Thermal characterization of a mercury arc lamp for a projection display system

B. Bush, Shu Li, D. Kelley
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Abstract

Avionics displays that operate in high temperature, low-pressure environments are challenging to design. Since the trend has been to reduce the physical dimensions of the electronics while increasing the effective display area with higher luminance and optical performance, the thermal design of this type of display product is a critical step in the design process. At the heart of one such display product is a high-pressure mercury arc lamp module, comprising of an arc tube and reflector housing. It dissipates roughly 1/3 to 1/2 of the total power in a display enclosure. The methods used to cool a high power light source could have a dramatic effect on the performance and the reliability of the other electrical components within the display enclosure. This paper will discuss the thermal design of the light source, a custom-designed high-pressure mercury arc lamp module for a projection display used in an avionics application. Computational Fluid Dynamics (CFD) was used to characterize the heat transfer path from the plasma arc to the lamp's outer housing and rest of the electronics within the enclosure. A few of the higher end CFD companies have developed plasma capabilities within their codes. These codes typically do not have the functionality to solve electronics box type problems efficiently. On the other hand, the "electronics specific" CFD codes do not have the higher end computational capabilities or the ability to mesh complex geometry. Because of this, both a general purpose and an electronics specific CFD code were used to accurately predict the temperatures in a projection enclosure used for an avionics display. To establish the complete model, a series of optical measurements was conducted on a typical arc tube and real lamp to obtain the critical parameters that are too complicated or impossible to generate by modeling alone. These parameters include the total radiant power of the lamp, radiant power distribution in different wavelength range, and the optical properties of the optical surfaces. Also measured was the temperature distribution of the lamp at predetermined points in well-controlled conditions. This optical and thermal data are used in the modeling process so the model can produce consistent and convergent results.
投影显示系统用汞弧灯的热特性
在高温、低压环境下工作的航空电子显示器的设计具有挑战性。由于目前的趋势是减小电子器件的物理尺寸,同时增加具有更高亮度和光学性能的有效显示面积,因此这类显示产品的热设计是设计过程中的关键步骤。其中一种显示产品的核心是高压汞灯模块,由电弧管和反射罩组成。它大约耗散了显示框总功率的1/3到1/2。用于冷却高功率光源的方法可能对显示框内其他电子元件的性能和可靠性产生巨大影响。本文将讨论光源的热设计,这是一种为航空电子应用中的投影显示器定制的高压汞弧灯模块。计算流体动力学(CFD)用于表征从等离子弧到灯外壳和外壳内其余电子设备的传热路径。一些高端的CFD公司已经在他们的代码中开发了等离子能力。这些代码通常不具备有效解决电子盒类型问题的功能。另一方面,“电子特定”CFD代码不具备高端计算能力或网格复杂几何形状的能力。正因为如此,通用和电子特定的CFD代码都被用于准确预测用于航空电子显示器的投影框中的温度。为了建立完整的模型,对一个典型的弧管和真实的灯进行了一系列的光学测量,获得了单独建模过于复杂或无法生成的关键参数。这些参数包括灯的总辐射功率、不同波长范围内的辐射功率分布以及光学表面的光学特性。在控制良好的条件下,还测量了灯在预定点的温度分布。在建模过程中使用了这些光学和热数据,因此模型可以产生一致和收敛的结果。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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