首页> 外文会议>2003 ASME(American Society of Mechanical Engineers) Turbo Expo; Jun 16-19, 2003; Atlanta, Georgia >DETAILED INVESTIGATION OF HEAT FLUX MEASUREMENTS MADE IN A STANDARD PROPANE-AIR FIRE-CERTIFICATION BURNER COMPARED TO LEVELS DERIVED FROM A LOW-TEMPERATURE ANALOGUE BURNER
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DETAILED INVESTIGATION OF HEAT FLUX MEASUREMENTS MADE IN A STANDARD PROPANE-AIR FIRE-CERTIFICATION BURNER COMPARED TO LEVELS DERIVED FROM A LOW-TEMPERATURE ANALOGUE BURNER

机译:标准丙烷-空气失火鉴定燃烧器中的热通量测量值的详细调查,与从低温模拟燃烧器得出的水平相比

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This paper presents detailed heat flux measurements to a flat plate from an ISO2685 standard, large propane fuelled burner used throughout the industry in aero-engine fire-certification. The authors have developed a custom-built heat transfer gauge to measure the heat flux from the burner under isothermal wall conditions. The heat flux from the standard burner is normally calibrated using either a water-cooled copper rube or a Gardon gauge, each positioned at a single location. There are no reports in the literature of a detailed survey of heat flux distribution for the burner and the results are therefore of great interest to thermal engineers. These measurements provide benchmark data to allow the heat flux distribution from the ISO burner to be compared to levels derived from the low-temperature analogue burner developed by the authors. The analogue burner uses liquid crystals to measure heat transfer coefficient and adiabatic wall temperature on scale models of engine components and provides key data to facilitate the successful design of components used in fire zones. The objective of this paper is to further validate the low-temperature analogue burner technique developed by the authors which simulates the standard large propane-air burner for fire-certification in aero engine.
机译:本文介绍了从ISO2685标准,大型丙烷燃料燃烧器到平板的热通量的详细测量结果,该燃烧器在整个行业用于航空发动机防火认证。作者开发了一种定制的传热计,以测量等温壁条件下燃烧器的热通量。来自标准燃烧器的热通量通常使用水冷铜线或Gardon量规进行校准,每个都放置在单个位置。文献中没有关于燃烧器的热通量分布的详细调查的报告,因此,热工对此非常感兴趣。这些测量提供了基准数据,可以将来自ISO燃烧器的热通量分布与由作者开发的低温模拟燃烧器得出的水平进行比较。模拟燃烧器使用液晶来测量发动机部件的比例模型上的传热系数和绝热壁温,并提供关键数据以促进火区中使用的部件的成功设计。本文的目的是进一步验证作者开发的低温模拟燃烧器技术,该技术模拟了标准大型丙烷空气燃烧器,用于航空发动机的防火认证。

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