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Unmanned plane capable of adapting different taking-off and landing modes and different mission loads by replacing multiple power combinations

A technology that adapts to different and multi-power, applied in the field of drones, can solve the problems of low versatility and platform, high occupation cost, and large space occupation of drones, so as to improve the performance of transition operations, use convenience and economy , the effect of convenient transportation

Active Publication Date: 2017-05-10
北京奇正数元科技股份有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, the power system of a general small UAV is fixedly connected to the body, so it is difficult to realize the application of multiple adaptation scenarios and multiple power combination modes on the same UAV body platform, resulting in the Less versatility and platform
[0004] If a specific model is used to complete a specific task, there are problems such as high occupation cost, large space occupation, and difficult transportation

Method used

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  • Unmanned plane capable of adapting different taking-off and landing modes and different mission loads by replacing multiple power combinations
  • Unmanned plane capable of adapting different taking-off and landing modes and different mission loads by replacing multiple power combinations
  • Unmanned plane capable of adapting different taking-off and landing modes and different mission loads by replacing multiple power combinations

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Embodiment Construction

[0058] The present invention will be specifically introduced below in conjunction with the accompanying drawings and specific embodiments.

[0059] refer to Image 6 , Figure 7 , Figure 8 with Figure 9 , the multi-power combination of the present invention replaces the unmanned aerial vehicle that adapts to different take-off and landing modes and different task loads, including: a fuselage 10, a left wing 20, a right wing 30 and an empennage 40, wherein the empennage 40 is screwed to the fuselage 10 . In addition, it also includes: main power module A50, main power module B60, auxiliary power module A70, auxiliary power module B80 and tail shaping module C90, choose to use different main power module A50, main power module Group B60, auxiliary power module A70, auxiliary power module B80 and tail shaping module C90 can form multiple power combination modes, so that the drone of the present invention can adapt to various scenarios.

[0060] Both the active power module ...

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Abstract

The invention discloses an unmanned plane capable of adapting different taking-off and landing modes and different mission loads by replacing multiple power combinations. The unmanned plane comprises a fuselage, a left wing, a right wing, an empennage, a main power module A, a main power module B, an auxiliary power module A, an auxiliary power module B and an empennage shaping module C. The unmanned plane has the beneficial effects that (1) the unmanned plane has various power combination modes, the unmanned plane can adapt to various occasions on the same unmanned fuselage platform, and the universality and platform performance of the unmanned plane are greatly improved; and (2) all the modules are designed in a modular mode, the transferring operation performance is improved, transportation, preservation, maintenance and debugging of the unmanned plane are greatly facilitated, and the unmanned plane is quite convenient to use and economical.

Description

technical field [0001] The invention relates to a small-sized unmanned aerial vehicle, in particular to an unmanned aerial vehicle with multi-power combination replacement and adapting to different take-off and landing modes and different task loads, and belongs to the technical field of unmanned aerial vehicles. Background technique [0002] The power system of the drone is used to provide thrust for the flight of the drone, which is a very important part of the design and manufacture of the drone. Due to different take-off and landing places, endurance time, cruising radius, and mission loads, UAVs may need to be replaced with different power systems. [0003] However, the power system of a general small UAV is fixedly connected to the body, so it is difficult to realize the application of multiple adaptation scenarios and multiple power combination modes on the same UAV body platform, resulting in the Versatility and platform are low. [0004] If a specific model is use...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D27/26B64C27/28B64C27/26B64D27/40
CPCB64C27/26B64C27/28B64U30/10B64U30/20B64U50/19B64D27/40Y02T50/60
Inventor 崔艳鸿周烈
Owner 北京奇正数元科技股份有限公司