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| 涡轴发动机通用仿真平台研究 | |
| 引用本文： | 吴燕燕,刘明,王栋,杨小龙,郭芳.涡轴发动机通用仿真平台研究[J].直升机技术,2013(2):59-64. |
| 作者姓名： | 吴燕燕 刘明 王栋 杨小龙 郭芳 |
| 作者单位： | 1. 中国直升机设计研究所,江西景德镇,333001 2. 海军驻景德镇地区航空军事代表室,江西景德镇,333001 3. 陆航驻景德镇地区代表室,江西景德镇,333002 |
| 摘 要： | 采用部件法建立涡轴发动机通用模型的难点是:如何为发动机模型的各部件参数和特性数据块建立统一的输入接口；建立的稳态模型和动态模型均要在全包线范围内收敛；动态模型要求在任意高度和马赫数下均能满足实时性要求.文章利用Vc++编程语言建立了统一特性数据输入接口；综合使用多种方法使数学模型达到全包线范围内收敛和满足实时性要求的目的. |
| 关 键 词： | 涡轴发动机 实时要求 通用仿真平台 |
Study of Turboshaft Engine General Simulation Interface |
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| Authors: | WU Yanyan LIU Ming WANG Dong YANG Xiaolong GUO Fang |
| Institution: | 1.China Helicopter Research and Development Institute, Jingdezhen 333001, China; 2. Military Representative Bureau Based in Jingdezhen Area of Navy, Jingdezhen 333001, China; 3. Army Aviation Department of the PLA General Staff Military Representative Office in Jingdezhen Region, Jingdezhen 333002, China) |
| Abstract: | The difficuhy of general simulation interface is to building uniform input interface of en-gine model components parameter and characteristic data, the model can fulfil constringency require-ment in whole envelopment, and fulfil the real-time requirement at any height and speed. In order to solve those problems, using VC ＋ ＋ programme language built unity characteristic data input inter-face, many method were used in this paper. |
| Keywords: | turboshaft engine real-time requirement general simulation interface |
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