Unmanned aerial vehicle electric cabin composite cephalic cone integrated forming tool and process

A composite material and forming tooling technology, which is applied in the direction of household components, household appliances, and other household appliances, can solve problems such as insufficient operating space and difficult operation of female molds, and achieve the effect of ensuring assembly accuracy and reducing equipment costs

Active Publication Date: 2020-05-22
AEROSPACE SHENZHOU AIRCRAFT
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] In the existing UAV technology, the composite material parts must ensure both the aerodynamic shape and the assembly accuracy. For the composite material structure of the secondary bonding and secondary assembly, the...

Method used

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  • Unmanned aerial vehicle electric cabin composite cephalic cone integrated forming tool and process

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Embodiment approach

[0036] As a preferred embodiment of the present invention, the forming tooling manufactures metal male molds and related assembly components according to product precision requirements, and combines three coordinates to ensure assembly accuracy, and prepares qualified composite nose cones 15 with the forming tooling.

[0037] As a preferred embodiment of the present invention, in the step 2 and step 3, the requirements for the paving environment are as follows: the temperature is 22°C±4°C, the humidity is 30%-65%, and the indoor cleanliness should reach ≥10μm of dust particles No more than 10 pieces / L; the pre-compaction vacuum pressure is ≥0.09MPa, and the time is 30 minutes.

[0038] As a preferred embodiment of the present invention, in the step 2 and step 3, the number of layers of carbon fiber prepreg is 20 layers.

[0039] As a preferred embodiment of the present invention, the male model surface 1 , the inner square tube support 2 , the inner central circular tube suppo...

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PUM

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Abstract

The invention provides an unmanned aerial vehicle electric cabin composite cephalic cone integrated forming tool and process. The unmanned aerial vehicle electric cabin composite cephalic cone integrated forming tool comprises a male molded surface, internal square pipe supports, a blocked metal core model, a metal moving disc, internal center circular pipe supports, positioning pins, fastening bolts, demolding bolts and demolding blocks, four swivels are mounted on the outer side wall of the male molded surface, a vacuum bag area is formed in the surface of the male molded surface, the blocked metal core model sleeves the top of the male molded surface, and the blocked metal core model and the male molded surface are in positioning butt-joint through the positioning pins. According to theunmanned aerial vehicle electric cabin composite cephalic cone integrated forming tool and process, design is reasonable, the assembly accuracy can be guaranteed, it is guaranteed that secondary bonding co-curing forming of a composite cephalic cone and a motor mounting metal clamping disc meets the requirements, and meanwhile the equipment cost can be lowered.

Description

technical field [0001] The invention belongs to the technical field of UAV accessories processing, and in particular relates to an integrated molding tooling and molding process of a composite material nose cone of an UAV motor cabin. Background technique [0002] With the continuous development of aviation technology, UAV has become the focus of research in various countries. Due to its characteristics of being unmanned, long in the air, and high precision, it can be used in relay communication, monitoring, reconnaissance, surveillance, and strikes in different terrains and regions, and has broad application prospects in military and civilian fields. [0003] Advanced composite materials have the advantages of high specific strength, high specific modulus, and strong designability. Due to the requirement of lightweight, more and more aircrafts adopt composite materials. Since the use of composite materials can greatly reduce the structural weight, improve the overall perf...

Claims

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Application Information

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IPC IPC(8): B29C70/34B29C70/54B29C33/38B29C33/30B29L31/30
CPCB29C33/30B29C33/305B29C33/38B29C70/342B29C70/54B29C70/545B29L2031/3076
Inventor 李宁刘瑞东彭海珍沙灯卜李小勇
Owner AEROSPACE SHENZHOU AIRCRAFT
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