气体发生式推进系统降温与点火特性分析
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摘要
论文以气体发生式推进系统作为研究对象,通过建立数学模型和仿真模型,对其降温、点火装置的结构进行了研究设计。并建立了地面实验系统,通过实验验证了降温组件的性能。主要内容包括:
1、对翅片辐射降温器的设计方法进行了探索。采用螺旋通道使气体与降温器内壁面充分对流换热,用翅片加强降温器壳体与外界的辐射换热;建立数学模型,并运用流体仿真计算软件进行数值仿真计算,通过对仿真计算结果的分析比较,得出最佳设计参数。
2、对三种翅片辐射降温器进行地面实验。针对应用领域的要求,设计并加工出了三种不同的翅片辐射降温器,并建立了地面实验系统,检验了三个加工件的降温性能。
3、研究了气体发生剂单元的点火过程。运用热力计算的方式探索了气体发生剂配方的设计方法,完成了对气体发生剂单元结构的设计;并对点火技术进行了研究,确定了最佳的点火方式。
4、对仿真软件的原理进行了介绍,通过对共用节点法、接触耦合法和流固耦合法三种爆炸仿真方法的分析,结合本文研究对象的特点,在仿真过程设计过程中采用了以多物资流固耦合法为主、其它方法为辅的方法,取得了较好的效果。
5、为气体发生剂单元建立了仿真模型,并采用较为合适的材料模型、状态方程和仿真参数,对它的工作过程进行了仿真分析,直观地观察了燃气的膨胀过程、燃气对膜片的切割分离过程和膜片的破口形状。
This paper aims to study Gas-Generating Propulsion System. The research is mainly focused on the structure of its cooling system and ignition device by building mathematical model and simulation model. And the ground experimental system was built to test the performance of the cooling instrument. The content of the study can be summarized as below.
1. The finned radiation cooler was designed and explored. Spiral channels were used to make the heat convection between working medium and cooler pipe wall to be full. Meantime, the fin was used for strengthening radiation heat transfer between cooler shell and external. A mathematical model was established to imitate the process and fluid simulation software was used for the numerical simulation of the model. Then the best design parameters were obtained through the simulation results analysis.
2. Three finned radiation coolers were studied in the ground laboratory. According to the requirements from application fields, three different finned radiation coolers were designed and manufactured. And the cooling performances of three manufactures were tested in ground laboratory.
3. The ignition process of gas generating unit was studied. After exploring the design method for gas generating reagents formula by using thermodynamic calculation, we succeeded in the structure design of the gas generating unit. And we studied the ignite methods and got the best one.
4. The principle of the simulation software was introduced and three explosion simulation method including shared node, contact coupling and fluid-solid coupling were analyzed. We gained good results in the simulation process by using the multi-material fluid-solid coupling methods as the major method and other method for supplement.
5. The simulation model of gas generating agent was built and its working process was analyzed by using proper material model, state equation and simulation parameters. The process of fuel gas expand, the process of diaphragm cutting separation cut by fuel gas and the shape of crevasse in diaphragm were all observed directly during the analysis.
1、对翅片辐射降温器的设计方法进行了探索。采用螺旋通道使气体与降温器内壁面充分对流换热,用翅片加强降温器壳体与外界的辐射换热;建立数学模型,并运用流体仿真计算软件进行数值仿真计算,通过对仿真计算结果的分析比较,得出最佳设计参数。
2、对三种翅片辐射降温器进行地面实验。针对应用领域的要求,设计并加工出了三种不同的翅片辐射降温器,并建立了地面实验系统,检验了三个加工件的降温性能。
3、研究了气体发生剂单元的点火过程。运用热力计算的方式探索了气体发生剂配方的设计方法,完成了对气体发生剂单元结构的设计;并对点火技术进行了研究,确定了最佳的点火方式。
4、对仿真软件的原理进行了介绍,通过对共用节点法、接触耦合法和流固耦合法三种爆炸仿真方法的分析,结合本文研究对象的特点,在仿真过程设计过程中采用了以多物资流固耦合法为主、其它方法为辅的方法,取得了较好的效果。
5、为气体发生剂单元建立了仿真模型,并采用较为合适的材料模型、状态方程和仿真参数,对它的工作过程进行了仿真分析,直观地观察了燃气的膨胀过程、燃气对膜片的切割分离过程和膜片的破口形状。
This paper aims to study Gas-Generating Propulsion System. The research is mainly focused on the structure of its cooling system and ignition device by building mathematical model and simulation model. And the ground experimental system was built to test the performance of the cooling instrument. The content of the study can be summarized as below.
1. The finned radiation cooler was designed and explored. Spiral channels were used to make the heat convection between working medium and cooler pipe wall to be full. Meantime, the fin was used for strengthening radiation heat transfer between cooler shell and external. A mathematical model was established to imitate the process and fluid simulation software was used for the numerical simulation of the model. Then the best design parameters were obtained through the simulation results analysis.
2. Three finned radiation coolers were studied in the ground laboratory. According to the requirements from application fields, three different finned radiation coolers were designed and manufactured. And the cooling performances of three manufactures were tested in ground laboratory.
3. The ignition process of gas generating unit was studied. After exploring the design method for gas generating reagents formula by using thermodynamic calculation, we succeeded in the structure design of the gas generating unit. And we studied the ignite methods and got the best one.
4. The principle of the simulation software was introduced and three explosion simulation method including shared node, contact coupling and fluid-solid coupling were analyzed. We gained good results in the simulation process by using the multi-material fluid-solid coupling methods as the major method and other method for supplement.
5. The simulation model of gas generating agent was built and its working process was analyzed by using proper material model, state equation and simulation parameters. The process of fuel gas expand, the process of diaphragm cutting separation cut by fuel gas and the shape of crevasse in diaphragm were all observed directly during the analysis.
引文
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