Turnover device for unmanned aerial vehicle fuel tank cap machining

A technology of turning over device and oil tank, applied in the direction of injection device, grinding drive device, metal processing equipment, etc., can solve the problems of inconvenient adjustment, different sizes, waste accumulation and clamping force, etc. The effect of working efficiency and improving stability and security

Inactive Publication Date: 2022-04-15
宿迁旋飞智能科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The invention provides an overturning device for the processing of the fuel tank cap of an unmanned aerial vehicle, which has the advantages of clamping according to specifications, convenient adjustment, waste collection and clamping protection, so as to solve the problems of different specifications, inconvenient adjustment, waste accumulation and clamping during processing. The problem of too much staying power

Method used

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  • Turnover device for unmanned aerial vehicle fuel tank cap machining
  • Turnover device for unmanned aerial vehicle fuel tank cap machining
  • Turnover device for unmanned aerial vehicle fuel tank cap machining

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Embodiment Construction

[0021] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0022] see Figure 1-3 , the present invention discloses an overturning device for processing the fuel tank cap of an unmanned aerial vehicle. The top of the plate 2 is fixedly provided with a horizontal support plate 201, and the inside of the horizontal support plate 201 is provided with positive and negative threaded rods 202, and the end of the positive and negative threaded rods 202 away from the left support plate 2 is provided with a first motor 203, T...

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Abstract

The invention discloses a turnover device for unmanned aerial vehicle fuel tank cap machining, and relates to the technical field of unmanned aerial vehicle production. Comprising a workbench, a left supporting plate and a right supporting plate are sequentially arranged at the top of the workbench from left to right, a transverse supporting plate is fixedly arranged at the top of the left supporting plate, a right-and-left threaded rod is movably arranged in the transverse supporting plate, and a first motor is arranged at the end, away from the left supporting plate, of the right-and-left threaded rod; a right supporting plate is fixedly arranged at the bottom of the first motor, movable blocks are movably arranged at the two ends of the right-hand and left-hand threaded rod, sliding blocks are fixedly arranged at the bottoms of the movable blocks, and the bottoms of the sliding blocks are provided with the inner walls, located in sliding grooves in the sliding groove plates, of sliding grooves. And the oil tank cap can be stabilized during overturning machining, buffering and damping protection can be conducted on the oil tank cap through springs, and the friction force can be increased and the surface of the oil tank cap can be protected through rubber positioning grooves.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicle production, in particular to a turning device for processing the fuel tank cap of an unmanned aerial vehicle. Background technique [0002] Unmanned aircraft, referred to as "UAV", is an unmanned aircraft controlled by radio remote control equipment and its own program control device. Unmanned aircraft is actually a general term for unmanned aircraft. From a technical point of view, it can be divided into Unmanned fixed-wing aircraft, unmanned vertical take-off and landing aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aircraft, unmanned parawing aircraft, etc., compared with manned aircraft, it has small size, low cost, easy to use It has the advantages of convenience, low requirements on the combat environment, and strong battlefield survivability. [0003] The fuel tank is an important basic component in the UAV system. It is used to store the fuel requir...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B05B13/02B05B14/00B24B19/00B24B41/06B24B47/12B24B47/22
Inventor 许旋旋
Owner 宿迁旋飞智能科技有限公司
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