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Design methodology for wing trailing edge device mechanisms

机译:机翼后缘装置机构的设计方法

摘要

Over the last few decades the design of high lift devices has become a veryimportant part of the total aircraft design process. Reviews of the design processare performed on a regular basis, with the intent to improve and optimize thedesign process.This thesis describes a new and innovative methodology for the design andevaluation of mechanisms for Trailing Edge High-Lift devices. The initial researchreviewed existing High-Lift device design methodologies and current flap systemsused on existing commercial transport aircraft. This revealed the need for a designmethodology that could improve the design process of High-Lift devices, movingaway from the conventional "trial and error" design approach, and cover a widerrange of design attributes. This new methodology includes the use of theinnovative design tool called SYNAMEC. This is a state-of-the-art engineeringdesign tool for the synthesis and optimizations of aeronautical mechanisms. Thenew multidisciplinary design methodology also looks into issues not usuallyassociated with the initial stages of the design process, such as Maintainability,Reliability, Weight and Cost.The availability of the SYNAMEC design tool and its ability to perform Synthesisand Optimization of mechanisms led to it being used as an important module inthe development of the new design methodology. The SYNAMEC tool allowsdesigners to assess more mechanisms in a given time than the traditional designmethodologies.A validation of the new methodology was performed and showed that creditableresults were achieved.A case study was performed on the ATRA-Advance Transport Regional Aircraft,a Cranfield University design project, to apply the design methodology and selectfrom within a group of viable solutions the most suitable type of mechanism for theVariable Camber Wing concept initially defined for the aircraft. The results showthat the most appropriate mechanism type for the ATRA Variable Camber Wing isthe Link /Track Mechanism. It also demonstrated how a wide range of designattributes can now be considered at a much earlier stage of the design.
机译:在过去的几十年中,高升力设备的设计已成为整个飞机设计过程中非常重要的一部分。定期对设计过程进行审查,以期改进和优化设计过程。本文介绍了一种新的创新方法,用于后缘高举装置的设计和评估。最初的研究回顾了现有的高空设备设计方法和在现有商用运输飞机上使用的当前襟翼系统。这表明需要一种可以改进High-Lift器件设计过程的设计方法,以摆脱传统的“试错法”设计方法,并涵盖更广泛的设计属性。这种新方法包括使用名为SYNAMEC的创新设计工具。这是用于综合和优化航空机制的最先进的工程设计工具。新的多学科设计方法还研究了通常与设计过程的初始阶段不相关的问题,例如可维护性,可靠性,重量和成本。SYNAMEC设计工具的可用性及其执行综合和机制优化的能力导致其被使用。作为开发新设计方法的重要模块。与传统的设计方法相比,SYNAMEC工具可以使设计人员在给定的时间内评估更多的机制。对新方法进行了验证,并显示了可信赖的结果。对克兰菲尔德大学设计的ATRA-先进运输支线飞机进行了案例研究项目,以应用设计方法并从一组可行的解决方案中选择最适合最初为飞机定义的可变弧度机翼概念的机械类型。结果表明,ATRA可变弯度机翼最合适的机构类型是连杆/履带机构。它还说明了如何在设计的早期阶段就可以考虑各种设计属性。

著录项

  • 作者

    Martins Pires Rui Miguel;

  • 作者单位
  • 年度 2007
  • 总页数
  • 原文格式 PDF
  • 正文语种 {"code":"en","name":"English","id":9}
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