An automatic interface method for vibration cloud simulation of an avionics product based on ANSYS scripting language

A technology of avionics and scripting language, applied in design optimization/simulation, geometric CAD, electrical digital data processing, etc., can solve the problems of low efficiency and high cost, save hardware cost and labor cost, overcome computing resources and High requirements for technical personnel and the effect of improving computing efficiency

Inactive Publication Date: 2019-04-26
BEIHANG UNIV
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Problems solved by technology

[0005] Aiming at the deficiencies of the prior art, the present invention provides an automatic interface method for performing vibration cloud simulation of avionics products on the cloud. Its appearance can overcome the low efficiency, high cost and high cost of the existing vibration simulation in local calculation. The lack of high requirements for technical personnel makes the vibration simulation of avionics products more efficient, saves costs, and is easy to promote, thereby improving the reliability level of avionics products

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  • An automatic interface method for vibration cloud simulation of an avionics product based on ANSYS scripting language
  • An automatic interface method for vibration cloud simulation of an avionics product based on ANSYS scripting language
  • An automatic interface method for vibration cloud simulation of an avionics product based on ANSYS scripting language

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Embodiment Construction

[0048] The general flow of an automatic interface method for vibration cloud simulation of avionics products based on the ANSYS scripting language claimed in this application is as follows: figure 1 Shown, below will carry out detailed explanation according to specific embodiment, its concrete steps are as follows:

[0049] Step 1. Open the visualization interface of the vibration cloud simulation of the local avionics product, and input the local address of the 3D geometric model of the avionics product, the material parameters of the avionics product for vibration simulation analysis, fixed constraint position, load PSD spectrum value and direction, and the user selects the analysis type according to the working environment of the avionics product; after all the input is completed, the input data is uploaded to the cloud.

[0050] The visualization interface of local avionics product vibration cloud simulation includes 3D geometric model display area, geometric model label a...

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Abstract

The invention discloses an automatic interface method for vibration cloud simulation of an avionics product based on ANSYS scripting language. The method comprises the following steps: inputting a 3Dgeometric model local address, material parameters, fixed restraint position, a load PSD spectrum value, a direction and an analysis type in a local visual interface, ; uploading data to the cloud end, importing ANSYS work simulation software at the cloud end into the 3D geometric model; giving material parameters to a 3D geometric model, updating and meshing the 3D geometric model, then applyingmodal boundary conditions, then performing post-processing of modal analysis, selecting one of random vibration analysis, harmonic response analysis and transient analysis according to a user, then applying different loads, and correspondingly performing post-processing. The cloud platform is used for simulation, the simulation efficiency is improved, and aviation electronic product fault behaviorsimulation and reliability prediction are rapidly and accurately conducted.

Description

technical field [0001] The invention belongs to the technical field of stress simulation of aviation products, and in particular relates to an automatic interface method for vibration cloud simulation of aviation electronic products based on ANSYS script language. Background technique [0002] Avionics products are generally composed of various electronic systems with independent functions, such as flight control systems, navigation systems, etc. They are the brains that control the operation of aircraft, and their reliability has always been valued. The structure of avionics products is roughly composed of chassis, circuit boards, components on them, and connecting parts. During the mission process, it is affected by temperature, vibration, air pressure, etc. At present, stress simulation methods are usually used to ensure its performance in various environments. reliability. Vibration simulation is a kind of stress simulation method, which is used to simulate the vibratio...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/50
CPCG06F30/15G06F30/23G06F2119/06Y02T90/00
Inventor 陈颖方家玥康锐
Owner BEIHANG UNIV
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