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Tail support type water unmanned aerial vehicle

A technology of unmanned aerial vehicle and tail support, which can be used in seaplanes, unmanned aerial vehicles, motor vehicles, etc., can solve the problems of small payload, large body weight, inconvenient recycling, etc., and achieve strong survivability, stability and reliability. effect of structure

Pending Publication Date: 2019-02-19
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] At present, UAV technology is developing rapidly and has been widely used in many fields such as military and civil affairs. Existing UAVs generally use landing gear recovery and net recovery. If a suitable landing environment cannot be found, the drone will crash when its energy is exhausted
Therefore, traditional UAVs face problems such as being unable to take off and land on the water surface, and inconvenient to recover when sailing at sea.
At the same time, it also has the disadvantages of heavy body weight and small payload.

Method used

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  • Tail support type water unmanned aerial vehicle
  • Tail support type water unmanned aerial vehicle
  • Tail support type water unmanned aerial vehicle

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Embodiment Construction

[0020] The preferred implementation of the device and method of the present invention will be further described in detail below in conjunction with the accompanying drawings.

[0021] Such as figure 1 As shown, a tail support type water unmanned aerial vehicle, including a fuselage 1, is installed on the top of the fuselage 1 along the wings 5 ​​extending on both sides of the central axis of the fuselage 1, and is installed on the electronic pod below the front of the fuselage 1. 2. The propeller engine 12 installed at the rear of the fuselage 1 provides power for the UAV, the fairing 13 fixed on the fuselage 1, the tail brace 6 connected with the fairing 13, and the empennage connected with the tail brace 6 , connected to the buoys 3 extending obliquely downward along both sides of the central axis below the fuselage 1 . The tail support 6 can make the UAV have a more stable structure and a wider detection field of view.

[0022] Such as figure 1 with Figure 4 As shown, ...

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Abstract

The invention discloses a tail support type water unmanned aerial vehicle, which comprises a vehicle body, two wings mounted on both sides of the vehicle body along the central axis of the vehicle body, an electronic pod mounted below the front of the vehicle body, a propeller engine mounted at the rear of the vehicle body anda fairing fixed to the vehicle body, a tail support connected to the fairing, a tail fin connected to the tail support, and a pontoon that extends obliquely downward along both side of the central axis below the vehicle body. The tail support type water unmanned aerial vehicle has a stable and reliable structure and a wider detection field, in which the vehicle can float and take off and land on the water surface.

Description

technical field [0001] The invention relates to the field of water drones, in particular to a tail support type water drone. Background technique [0002] At present, UAV technology is developing rapidly and has been widely used in many fields such as military and civil affairs. Existing UAVs generally use landing gear recovery and net recovery. If a suitable landing environment cannot be found, the UAV will crash when its energy is exhausted. Therefore, traditional UAVs face problems such as being unable to take off and land on the water surface, and inconvenient to recover when sailing at sea. At the same time, it also has the disadvantages of heavy body weight and small payload. [0003] Therefore, a new technical solution is needed to solve the above technical problems. Contents of the invention [0004] In order to solve the deficiencies of the prior art, the present invention proposes a tail-brace type water drone, which has a stable and reliable structure and a w...

Claims

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Application Information

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IPC IPC(8): B64C35/00
CPCB64C35/00B64U10/00
Inventor 申遂愿朱清华曾嘉楠朱振华招启军王坤
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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