航空发动机弧齿锥齿轮着色印痕技术研究 |
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引用本文: | 王辉,王志哲,周思之.航空发动机弧齿锥齿轮着色印痕技术研究[J].航空发动机,2010,36(1):49-52. |
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作者姓名: | 王辉 王志哲 周思之 |
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作者单位: | 1. 沈阳发动机设计研究所,沈阳,110015 2. 北京航空航天大学能源与动力工程学院,北京,100083 |
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摘 要: | 为了提高航空发动机弧齿锥齿轮在装配中的着色合格率,分析了弧齿锥齿轮啮合机理,找到了影响啮合面和齿隙不正确的因素,提出了检查和调整弧齿锥齿轮啮合面与齿隙的方法。
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关 键 词: | 喷管 喷流 红外辐射特征 航空发动机 数值模拟 试验 |
Investigation of Color Marking for Spiral Bevel Gear of Areoengine |
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Authors: | WANG Hui WANG Zhi zhe ZHOU Si-zhi |
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Institution: | 1. Shenyang Aeroengine Research Institute, Shenyang 110015, China; 2. School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100083, China) |
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Abstract: | The numerical models of an aeroengine exhaust nozzle and its jet flow field were built based on the Navier-Stokes equations. The infrared radiation characteristics of the exhaust nozzle at non-afterburning condition were obtained by infrared radiation characteristics calculation program compiled by the integrated method of the Radiation Transfer Equation (RTE). The infrared radiation characteristics of the modeled exhaust nozzle were measured by the test. The results of numerical simulation and measurement for infrared radiation characteristics for the exhaust nozzle in the. spectrum range of 3.0-5.0 μm were given. The results show that the numerical simulation are in accord with the measurement. |
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Keywords: | nozzle jet infrared radiation characteristics aeroengine numerical simulation experiment |
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