| 加力燃烧室壁温测量试验研究 |
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| 引用本文： | 季鹤鸣,王乃绪,邵万仁.加力燃烧室壁温测量试验研究[J].燃气涡轮试验与研究,2007,20(3):39-41. |
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| 作者姓名： | 季鹤鸣 王乃绪 邵万仁 |
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| 作者单位： | 沈阳航空发动机设计所,辽宁,沈阳,110015 |
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| 基金项目： | 致谢：感谢张兴高工、康丽华同志在壁温测量试验研究工作中所做的大量工作! |
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| 摘 要： | 加力燃烧室燃烧段的壁温对飞机和发动机的安全关系重大,单靠数值计算是很不够的,目前主要靠测试取得。燃烧段通常是双层壁,加风罩则为三层。本文介绍了内外壁和风罩的温度测量方法及其试验研究。该方法对加力燃烧室的研制具有重要意义,无论是对于新机还是批生产发动机都有重要的参考价值。
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| 关 键 词： | 涡轮喷气发动机 加力燃烧室 加力试验 壁温测量 |
| 文章编号： | 1672-2620（2007）03-0039-03 |
| 修稿时间： | 2007-01-29 |
Experimental Investigation of Temperature Measurement on the Wall of an Afterburner |
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| JI He-ming,WANG Nai-xu,SHAO Wan-ren.Experimental Investigation of Temperature Measurement on the Wall of an Afterburner[J].Gas Turbine Experiment and Research,2007,20(3):39-41. |
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| Authors: | JI He-ming WANG Nai-xu SHAO Wan-ren |
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| Institution: | Shenyang Aeroengine Research Institute, Shenyang 110015, China |
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| Abstract: | The wall temperature of combustion section for an afterburner is significantly related to the safety of an aircraft and aeroengine.It will be not enough if only relying on the numerical calculation.The data currently used is mainly obtained from instrumentation.The combustion section generally consists of double-layer walls,with an additional ventilator jacket together being three layers.Measurement method and test investigation of temperature for the inner/outer walls and jacket are described in the paper.The method is of great importance to the development of afterburner.It is an important reference to both new engine and engine in production. |
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| Keywords: | turbine jet engine afterburner afterburner experiment wall temperature measuremen |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
