A platform system for the integrated design of aircraft structure and function based on uncertain optimization

An aircraft, uncertainty technology, applied in design optimization/simulation, instruments, calculations, etc., can solve problems such as difficult to use engineering applications, and achieve the effect of easy modification and maintenance

Active Publication Date: 2019-08-13
宁波智正伟盈信息科技有限公司
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Problems solved by technology

From the current application point of view, this method is suitable for theoretical research, but difficult for engineering applications
In terms of multidisciplinary optimization considering uncertain factors, there is no mature and practical software to choose from, and there is no related software integration platform for professional uncertainty analysis. Therefore, the practical application of uncertain multidisciplinary optimization design technology has arisen negative effect

Method used

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  • A platform system for the integrated design of aircraft structure and function based on uncertain optimization
  • A platform system for the integrated design of aircraft structure and function based on uncertain optimization
  • A platform system for the integrated design of aircraft structure and function based on uncertain optimization

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Embodiment Construction

[0095] The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments.

[0096] Such as figure 1 As can be seen from the system frame diagram shown, the present invention is an aircraft structure-function integrated design platform system based on uncertain optimization, which consists of an aerodynamic shape design optimization module, a thermal protection system (front cabin) design optimization module, a thermal protection system (wing ) design optimization module, composite material cold structure design optimization module, wing heat-resistant integrated structure optimization module, wing aerodynamic / structure / thermal coupling optimization analysis module, basic database module and system framework program for integrating the above modules . The overall implementation process is as follows:

[0097] (1) Aerodynamic shape design optimization module: it is used to realize the deterministic analysis and optimiz...

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Abstract

The invention discloses an aircraft structure function integrated design platform system based on uncertain optimization. The aircraft structure function integrated design platform system is composed of a system framework program and seven sub-modules comprising a pneumatic shape design optimization module, a forecabin thermal protection system design optimization module, a wing thermal protection system design optimization module, a composite cooled structure design optimization module, a wing heat-protection load-bearing integrated structure optimization module, a wing pneumatic / structure / thermal coupling optimization analysis module and a basic database module. An integrated design of the platform is achieved on the basis that certain analysis optimization and uncertain analysis optimization of system functions of each structure are carried out. The platform integrates an aerodynamic force / heat database, an integrated model database and various algorithms into the system, and a convenient tool is provided for non-professionals to carry out an integrated design.

Description

technical field [0001] The invention relates to an aircraft structure-function integrated design platform system based on uncertain optimization, and belongs to the technical field of uncertain multidisciplinary optimal design. Background technique [0002] Uncertainty multidisciplinary optimization design technology is complex and computationally complex due to the inherent loop characteristics of data transmission. Uncertainty is coupled and propagated in multiple discipline subsystems, making multidisciplinary optimization design based on uncertainty The practical application of it has become a challenging topic. [0003] At this stage, the uncertain structure-function optimization design of structures is mostly realized by integrating the required software and algorithms in a general multidisciplinary optimization design environment. [0004] The multidisciplinary optimization design environment refers to the design computing environment that integrates the analysis mod...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F17/50
CPCG06F30/15G06F30/23Y02T90/00
Inventor 罗明强王晓军王睿星韩一铭邱志平
Owner 宁波智正伟盈信息科技有限公司
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