| 基于TBS 的航空发动机技术风险识别方法研究 |
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| 引用本文： | 刘晓松,王桂华,刘庆东,贾淑芝,王艳丽,史妍妍.基于TBS 的航空发动机技术风险识别方法研究[J].航空发动机,2017,43(3):93-97. |
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| 作者姓名： | 刘晓松 王桂华 刘庆东 贾淑芝 王艳丽 史妍妍 |
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| 作者单位： | 中国航发沈阳发动机研究所，沈阳110015 |
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| 基金项目： | 航空动力基础研究项目资助 |
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| 摘 要： | 为提升中国航空发动机研制项目中技术风险的管控能力,根据航空发动机的研制特点,提出1种基于技术分解结构的航空发动机技术风险识别方法。该方法涵盖技术分解结构的构建方式、技术风险的识别方法和排序方法等内容,通过在实际发动机研制项目中的应用,证明该方法有效、可行,能够实现技术风险完整、合理地识别,同时提出了该方法在应用过程中应注意基于TBS的技术风险识别为动态过程等问题,为中国航空发动机研制行业技术风险的识别提供参考。
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| 关 键 词： | 技术风险 风险识别 技术分解结构 航空发动机 |
Research on Aeroengine Technical Risk Identification Method Based on TBS |
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| Authors: | LIU Xiao-song WANG Gui-hu LIU Qing-dong JIA Shu-zhi WANG Yan-li SHI Yan-yan |
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| Institution: | AECC Shenyang Engine Research Institution, Shenyang 110015, China |
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| Abstract: | In order to improve capacity of control risk in Chinese aeroengine development, according to the research characteristics of
aeroengine, a technical risk identification method was presented based on Technology Breakdown Structure (TBS) ,which includes the
establishment method of TBS, the identification method of technical risk and the sorting method of technical risk. The application situation
of actual project indicates that the method is feasible and acceptable, and some advice was given in its application, which is taken as a
reference to risk management in Chinese aeroengine development |
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| Keywords: | technical risk risk identification Technology Breakdown Structure aeroengine |
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