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Flexible cable process digital prototype construction system and method for spacecraft assembly

A spacecraft assembly and flexible cable technology, applied in the direction of electrical digital data processing, instruments, computer-aided design, etc., can solve problems such as unavoidable, complicated branch relationship of cable components, and narrow space for spacecraft assembly, so as to reduce the occurrence of quality problems The effect of probability

Active Publication Date: 2019-08-23
BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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AI Technical Summary

Problems solved by technology

[0003] 1) The branching relationship of the cable assembly is complex. Generally, one cable is connected to multiple stand-alone devices. However, all cables are displayed synchronously in the cable design model, and the final assembly implementation needs to be laid one by one. Find the information of the laid cables (such as connected products, direction, products to be avoided, etc.);
[0004] 2) Due to the extremely narrow assembly space of satellites and other spacecraft, if the cables cannot avoid related products or do not reserve a safety gap when laying cables, it may cause quality problems such as cable damage;

Method used

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[0035]The following is a specific implementation manner of the content of the present invention, and the content of the present invention will be further clarified through the specific implementation mode below. Of course, the following specific embodiments are described only to illustrate different aspects of the present invention, and should not be construed as limiting the scope of the present invention.

[0036] see figure 1 , figure 1 It shows a schematic diagram of the module structure of the digital prototype automatic construction system for the spacecraft general assembly flexible cable process of the present invention. Among them, the module structure of the automatic construction system of digital prototype of flexible cable technology for spacecraft assembly mainly includes the following modules: interface module, product classification module, connection relationship identification module, assembly relationship calculation module, and cable technology digital pro...

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Abstract

The invention discloses a flexible cable process digital prototype automatic construction system for spacecraft assembly. The flexible cable process digital prototype automatic construction system mainly comprises the following modules: an interface module, a product classification module, a connection relationship identification module, an assembly relationship resolving module and a cable process digital prototype construction module. According to the invention, rapid construction of the flexible cable process digital prototype is realized, and related requirements of cable laying are met; on the basis of simplifying an overall unit cable design model, complete information required by cable laying is reserved, and the probability of quality occurrence in the cable laying process in narrow spaces such as satellites is reduced.

Description

technical field [0001] The invention belongs to the technical field of spacecraft general assembly, and in particular relates to a system and method for automatically constructing a digital prototype of a flexible cable process oriented to spacecraft general assembly. Background technique [0002] At present, the design work of my country's satellites and other spacecraft products has been widely realized in 3D, and various design information is transmitted in the form of 3D models combined with external controlled technical documents. Based on the 3D design model of the overall unit, the final assembly department built a digital prototype of the general assembly process through lightweight processing and BOM (Bill Of Material) reconstruction (such as adding tooling tools, process protection parts, assembly relationship reconstruction, etc.), and realized Material matching and convenient application of stand-alone equipment. However, for the laying and assembly of flexible ...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/50
CPCG06F30/18G06F2113/16G06F30/15G06F30/20
Inventor 刘国青易旺民闫荣鑫贺文兴刘广通张伟陈畅宇魏鹏许凯冯伟李新宇肖正懿李娜张强
Owner BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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