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Manufacturing method for composite tailplane of small and medium size unmanned aerial vehicles

A technology of composite materials and horizontal fins, which is applied in the direction of household components, household appliances, and other household appliances, to achieve the effects of simplifying the molding process, reducing quality risks, and reliable product performance

Active Publication Date: 2018-11-27
XIAN AISHENG TECH GRP +1
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  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The technical problem solved by the present invention is: in view of the limitations of the prior art, the present invention provides a method for manufacturing a composite horizontal tail of a small and medium-sized UAV. The operability, sealing and demoulding during the product molding process effectively improve the complexity of the overall molding tooling and the scope of application of the overall molding of the horizontal tail structure

Method used

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  • Manufacturing method for composite tailplane of small and medium size unmanned aerial vehicles
  • Manufacturing method for composite tailplane of small and medium size unmanned aerial vehicles
  • Manufacturing method for composite tailplane of small and medium size unmanned aerial vehicles

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Embodiment Construction

[0032] see Figure 1-Figure 3 , the technical solution of the present invention is: a kind of manufacturing method of composite material horizontal tail of small and medium-sized unmanned aerial vehicles, and this process comprises the following steps:

[0033] Step 1, tooling design: According to the structural characteristics of the product, use CATIA software for 3D modeling and tooling design, and process the tooling mold according to the digital model to obtain the overall forming mold. The tooling design adopts block design to ensure process molding and product demoulding.

[0034] The auxiliary tooling for manufacturing the silicone rubber core mold includes a metal plate and a false beam. The metal plate is located at the end of one end of the assembled integral molding mold, and has the same cross-section as the end face; Between the rubber molding mandrel 5, it is used to replace the beam structure in the product, and its external dimensions are determined by the th...

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Abstract

The invention relates to a manufacturing method for a composite tailplane of small and medium size unmanned aerial vehicles. According to the method, the problem of limitation to the application of the present integrally molded tailplane structure is solved, the operability, airtightness and demolding property during the molding process of the product are promoted, and the complexity of integrallymolding assembling and the application scope of integral molding for the tailplane structure are effectively improved. The potential quality hazard in the present integral molding is effectively reduced, the quality of the integrally molded tailplane is more stable and the reliability of the products is effectively promoted; the integrally molding assembling is simplified and the molding technology is simplified; the performance stability and size stability of the integrally molded product are guaranteed, the design / manufacturing integration is realized, the technological difficulty is reduced and the production cycle is shortened.

Description

technical field [0001] The invention belongs to the technical field of UAV composite material forming technology, and relates to a method for manufacturing a composite horizontal tail of a small and medium-sized UAV. Background technique [0002] The designability, light weight, and high strength of composite materials have made them widely used in the field of aviation drones; for structural parts with complex structures, the use of composite material integral molding manufacturing technology not only gives full play to the overall advantages of composite materials , greatly reducing the number of parts and intermediate processing links, etc., and effectively improving the overall performance, reducing the structural weight, shortening the production cycle, reducing production costs, and improving the structural performance of the product. [0003] The Chinese invention patent with the notification number CN 103057126 A announced "a large-scale composite material integral m...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B29C70/34B29C70/54B29C33/38B29L31/30
CPCB29C33/3842B29C70/342B29C70/54B29C2033/385B29L2031/3085
Inventor 赵伟超孙奇赵景丽何颖段国晨童话王安文
Owner XIAN AISHENG TECH GRP
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