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Electrocatalytic CO_(2)reduction for the selective production of liquid oxygenates 被引量:1
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作者 Jiapeng Ji Junnan Chen +2 位作者 Juxia Xiong Xiaolong Zhang Hui-Ming Cheng 《Journal of Energy Chemistry》 2025年第4期568-600,共33页
Electrocatalytic CO_(2)reduction(ECR)to produce value-added fuels and chemicals using renewable electricity is an emerging strategy to mitigate global warming and decrease reliance on fossil fuels.Among various ECR pr... Electrocatalytic CO_(2)reduction(ECR)to produce value-added fuels and chemicals using renewable electricity is an emerging strategy to mitigate global warming and decrease reliance on fossil fuels.Among various ECR products,liquid oxygenates(Oxys)are especially attractive due to their high energy density,high safety and transportability that could be adapted to the existing infrastructure and transportation system.However,efficiently generating these highly reduced oxygen-containing products by ECR remains challenging due to the complexity of coupled proton and electron transfer processes.In recent years,in-depth studies of reaction mechanisms have advanced the design of catalysts and the regulation of reaction systems for ECR to produce Oxys,Here,by focusing on the production of typical Oxys,such as methanol,acetic acid,ethanol,acetone,n-propanol,and isopropanol,we outline various reaction paths and key intermediates for the electrochemical conversion of CO_(2)into these target products.We also summarize the current research status and recent advances in catalysts based on their elemental composition,and consider recent studies on the change of catalyst geometry and electronic structure,as well as the optimization of reaction systems to increase ECR performance.Finally,we analyze the challenges in the field of ECR to Oxys and provide an outlook on future directions for high-efficiency catalyst prediction and design,as well as the development of advanced reaction systems. 展开更多
关键词 Electrocatalytic CO_(2)reduction Geometry and electronic structure Parameters and system configurations liquid oxygenates
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Gas film/regenerative composite cooling characteristics of the liquid oxygen/liquid methane (LOX/LCH4) rocket engine
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作者 Xinlin LIU Jun SUN +3 位作者 Zhuohang JIANG Qinglian LI Peng CHENG Jie SONG 《Journal of Zhejiang University-Science A(Applied Physics & Engineering)》 SCIE EI CAS CSCD 2024年第8期631-649,共19页
The thermal protection of rocket engines is a crucial aspect of rocket engine design.In this paper,the gas film/regenerative composite cooling of the liquid oxygen/liquid methane(LOX/LCH4)rocket engine thrust chamber ... The thermal protection of rocket engines is a crucial aspect of rocket engine design.In this paper,the gas film/regenerative composite cooling of the liquid oxygen/liquid methane(LOX/LCH4)rocket engine thrust chamber was investigated.A gas film/regenerative composite cooling model was developed based on the Grisson gas film cooling efficiency formula and the one-dimensional regenerative cooling model.The accuracy of the model was validated through experiments conducted on a 6 kg/s level gas film/regenerative composite cooling thrust chamber.Additionally,key parameters related to heat transfer performance were calculated.The results demonstrate that the model is sufficiently accurate to be used as a preliminary design tool.The temperature rise error of the coolant,when compared with the experimental results,was found to be less than 10%.Although the pressure drop error is relatively large,the calculated results still provide valuable guidance for heat transfer analysis.In addition,the performance of composite cooling is observed to be superior to regenerative cooling.Increasing the gas film flow rate results in higher cooling efficiency and a lower gas-side wall temperature.Furthermore,the position at which the gas film is introduced greatly impacts the cooling performance.The optimal introduction position for the gas film is determined when the film is introduced from a single row of holes.This optimal introduction position results in a more uniform wall temperature distribution and reduces the peak temperature.Lastly,it is observed that a double row of holes,when compared to a single row of holes,enhances the cooling effect in the superposition area of the gas film and further lowers the gas-side wall temperature.These results provide a basis for the design of gas film/regenerative composite cooling systems. 展开更多
