首页> 外文学位 >Conceptual design optimization for military helicopter maneuverability and agility.
【24h】

Conceptual design optimization for military helicopter maneuverability and agility.

机译:军用直升机机动性和敏捷性的概念设计优化。

获取原文
获取原文并翻译 | 示例

摘要

Even though the government has recently shown interest for more affordable systems in future military endeavors, the ultimate requirement in tomorrow's battlefield for military helicopters, has been and always will be, maneuverability and agility.;However, the helicopter conceptual design process has traditionally focused on the characteristics of weight, performance, and cost. Maneuverability and agility have seldom, if ever, been a conceptual design driver. Rotorcraft maneuverability and agility attributes should be "designed-in" from the beginning, rather than being treated as fall-outs from more traditional design approaches. The obvious problem in the traditional design approach is the short conceptual design phase. This places an unequal distribution of disciplines which does not allow the use of design freedom to improve quality and integrate disciplines for optimization.;The primary objective of this research is to develop a new approach to integrate rotorcraft maneuverability and agility into a generic conceptual design using an Integrated Product/Process Development methodology. To accomplish this objective successfully, adequate tools should be developed simultaneously.;This research was accomplished by using a unique approach to conceptual and early preliminary aircraft design. The system synthesis and optimization were achieved using statistical methods, specifically Design of Experiments and Response Surface Methodology and using a newly integrated computer program, Preliminary Design, Performance, Stability, and Control (PDPSC) program.;Maneuverability and agility parameters were selected based on mission roles. The existing three included programs, which capture the selected parameters, were modified and integrated in order to more efficiently and accurately search the design space for optimum configurations.;Using DOE/RSM, the optimum configuration was determined and the maneuverability and agility were compared with the baseline values. The handling qualities were also analyzed by using stability and control information obtained from PDPSC. This kind of process and information are very evolutionary for the concept of traditional design. The modern approach towards design should involve a constructional shift of several concepts to an earlier phase. The designer can obtain the information during the conceptual design phase which allows this system to be used throughout the entire design process.;This research demonstrated the increment of maneuverability and agility quantitatively. Through this research, a methodology has been created to conclude that maneuverability and agility can be evaluated during the conceptual design phase.
机译:即使政府最近对未来的军事行动表现出了对更实惠的系统的兴趣,但在明天的战场上,对军用直升机的最终要求一直是,并将始终是机动性和敏捷性。重量,性能和成本的特征。机动性和敏捷性很少(如果有的话)成为概念设计的驱动力。旋翼飞机的机动性和敏捷性属性应该从一开始就进行“设计”,而不是被视为更传统的设计方法的结果。传统设计方法中明显的问题是概念设计阶段短。这会导致学科分配不均,从而不允许利用设计自由来提高质量并整合学科以进行优化。;本研究的主要目的是开发一种新方法,将旋翼飞机的可操纵性和敏捷性整合到通用的概念设计中,方法是使用一种集成的产品/流程开发方法。为了成功实现这一目标,应同时开发适当的工具。该研究是通过采用独特的方法对概念飞机和早期飞机进行初步设计而完成的。该系统的综合和优化是通过统计方法实现的,特别是通过实验设计和响应面方法学,以及使用新集成的计算机程序(初步设计,性能,稳定性和控制(PDPSC)程序);基于以下因素选择了可操纵性和敏捷性参数:任务角色。修改并集成了现有的三个程序,这些程序捕获了选定的参数,以便更高效,准确地搜索设计空间以获取最佳配置。;使用DOE / RSM确定最佳配置,并与可操作性和敏捷性进行比较。基线值。还通过使用从PDPSC获得的稳定性和控制信息来分析处理质量。对于传统设计的概念而言,这种过程和信息是非常进化的。现代的设计方法应涉及将几个概念的结构性转变为早期阶段。设计者可以在概念设计阶段获得信息,从而可以在整个设计过程中使用该系统。本研究定量地证明了可操作性和敏捷性的提高。通过这项研究,已经创建了一种方法,可以得出结论,可以在概念设计阶段评估可操作性和敏捷性。

著录项

  • 作者

    Kim, Ho-Sik.;

  • 作者单位

    Georgia Institute of Technology.;

  • 授予单位 Georgia Institute of Technology.;
  • 学科 Aerospace engineering.
  • 学位 Ph.D.
  • 年度 1997
  • 页码 170 p.
  • 总页数 170
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号