of the semi-arched beam 3 facing the fuselage of the unmanned helicopter is hinged with the fuselage of the unmanned helicopter.

[0039] Compared with the prior art, the skid-type landing gear of the unmanned helicopter provided by this e...

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Abstract

The invention discloses a skid-type landing gear of an unmanned helicopter, which belongs to the technical field of unmanned helicopters, and solves the problem of heavy structure, large and complex parts, and limited deformation of the bow beam of the landing gear in the prior art, resulting in its shock absorption and limited ability to absorb impact energy. The landing gear includes two sets of skid tube assemblies and two sets of arch beam assemblies; the skid tube assembly includes a skid tube, the arch beam assembly includes a sleeve and two half arch beams, one end of one half arch beam passes through the sleeve It is slidingly connected with one end of the other half-arch beam, and the other end of the half-arch beam is fixedly connected with the skid tube; along the direction gradually away from the sleeve, the half-arch beam is divided into successively connected horizontal sections, arc sections and inclined sections ; The side of the semi-arched beam facing the fuselage of the unmanned helicopter is hinged with the fuselage of the unmanned helicopter. The landing gear can be used for buffering when the unmanned helicopter lands.

Description

technical field [0001] The invention belongs to the technical field of equipment used for cooperating with or mounted on an aircraft, and in particular relates to a skid-type landing gear of an unmanned helicopter. Background technique [0002] The unmanned helicopter landing gear has the functions of supporting the carrier, transmitting ground loads, shock absorption and absorbing impact energy, reducing overload caused by landing impact, and providing a ground transfer interface. [0003] The existing unmanned helicopter landing gear usually includes the following two types: one of them relies on a buffer for shock absorption and buffering. The landing gear of this structure has a heavy structure, a large number of parts and is complicated due to the buffer, and the use of More maintenance work is required in the process; the other one only relies on the elastic deformation of the thin-walled pipe (mainly the bending deformation of the bow beam as a whole) to absorb energy...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C25/52B64C25/62
CPCB64C25/52B64C25/62B64C2025/325B64U10/10
Inventor 裴桃林霍亚东邓海波刘杨舜田刚印
Owner BEIJING ZHZ TECH
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