关键词 liquid oxygen/liquid methane(LOX/LCH4)rocket engine Gas film cooling Regenerative cooling Heat transfer characteristics
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Study on fluid-structure interaction in liquid oxygen feeding pipe systems using finite volume method
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作者 Xin Wei Bing Sun 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2011年第5期706-712,共7页
The fluid-structure interaction may occur in space launch vehicles,which would lead to bad performance of vehicles,damage equipments on vehicles,or even affect astronauts' health.In this paper,analysis on dynamic beh... The fluid-structure interaction may occur in space launch vehicles,which would lead to bad performance of vehicles,damage equipments on vehicles,or even affect astronauts' health.In this paper,analysis on dynamic behavior of liquid oxygen (LOX) feeding pipe system in a large scale launch vehicle is performed,with the effect of fluid-structure interaction (FSI) taken into consideration.The pipe system is simplified as a planar FSI model with Poisson coupling and junction coupling.Numerical tests on pipes between the tank and the pump are solved by the finite volume method.Results show that restrictions weaken the interaction between axial and lateral vibrations.The reasonable results regarding frequencies and modes indicate that the FSI affects substantially the dynamic analysis,and thus highlight the usefulness of the proposed model.This study would provide a reference to the pipe test,as well as facilitate further studies on oscillation suppression. 展开更多
关键词 Fluid-structure interaction · liquid oxygen · Finite volume method
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Simulation and Experiment for Oxygen-enriched Combustion Engine Using Liquid Oxygen to Solidify CO_(2) 被引量:5
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作者 LIU Yongfeng JIA Xiaoshe +3 位作者 PEI Pucheng LU Yong YI Li SHI Yan 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2016年第1期188-194,共7页
For capturing and recycling of CO_(2)in the internal combustion engine,Rankle cycle engine can reduce the exhaust pollutants effectively under the condition of ensuring the engine thermal efficiency by using the techn... For capturing and recycling of CO_(2)in the internal combustion engine,Rankle cycle engine can reduce the exhaust pollutants effectively under the condition of ensuring the engine thermal efficiency by using the techniques of spraying water in the cylinder and optimizing the ignition advance angle.However,due to the water spray nozzle need to be installed on the cylinder,which increases the cylinder head design difficulty and makes the combustion conditions become more complicated.In this paper,a new method is presented to carry out the closing inlet and exhaust system for internal combustion engines.The proposed new method uses liquid oxygen to solidify part of cooled CO_(2)from exhaust system into dry ice and the liquid oxygen turns into gas oxygen which is sent to inlet system.The other part of CO_(2)is sent to inlet system and mixed with oxygen,which can reduce the oxygen-enriched combustion detonation tendency and make combustion stable.Computing grid of the IP52FMI single-cylinder four-stroke gasoline-engine is established according to the actual shape of the combustion chamber using KIVA-3V program.The effects of exhaust gas recirculation(EGR)rate are analyzed on the temperatures,the pressures and the instantaneous heat release rates when the EGR rate is more than 8%.The possibility of enclosing intake and exhaust system for engine is verified.The carbon dioxide trapping device is designed and the IP52FMI engine is transformed and the CO_(2)capture experiment is carried out.The experimental results show that when the EGR rate is 36%for the optimum EGR rate.When the liquid oxygen of 35.80-437.40 g is imported into the device and last 1-20 min,respectively,21.50-701.30 g dry ice is obtained.This research proposes a new design method which can capture CO_(2)for vehicular internal combustion engine. 展开更多
