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An unmanned helicopter fuel tank and an unmanned helicopter

A technology of unmanned helicopter and helicopter body, which is applied to the fuel tank of the power unit and other directions, can solve the problems of low installation efficiency, inconvenient installation, and labor consumption, and achieve the effect of convenient and simple installation.

Pending Publication Date: 2018-12-21
必扬星环(北京)航空科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0004] The purpose of the present invention is to provide an unmanned helicopter fuel tank and an unmanned helicopter, to solve the inconvenience of installation in the process of installing the unmanned helicopter fuel tank in the prior art, which requires the cooperation of many people to complete, and consumes a lot of manpower And the technical problem of low installation efficiency

Method used

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  • An unmanned helicopter fuel tank and an unmanned helicopter
  • An unmanned helicopter fuel tank and an unmanned helicopter
  • An unmanned helicopter fuel tank and an unmanned helicopter

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Embodiment Construction

[0032] In order to make the purpose, technical solution and advantages of the present invention clearer, the technical solution of the present invention will be described in detail below. Apparently, the described embodiments are only some of the embodiments of the present invention, but not all of them. Based on the embodiments of the present invention, all other implementations obtained by persons of ordinary skill in the art without making creative efforts fall within the protection scope of the present invention.

[0033] The invention provides an unmanned helicopter fuel tank, figure 1 It is the structural representation of the fuel tank of the unmanned helicopter in this embodiment, as figure 1 As shown, a fuel tank body 1 is included, and a first connecting piece 2 is fixed on the fuel tank body 1, and the first connecting piece 2 is slidably connected with a second connecting piece 3 fixed on the unmanned helicopter.

[0034] By setting the fuel tank through the slid...

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Abstract

An unmanned helicopter fuel tank and an unmanned helicopter are provided, A technical field relate to that mechanical equipment of an unmanned helicopter, so as to solve the installation inconvenienceduring the installation of the fuel tank of an unmanned helicopter in the prior art, It takes a lot of people to do it, technical problems that cost a lot of manpower and are inefficient to install,The fuel tank of the unmanned helicopter comprises a fuel tank body, a first connecting piece is fixedly arranged on the fuel tank body, and the first connecting piece is slidably connected with a second connecting piece fixed on the unmanned helicopter. The invention is used for reducing the human resources consumed in installing the unmanned helicopter and improving the installation efficiency of the unmanned helicopter.

Description

technical field [0001] The invention relates to the technical field of unmanned helicopter mechanical equipment, in particular to an unmanned helicopter fuel tank and an unmanned helicopter. Background technique [0002] As we all know, the fuel tank of the unmanned helicopter is installed inside the fuselage of the unmanned helicopter, which is an indispensable part of the unmanned helicopter. [0003] At present, in the process of installing the fuel tank of unmanned helicopters, most of the fuel tanks are fixed by screw straps for safety and stability in order to avoid the fluctuation of the fuel in the fuel tank due to inertia and gravity when the drone is flying. The fuel tank is fixed in the unmanned helicopter, but the installation form of this structure is inconvenient to install, and it needs the cooperation of multiple people to complete the installation, which consumes a lot of manpower and has low installation efficiency. Contents of the invention [0004] The...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D37/04B64D37/06
CPCB64D37/04B64D37/06
Inventor 田松
Owner 必扬星环(北京)航空科技有限公司