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Design and analysis of the federal aviation administration next generation fire test burner.

机译:联邦航空局下一代防火测试燃烧器的设计和分析。

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摘要

The United States Federal Aviation Administration makes use of threat-based fire test methods for the certification of aircraft cabin materials to enhance the level of safety in the event of an in-flight or post-crash fire on a transport airplane. The global nature of the aviation industry results in these test methods being performed at hundreds of laboratories around the world; in some cases testing identical materials at multiple labs but yielding different results. Maintenance of this standard for an elevated level of safety requires that the test methods be as well defined as possible, necessitating a comprehensive understanding of critical test method parameters. The tests have evolved from simple Bunsen burner material tests to larger, more complicated apparatuses, requiring greater understanding of the device for proper application. The FAA specifies a modified home heating oil burner to simulate the effects of large, intense fires for testing of aircraft seat cushions, cargo compartment liners, power plant components, and thermal acoustic insulation. Recently, the FAA has developed a Next Generation (NexGen) Fire Test burner to replace the original oil burner that has become commercially unavailable. The NexGen burner design is based on the original oil burner but with more precise control of the air and fuel flow rates with the addition of a sonic nozzle and a pressurized fuel system. Knowledge of the fundamental flow properties created by various burner configurations is desired to develop an updated and standardized burner configuration for use around the world for aircraft materials fire testing and airplane certification. To that end, the NexGen fire test burner was analyzed with Particle Image Velocimetry (PIV) to resolve the non-reacting exit flow field and determine the influence of the configuration of burner components. The correlation between the measured flow fields and the standard burner performance metrics of flame temperature and burnthrough time was studied. Potential design improvements were also evaluated that could simplify burner set up and operation.
机译:美国联邦航空局使用基于威胁的防火测试方法对机舱材料进行认证,以提高运输飞机在飞行中或坠毁后着火时的安全水平。航空业的全球性导致在全球数百个实验室中执行这些测试方法。在某些情况下,要在多个实验室测试相同的材料,但会得出不同的结果。为了提高安全性而维持此标准要求对测试方法进行尽可能详细的定义,从而有必要全面了解关键的测试方法参数。测试已经从简单的本生灯测试器发展到更大,更复杂的设备,需要对设备进行更好的理解才能正确使用。 FAA指定了一种改进的家用取暖油燃烧器,以模拟大火的影响,以测试飞机座垫,货舱内衬,发电厂组件和隔热隔音材料。最近,FAA已开发了下一代(NexGen)耐火测试燃烧器,以取代商业上无法获得的原始燃油燃烧器。 NexGen燃烧器的设计基于原始的燃油燃烧器,但通过添加声波喷嘴和加压燃料系统,可以更精确地控制空气和燃料的流量。需要了解由各种燃烧器配置产生的基本流动特性,以开发更新和标准化的燃烧器配置,以在世界范围内用于飞机材料着火测试和飞机认证。为此,使用粒子图像测速(PIV)技术对NexGen耐火试验燃烧器进行了分析,以解决无反应的出口流场并确定燃烧器组件的配置的影响。研究了测得的流场与火焰温度和燃烧时间的标准燃烧器性能指标之间的相关性。还评估了可能的设计改进,以简化燃烧器的设置和操作。

著录项

  • 作者

    Ochs, Robert Ian.;

  • 作者单位

    Rutgers The State University of New Jersey - New Brunswick.;

  • 授予单位 Rutgers The State University of New Jersey - New Brunswick.;
  • 学科 Engineering Mechanical.;Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2013
  • 页码 240 p.
  • 总页数 240
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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