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Man-machine hybrid enhanced aircraft structural member design method based on instance reasoning

A technology of aircraft structural parts and case-by-case reasoning, which is applied to computer parts, calculation, image data processing, etc., can solve the time-consuming and labor-intensive pass rate of similar model parts, so as to save modeling time, shorten development cycle, and improve modeling efficiency effect

Pending Publication Date: 2022-05-27
NORTHEASTERN UNIV
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  • Abstract
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  • Application Information

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Problems solved by technology

[0007] The purpose of the present invention is to provide a human-computer hybrid enhanced aircraft structural parts design method based on case-based reasoning, in order to solve the time-consuming and labor-intensive and qualified rate problems of creating a large number of similar model parts

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  • Man-machine hybrid enhanced aircraft structural member design method based on instance reasoning
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  • Man-machine hybrid enhanced aircraft structural member design method based on instance reasoning

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Embodiment Construction

[0038] The present invention will be further described in detail below in conjunction with the accompanying drawings. The drawings described here are a part of the present application, and are used to further explain the present invention, but do not constitute a limitation of the present invention.

[0039] (1) Step 1, according to the requirements of the components in the existing design requirements, the designer analyzes its needs in terms of bearing capacity, manufacturing cost, life and its working conditions, from machining parts, sheet metal parts Among the three categories of parts and components, the rudder surface suspension joints in the frame parts are obtained, because the rudder surface suspension joints also include single-head suspension joints, double-head suspension joints, three-head suspension joints and rudder surfaces. Suspension joints, and there are differences in the dimensions of the same type of suspension joints, so further reasoning is required to...

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Abstract

The invention provides a man-machine hybrid enhanced aircraft structural member design method based on instance reasoning, which comprises the following steps: step 1, according to structural member design requirements, designers clearly design the type and other information of a target part; 2, after the information input in the step 1 is received, a computer conducts reasoning matching of similar cases in an instance library, and according to an instance reasoning algorithm, a similarity value is output; and 3, calling out examples with certain similarity deduced by a computer from the example library, directly using the examples if the examples directly meet the requirements, otherwise, performing deformation design by a designer according to the requirements, finally outputting parts meeting the requirements, and adding the parts into the example library to add more reference applications for subsequent example reasoning. The workload of designers can be reduced, and the design period is shortened. In actual detection, the modeling time can be saved by more than 80% under the same workload.

Description

technical field [0001] The invention belongs to the field of computer-aided design of aircraft structural parts, and particularly relates to a human-machine hybrid enhanced aircraft structural part design method based on case-based reasoning. Background technique [0002] With the development of the aviation industry, my country has put forward higher requirements for the design quality and design efficiency of aircraft structural parts. In the process of product development, new technologies such as computer-aided design are inevitably used to shorten the development cycle, thereby reducing costs and enhancing Competitiveness. [0003] China's aviation industry is at a critical stage of overtaking with the world's aviation powerhouse, and shortening the development cycle of aircraft is an inevitable choice in this process. There are many similar parts on the aircraft structure. When such similar parts are modeled by CATIA software, the steps and processes are exactly the sa...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/15G06F30/17G06K9/62G06T17/00
CPCG06F30/15G06T17/00G06F30/17G06F18/22Y02T90/00
Inventor 郝博王杰刘芳尹兴超张鹏汪万炯王明阳王婵娟袁辉
Owner NORTHEASTERN UNIV
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