关键词 internal combustion Rankle cycle engine CO_(2)emission reduction carbon-sequestration with liquid oxygen KIVA-3V program oxygen-enriched combustion numerical simulation experiments
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Hierarchical BiOBr microspheres with oxygen vacancies synthesized via reactable ionic liquids for dyes removal 被引量:3
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作者 Zhi-Dong Wei Rui Wang 《Chinese Chemical Letters》 SCIE CAS CSCD 2016年第5期769-772,共4页
Hierarchical BiOBr microspheres with oxygen vacancies, which can be used for the dyes removal, have been synthesized successfully in the presence of different kinds of ionic liquids. It was revealed that BiOBr prepare... Hierarchical BiOBr microspheres with oxygen vacancies, which can be used for the dyes removal, have been synthesized successfully in the presence of different kinds of ionic liquids. It was revealed that BiOBr prepared by the ionic liquids with short chain length exhibited higher photocatalytic activity in the degradation of methyl orange (MO) under visible light. The experimental results showed that the phenomenon of the photocatalytic degradation of MO can be explained by the photoluminescence spectra. 展开更多
关键词 BiOBr Dyes removal Photocatalytic Ionic liquids oxygen vacancies
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Analysis of Magnetic Positioning for Liquid Oxygen Under Microgravity Condition
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作者 ZHONG Dinghan LIU Hongbo LU Xiang 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI CSCD 2022年第6期750-758,共9页
Due to the paramagnetic property of liquid oxygen,the Kelvin force can be induced in liquid oxygen under non-uniform magnetic field.Based on the volume of fluid(VOF)model,the positioning effect of the force in liquid ... Due to the paramagnetic property of liquid oxygen,the Kelvin force can be induced in liquid oxygen under non-uniform magnetic field.Based on the volume of fluid(VOF)model,the positioning effect of the force in liquid oxygen tanks is analyzed under various Bond numbers(Bo)and magnetic Bond numbers(Bom).The results show that the magnetic field has the effect of repositioning the liquid oxygen in the tank when the gravity field is not enough or absent.Additionally,the gas-liquid interface has a periodic fluctuation during the process due to the inhomogeneous Kelvin force distribution,and more effective suppression of fluctuation can be achieved under the condition of a larger Bom.The new method of controlling gas-liquid interface of liquid oxygen tank under micro gravity condition is hoped to be developed in the future. 展开更多
关键词 magnetic field microgravity environment liquid oxygen gas-liquid interface
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INTERACTION OF PLASMA—LIQUID IN AN OXYGEN GLOW DISCHARGE Ⅲ.OXIDATION DESULFURIZATION OF ETHYL—THIOETHER
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作者 Wan Ying LIU Wei LU Zheng Lan LEI Jin Kun WANG Chengdu Institute of Organic Chemistry,Academia Sinica Chengdu 610015 《Chinese Chemical Letters》 SCIE CAS CSCD 1993年第10期883-884,共2页
A few factors affecting plasma oxidation desulfurization of ethyl- thioether were investigated.Under the typical conditions,the conversion and degree of desulfurization of ethyl-thioether can be achieved up to 88% and... A few factors affecting plasma oxidation desulfurization of ethyl- thioether were investigated.Under the typical conditions,the conversion and degree of desulfurization of ethyl-thioether can be achieved up to 88% and 79% respectively. 展开更多
关键词 OC OXIDATION DESULFURIZATION OF ETHYL THIOETHER INTERACTION OF PLASMA liquid IN AN oxygen GLOW DISCHARGE
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Partial oxidation of methane by photocatalysis 被引量:2
