A 3D model parameter inspection system based on Creo software

Through the three-dimensional model parameter inspection system based on Creo software, the three-dimensional model parameters of solid rocket engines are automatically extracted and inspected, and the missed parameters and errors in traditional methods are solved, and efficient and accurate parameter filling and modification are achieved, and solid rocket engines are supported. rapid design and informatization development.

CN113392465BActive Publication Date: 2024-12-17INNER MONGOLIA INST OF POWER MASCH
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Patent Information

Application Number
CN202110467622.5
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2021-04-28
Publication Date
2024-12-17
Estimated Expiration
2041-04-28

AI Technical Summary

Technical Problem

Traditional methods are used to fill in and modify the three-dimensional model parameters of solid rocket engines, and repeated operations are prone to missed parameters, resulting in high probability of wasting time and filling incorrectly, and lack of efficient automation solutions.

Method used

Design a three-dimensional model parameter inspection system based on Creo software, including automatic extraction module and inspection rule setting module, automatically extract and display the three-dimensional model parameters of solid rocket engines through the interface, reduce manual operations, and improve the accuracy of parameter filling and modification.

Benefits of technology

It greatly improves the efficiency and accuracy of filling or modifying solid rocket engine parameters, saves time, reduces manpower and material investment, and supports the informatization development of solid engines.

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Abstract

The present invention relates to the field of digital design of aerospace products, and specifically to a three-dimensional model parameter inspection system based on Creo software. It comprises: a solid rocket engine three-dimensional model parameter automatic extraction module, which is used to extract the solid rocket engine three-dimensional model parameters into this software without opening the three-dimensional model. The interface is mainly composed of model selection mode, model selection, and three-dimensional model display area; a solid rocket engine three-dimensional model parameter inspection rule setting module, which is mainly used to add or modify parameters in the solid rocket engine three-dimensional model. The interface is mainly composed of inspection rule management, attribute setting, and attribute operation. The present invention extracts the parameters of solid rocket engine parts and components, and encapsulates and integrates them into a whole to form a professional process software, so that the data of solid rocket engine model parameters are automatically transmitted, which greatly improves the efficiency and accuracy of filling in or modifying solid rocket engine parameters, and achieves the goal of rapid design.
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Description

Technical Field

[0001] The present invention relates to the field of digital design of aerospace products, and in particular to a three-dimensional model parameter inspection system based on Creo software. Background Art

[0002] In the solid rocket engine engineering development process, the traditional method is to open the 3D model one by one, then open the parts or component parameter list, add and modify the parameters one by one, and finally save them; the traditional method is slow, time-consuming and prone to errors.

[0003] In view of the above reasons, the present invention provides a three-dimensional model parameter checking software based on Creo software, which greatly improves the efficiency and accuracy of filling in or modifying the model parameters of solid rocket engines, thereby saving a lot of time for the structural design of solid rocket engines.

[0004] Currently, operations are mainly performed by opening 3D models one by one manually, and have not been integrated into a general software.

[0005] There are many disadvantages in using the existing technology: First, the filling and modification of the parameters of the solid rocket engine 3D model requires opening each 3D model, completing the filling or modification of the parameters of a 3D model, and then saving it. The solid rocket engine 3D model is composed of a large number of parts and components, so this method is very time-consuming; secondly, in the process of opening the 3D model parameter operation, it is easy to miss the filling or modification of certain parameters, resulting in the lack of parameters in the subsequent structural model, causing repeated work and wasting time; finally, in the process of editing the 3D model parameters, the probability of incorrect parameter filling is increased. Summary of the invention

[0006] Technical Problems to be Solved by the Invention

[0007] The present invention provides a 3D model parameter checking system based on Creo software to solve the problems that the filling or modification of certain parameters is easily missed during repeated operations, resulting in the lack of parameters in subsequent structural models, causing repeated work and wasting time, and increasing the probability of incorrect parameter filling during the 3D model parameter editing process.

[0008] Technical solutions adopted to solve technical problems

[0009] A 3D model parameter inspection system based on Creo software, comprising:

[0010] The solid rocket engine 3D model parameter automatic extraction module is used to extract the solid rocket engine 3D model parameters into this software without opening the 3D model. The interface mainly consists of model selection mode, model selection, and 3D model display area.

[0011] The solid rocket engine 3D model parameter inspection rule setting module is mainly used to add or modify parameters in the solid rocket engine 3D model. The interface is mainly composed of inspection rule management, attribute setting and attribute operation.

[0012] Furthermore, the solid rocket engine three-dimensional model parameter automatic extraction module must set the model selection mode in the upper left corner of the module interface. In the upper part of the interface, "Model Selection" must be set to one of the modes. In the middle of the interface, the parameter display area extracts the solid rocket engine three-dimensional model parameters and displays them in that part.

[0013] Furthermore, in the solid rocket engine three-dimensional model parameter inspection rule setting module, the upper part of the interface requires the setting of parts or components, the middle part of the interface can adjust the required parameters of the three-dimensional model, and the lower part of the interface can increase the three-dimensional model parameters.

