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Erection girder body suitable for sea and air across amphibious unmanned aerial vehicle

A technology for drones and beams, applied in the direction of fuselage, aircraft parts, transportation and packaging, can solve the problems of inability to adjust the body structure, hinder the application of drones, etc., to simplify the production process, light weight, and reduce production. cost effect

Active Publication Date: 2013-06-26
北京华信智航科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] Most of the current body systems are integrated shells, and their wings and tails are fixed structures. When the operating environment (such as underwater environment, air environment, etc.) changes, it cannot adjust its own body structure according to environmental changes, which hinders unmanned The application of computer in unstructured and changing environmental conditions

Method used

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  • Erection girder body suitable for sea and air across amphibious unmanned aerial vehicle
  • Erection girder body suitable for sea and air across amphibious unmanned aerial vehicle
  • Erection girder body suitable for sea and air across amphibious unmanned aerial vehicle

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Embodiment Construction

[0050]The present invention will be further described in detail below in conjunction with the accompanying drawings.

[0051] A top view structure suitable for amphibious UAVs across sea and air such as figure 1 As shown, the UAV includes a coaxial anti-propeller assembly 1, an underwater propulsion assembly 2, a V-shaped tail assembly 3, a left wing assembly 4, a right wing assembly 5, a girder fuselage 6, a water air bag erection assembly 7, Left wing driving assembly 8, right wing driving assembly 9, folding wing support body 10 and folding and unfolding conversion assembly 11;

[0052] Wherein, the left wing assembly 4, the left wing drive assembly 8, the right wing assembly 5, the right wing drive assembly 9 and the folding wing support body 10 constitute the foldable wing part of the drone;

[0053] Wherein, the left wing assembly 4 has the same structure as the right wing assembly 5, and is installed symmetrically with the central axis of the fuselage;

[0054] Where...

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Abstract

The invention discloses an erection girder body suitable for a sea and air across amphibious unmanned aerial vehicle. The body comprises a first supporting rod, a second supporting rod, a third supporting rod, a fourth supporting rod, a first fixing plate, a second fixing plate, a third fixing plate, an erection girder shell, a supporting rod connecting disc and an erection girder outer sleeve, wherein the first supporting rod, the second supporting rod, the third supporting rod and the fourth supporting rod are supported through the first fixing plate and the second fixing plate which are arranged in parallel; the third fixing plate is arranged between the first fixing plate and the second fixing plate; the erection girder shell and the supporting rod connecting disc are connected through matching between the screw and the nut assembled in a lug; and one end of the erection girder outer sleeve is connected to the front end of the erection girder shell. The body has the rod piece structure, so that a sealing outer sleeve is not independently designed on the outer side, and when the unmanned aerial vehicle enters a water environment, gaps among various rod pieces can be rapidly filled with water, so that the average density of the unmanned aerial vehicle body is close to the density of water in a short time, and transition of the unmanned aerial vehicle from an air environment to a water environment is realized.

Description

technical field [0001] The invention relates to a fuselage of an unmanned aerial vehicle, more particularly, a fuselage with a girder structure suitable for an unmanned aerial vehicle with amphibious survivability in the sea and air. Background technique [0002] UAV is the abbreviation of unmanned aerial vehicle, and the English abbreviation is UAV (Unmanned Aerial Vehicle). [0003] The most important requirement for the design of the UAV is to be as light as possible while the fuselage system is strong enough. However, UAVs under various mission load requirements leave very limited space and quality quotas for motion transmission mechanisms. It is necessary to flexibly and efficiently convert basic engineering driving motions, such as high-speed rotation, into favorable controlled motions. The basic aviation transmission methods include direct drive, proportional amplification drive, electric servo drive and hydraulic servo drive. [0004] UAV is an unmanned aircraft op...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/00
Inventor 梁建宏杨兴帮吴海亮王田苗姚国才
Owner 北京华信智航科技有限公司
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