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Structural design and fabrication techniques of composite unmanned aerial vehicles.

机译:复合无人机的结构设计和制造技术。

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摘要

Popularity of unmanned aerial vehicles has grown substantially in recent years both in the private sector, as well as for government functions. This growth can be attributed largely to the increased performance of the technology that controls these vehicles, as well as decreasing cost and size of this technology. What is sometimes forgotten though, is that the research and advancement of the airframes themselves are equally as important as what is done with them. With current computer-aided design programs, the limits of design optimization can be pushed further than ever before, resulting in lighter and faster airframes that can achieve longer endurances, higher altitudes, and more complex missions. However, realization of a paper design is still limited by the physical restrictions of the real world and the structural constraints associated with it. The purpose of this paper is to not only step through current design and manufacturing processes of composite UAVs at Oklahoma State University, but to also focus on composite spars, utilizing and relating both calculated and empirical data.;Most of the experience gained for this thesis was from the Cessna Longitude project. The Longitude is a 1/8 scale, flying demonstrator Oklahoma State University constructed for Cessna. For the project, Cessna required dynamic flight data for their design process in order to make their 2017 release date. Oklahoma State University was privileged enough to assist Cessna with the mission of supporting the validation of design of their largest business jet to date. This paper will detail the steps of the fabrication process used in construction of the Longitude, as well as several other projects, beginning with structural design, machining, molding, skin layup, and ending with final assembly. Also, attention will be paid specifically towards spar design and testing in effort to ease the design phase. This document is intended to act not only as a further development of current practices, but also as a step-by-step manual for those who aspire to make composite airframes, predominantly the Oklahoma State University MAE students who either are, or will be using these techniques on a daily basis.
机译:近年来,无论是在私营部门还是在政府职能方面,无人驾驶飞行器的普及都已大大增加。这种增长主要归因于控制这些车辆的技术性能的提高,以及该技术成本的降低和尺寸的减小。但是,有时会忘记的是,机身本身的研究和改进与机身的完成同样重要。使用当前的计算机辅助设计程序,可以将设计优化的极限推到前所未有的高度,从而使机身更轻,更快,从而可以实现更长的耐用性,更高的高度和更复杂的任务。但是,纸张设计的实现仍然受到现实世界的物理限制和与之相关的结构限制。本文的目的不仅是逐步了解俄克拉荷马州立大学复合无人机的当前设计和制造过程,而且还要着重于利用和关联计算的和经验的数据来研究复合翼梁。来自塞斯纳经度项目。经度是为塞斯纳建造的1/8比例的飞行演示者俄克拉荷马州立大学。对于该项目,塞斯纳需要在其设计过程中提供动态飞行数据,才能确定其2017年发布日期。俄克拉荷马州立大学非常荣幸地协助塞斯纳完成了迄今为止验证其最大型公务机设计的任务。本文将详细介绍经度以及其他几个项目的制造过程,这些步骤将从结构设计,机加工,成型,蒙皮铺设到最终装配结束。另外,将特别关注梁的设计和测试,以简化设计阶段。本文档的目的不仅是作为当前实践的进一步发展,而且还为有志于制造复合机体的人(主要是正在或将要使用俄克拉荷马州立大学MAE的学生)提供循序渐进的手册。这些技术每天都有。

著录项

  • 作者

    Hunt, Daniel Stephen.;

  • 作者单位

    Oklahoma State University.;

  • 授予单位 Oklahoma State University.;
  • 学科 Aerospace engineering.;Materials science.;Mechanical engineering.
  • 学位 M.S.
  • 年度 2014
  • 页码 203 p.
  • 总页数 203
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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