[0014] Beneficial Effects

[0015] According to the development trend of high efficiency and informatization in the domestic solid rocket engine industry and based on the needs of the solid engine development process, the present invention has developed a three-dimensional model parameter inspection software based on Creo software, striving to improve the efficiency of three-dimensional structural design of solid rocket engines, saving manpower and material resources, and having important guiding significance for the improvement and development of solid engine informatization; the present invention extracts the parameters of solid rocket engine parts and components, and encapsulates and integrates them into an organic whole to form software oriented to professional processes, so that the data of solid rocket engine model parameters are automatically transmitted, which greatly improves the efficiency and accuracy of filling in or modifying solid rocket engine parameters and achieves the goal of rapid design. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] Figure 1 :Overall software architecture,

[0017] Figure 2 :Automatic extraction module of solid rocket engine 3D model parameters,

[0018] Figure 3 : Solid rocket engine three-dimensional model parameter inspection rule setting module,

[0019] Figure 4 : Parameter inspection results of solid rocket engine 3D model,

[0020] Figure 5 : Results after parameter repair of solid rocket engine 3D model. DETAILED DESCRIPTION

[0021] According to the development trend of efficiency and informatization in the domestic solid rocket engine industry and based on the needs of the solid engine development process, the present invention has developed a three-dimensional model parameter inspection software based on Creo software, striving to improve the efficiency of three-dimensional structure design of solid rocket engines, saving manpower and material resources, and has important guiding significance for the improvement and development of solid engine informatization.

[0022] In order to make the purpose, features and advantages of the technical solution proposed in the present invention more obvious and easy to understand, the technical solution proposed in the present invention will be clearly and completely described below in conjunction with the accompanying drawings. Obviously, the described embodiments are only part of the embodiments of the proposed technical solution, rather than all the embodiments. Based on the embodiments in the present invention, all other embodiments obtained by ordinary technicians in this field without making creative work belong to the scope of protection of the present invention.

[0023] The present invention provides a three-dimensional model parameter checking software based on Creo software, which includes the functions of checking, editing and modifying the parameters of solid rocket engine components, and guides engineering and technical personnel to complete the filling and modification of the three-dimensional model parameters of the solid rocket engine through process wizards, friendly interface and other operations.

[0024] like Figure 1 As shown in the figure, the overall framework of the solid rocket engine 3D model parameter inspection software. The software is divided into two modules: the solid rocket engine 3D model parameter automatic extraction module and the parameter inspection rule setting module. The solid rocket engine 3D model parameter automatic extraction module is used to extract the solid rocket engine 3D model parameters into this software without opening the 3D model. The parameter inspection rule setting module is mainly used to add or modify parameters in the solid rocket engine 3D model.

[0025] like Figure 2 As shown in the figure, the main interface of the solid rocket engine 3D model parameter automatic extraction module. This interface mainly consists of model selection mode, model selection, and 3D model display area. In the upper left corner of the interface, the model selection mode must be set. In the upper part of the interface, "Model selection" must set one of the modes. In the middle of the interface, the parameter display area extracts the solid rocket engine 3D model parameters and displays them in this part.

[0026] like Figure 3 As shown, the solid rocket engine 3D model parameter inspection rule setting module. This interface mainly consists of inspection rule management, attribute setting and attribute operation. In the upper part of this interface, parts or components must be set. In the middle of this interface, the required parameters of the 3D model can be adjusted. In the lower part of this interface, 3D model parameters can be added.

[0027] The automatic extraction module of solid rocket engine three-dimensional model parameters, ① first start the calculation software and enter the main interface of the software system; ② start the selection mode; if you select "current model", the solid rocket engine three-dimensional model parameters are extracted to the parameter display area; if you select "other models", activate the model selection module; ③ start the model selection module, you can select a single model or multiple models, and the solid rocket engine three-dimensional model parameters are extracted to the parameter display area.

[0028] Solid rocket engine three-dimensional model parameter inspection rule setting module: ① First start the calculation software and enter the main interface of the software system; ② Start the inspection rule setting module and input the parameters required for the solid rocket engine three-dimensional model; ③ Save the parameter settings.

[0029] The following is a clear and complete description of the technical solution of the present invention in conjunction with the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, rather than all the obtained embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field belong to the scope of protection of the present invention.

[0030] Take the parameter inspection of a solid rocket engine 3D model as an example. The first step is to start the software system; the second step is to start the solid rocket engine 3D model parameter automatic extraction module, select the solid rocket engine 3D model required, see Figure 1 and Figure 2 , and trigger the inspection rule setting module; the third step is to enter the required parameters and trigger the "Save Parameter Settings" button, see Figure 3 ; Step 4, trigger "Start Checking Model" to obtain the filling status of 3D model parameters, and "Checking Information" shows that it has failed. Figure 4 , Step 5, enter the correct parameters of the solid rocket engine 3D model in the prompt display area, and trigger "Repair model properties" and "Save current model", and "Check information" is displayed as passed, see Figure 5 Finally, complete the parameter filling or change to the solid rocket engine 3D model.

Claims

1. A 3D model parameter inspection system based on Creo software, characterized by: The solid rocket engine 3D model parameter automatic extraction module is used to extract the solid rocket engine 3D model parameters into this software without opening the 3D model. The interface mainly consists of model selection mode, model selection, and 3D model display area. The solid rocket engine 3D model parameter automatic extraction module must set the model selection mode in the upper left corner of the module interface. In the upper part of the interface, the "model selection" must be set to one of the modes. In the middle of the interface, the parameter display area extracts the solid rocket engine 3D model parameters and displays them in that area. The solid rocket engine three-dimensional model parameter inspection rule setting module is mainly used to add or modify parameters in the solid rocket engine three-dimensional model. The interface is mainly composed of inspection rule management, attribute setting and attribute operation; the solid rocket engine three-dimensional model parameter inspection rule setting module, the upper part of the interface, must set parts or components, the middle part of the interface, the required parameters of the three-dimensional model can be adjusted, and the lower part of the interface can add three-dimensional model parameters.