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A design pathfinder with material correlation points for inflatable systems.

机译:具有充气系统材料关联点的设计探路者。

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摘要

The incorporation of inflatable structures into aerospace systems can produce significant advantages in stowed volume to mechanical effectiveness and overall weight. Many applications of these ultra-lightweight systems are designed to precisely control internal or external surfaces, or both, to achieve desired performance. The modeling of these structures becomes complex due to the material nonlinearities inherent to the majority of construction materials used in inflatable structures. Furthermore, accurately modeling the response and behavior of the interfacing boundaries that are common to many inflatable systems will lead to better understanding of the entire class of structures. The research presented involved using nonlinear finite element simulations correlated with photogrammetry testing to develop a procedure for defining material properties for commercially available polyurethane-coated woven nylon fabric, which is representative of coated materials that have been proven materials for use in many inflatable systems. Further, the new material model was used to design and develop an inflatable pathfinder system which employs only internal pressure to control an assembly of internal membranes. This canonical inflatable system will be used for exploration and development of general understanding of efficient design methodology and analysis of future systems. Canonical structures are incorporated into the design of the phased pathfinder system to allow for more universal insight. Nonlinear finite element simulations were performed to evaluate the effect of various boundary conditions, loading configurations, and material orientations on the geometric precision of geometries representing typical internal/external surfaces commonly incorporated into inflatable pathfinder system. The response of the inflatable system to possible damage was also studied using nonlinear finite element simulations. Development of a correlated material model for analysis of the inflatable pathfinder system has improved the efficiency of design and analysis techniques of future inflatable structures.;KEYWORDS: Nonlinear Finite Element, Inflatable Structures, Gossamer Space Systems, Photogrammetry Measurements, Coated Woven Fabric.
机译:将可充气结构结合到航空航天系统中可在体积,机械效率和总重量方面产生显着优势。这些超轻量级系统的许多应用旨在精确控制内表面或外表面,或同时控制这两者,以实现所需的性能。由于可充气结构中使用的大多数建筑材料固有的材料非线性,这些结构的建模变得复杂。此外,对许多充气系统共有的接口边界的响应和行为进行准确建模,将有助于更好地理解整个结构类别。提出的研究涉及使用与摄影测量相关的非线性有限元模拟,以开发一种定义商购聚氨酯涂层尼龙编织材料的材料性能的程序,该材料代表了已被证明可用于许多充气系统的涂层材料。此外,新材料模型用于设计和开发可充气探路系统,该系统仅采用内部压力来控制内部膜的组装。这种规范的充气系统将用于探索和发展对有效设计方法的一般理解以及对未来系统的分析。规范结构被合并到分阶段探路器系统的设计中,以实现更广泛的洞察力。进行了非线性有限元模拟,以评估各种边界条件,载荷配置和材料取向对代表通常合并到充气探路者系统中的典型内/外表面的几何形状的几何精度的影响。还使用非线性有限元模拟研究了充气系统对可能损坏的响应。开发相关材料模型以分析可充气探路者系统可提高未来充气结构的设计和分析技术的效率。关键词:非线性有限元,可充气结构,Gossamer空间系统,摄影测量,涂层机织织物。

著录项

  • 作者

    Fulcher, Jared Terrell.;

  • 作者单位

    University of Kentucky.;

  • 授予单位 University of Kentucky.;
  • 学科 Aerospace engineering.;Mechanical engineering.
  • 学位 Ph.D.
  • 年度 2014
  • 页码 248 p.
  • 总页数 248
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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