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作者 Zhongshan Yang Qiqi Zhang +5 位作者 Hui Song Xin Chen Jiwei Cui Yanhui Sun Lequan Liu Jinhua Ye 《Chinese Chemical Letters》 SCIE CAS CSCD 2024年第1期153-168,共16页
Methane chemistry is one of the“Holy Grails of catalysis”.It is highly desirable but challenge to transform methane into value-added chemicals,because of its high C-H bonding energy(435 kJ/mol),lack ofπbonding or u... Methane chemistry is one of the“Holy Grails of catalysis”.It is highly desirable but challenge to transform methane into value-added chemicals,because of its high C-H bonding energy(435 kJ/mol),lack ofπbonding or unpaired electrons.Currently,commercial methane conversion is usually carried out in harsh conditions with enormous energy input.Photocatalytic partial oxidation of methane to liquid oxygenates(PPOMO)is a future-oriented technology towards realizing high efficiency and high selectivity under mild conditions.The selection of oxidant is crucial to the PPOMO performance.Hence,attentions are paid to the research progress of PPOMO with various oxidants(O_(2),H_(2)O,H_(2)O_(2)and other oxidants).Moreover,the activation of the selected oxidants is also highly emphasized.Meanwhile,we summarized the methane activation mechanisms focusing on the C-H bond that was broken mainly by·OH radical,O-specie or photogenerated hole(h+).Finally,the challenges and prospects in this subject are briefly discussed. 展开更多
关键词 Partial oxidation of methane PHOTOCATALYSIS liquid oxygenates OXIDANTS C-H activation
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空分装置贫氪氙液氧系统工艺流程简述及调试总结 被引量:1
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作者 党伟 《低温与特气》 CAS 2024年第5期41-42,45,共3页
简要介绍国能榆林化工有限公司3套十万等级空分附带贫氪氙液氧系统工艺流程、设备构成、调试运行,及注意事项。
关键词 空分 贫氪氙液氧系统 调试总结
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垂直起降重复使用运载火箭总体设计优化方法研究
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作者 朱雄峰 周城宏 +5 位作者 雍子豪 王一杉 崔朋 谭胜 刘鹰 刘阳 《载人航天》 CSCD 北大核心 2024年第2期197-205,共9页
针对垂直起降重复使用运载火箭总体设计多约束耦合问题,通过分析箭体构型、动力类型方案及动力布局类型,提出了优选两级单芯级构型、液氧甲烷动力和液氧煤油动力以及优选中小发动机多机并联方案,并优选5、7、9机并联动力布局。采用齐奥... 针对垂直起降重复使用运载火箭总体设计多约束耦合问题,通过分析箭体构型、动力类型方案及动力布局类型,提出了优选两级单芯级构型、液氧甲烷动力和液氧煤油动力以及优选中小发动机多机并联方案,并优选5、7、9机并联动力布局。采用齐奥科夫斯基公式,对垂直起降重复使用运载火箭的运载能力进行估算,并以一二级间比为优化变量,进行初步总体优化,得到在不同箭体直径、动力类型和动力布局下的基础运载能力,结合长细比分析得出两级单芯级、奇数台发动机并联的垂直起降重复使用运载火箭总体方案。 展开更多
关键词 发射运输系统 运载火箭 液氧煤油 液氧甲烷 重复使用 垂直起降
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液氧加注系统仿真研究 被引量:3
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作者 陈世超 黄福友 +2 位作者 丁鹏飞 唐强 何燚 《低温与超导》 CAS 北大核心 2016年第6期10-13,共4页
利用SINDA/FLUINT软件,对某液氧加注系统进行1:1建模,对预冷和大流量加注过程中的流体温度、压力、流量等主要参数进行仿真分析,通过仿真结果与加注任务实测数据的对比,验证了低温加注过程系统级仿真预示的可行性。
关键词 液氧 加注系统 仿真 预冷 大流量
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液氧加注过程热力性能分析 被引量:2
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作者 高婉丽 罗天培 +1 位作者 刘瑞敏 孙德 《火箭推进》 CAS 2017年第3期22-27,78,共7页
为满足某型号运载火箭动力系统试验液氧加注温度要求,需对加注过程进行热力性能分析。通过对常规氧加注过程因漏热和流阻损失引起的温升、液氧泵效率损失引起的温升进行理论计算,得出常规氧加注过程液氧温度变化规律。此外,通过对过冷... 为满足某型号运载火箭动力系统试验液氧加注温度要求,需对加注过程进行热力性能分析。通过对常规氧加注过程因漏热和流阻损失引起的温升、液氧泵效率损失引起的温升进行理论计算,得出常规氧加注过程液氧温度变化规律。此外,通过对过冷氧温度掺混特性进行理论计算和数值仿真,得出过冷氧加注的热力性能。上述分析结果与实测数据进行了比对,结果表明,理论分析结果与实测结果吻合性好,液氧加注过程热力特性分析方法正确可行。 展开更多
关键词 液氧加注系统 温度调节 数值模拟
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液体火箭发动机爆震波点火技术初步研究 被引量:6
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作者 郭红杰 梁国柱 +1 位作者 马彬 张振鹏 《北京航空航天大学学报》 EI CAS CSCD 北大核心 2005年第4期375-380,共6页
对液体火箭发动机各种点火技术优缺点进行了对比分析,探讨了各种点火技术方案应用于未来先进推进系统的多管多次点火系统的可行性,讨论了各种点火技术应用方案的结构形式.对爆震波点火技术进行了初步研究,建立了气氢气氧爆震波点火的简... 对液体火箭发动机各种点火技术优缺点进行了对比分析,探讨了各种点火技术方案应用于未来先进推进系统的多管多次点火系统的可行性,讨论了各种点火技术应用方案的结构形式.对爆震波点火技术进行了初步研究,建立了气氢气氧爆震波点火的简化理论分析模型,对其在实际液氢液氧发动机中应用的具体方案进行了分析.分析结果表明,爆震波点火技术可以由低压混合气体产生高温高压的爆震产物,爆震波以高马赫数速度传播,迅速到达各点火位置.爆震波点火技术具备良好的同步性能和简单的结构方案形式,适用于液体火箭发动机多管多次同步点火. 展开更多
关键词 火箭发动机 爆震 点火 点火系统
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爆震波点火技术基本特性实验 被引量:9
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作者 郭红杰 梁国柱 +1 位作者 马彬 张振鹏 《推进技术》 EI CAS CSCD 北大核心 2005年第1期76-79,共4页
为了研究爆震波点火技术的基本特性,组建了氢氧爆震波点火实验系统,氢氧压力0.1~0.5MPa(表压),混合比1.6~9.4,常温条件下,得到了爆震波在管路中的传播特性以及爆震波点火的单管重复性能实验数据.结果表明:爆震波点火技术可以在较低的... 为了研究爆震波点火技术的基本特性,组建了氢氧爆震波点火实验系统,氢氧压力0.1~0.5MPa(表压),混合比1.6~9.4,常温条件下,得到了爆震波在管路中的传播特性以及爆震波点火的单管重复性能实验数据.结果表明:爆震波点火技术可以在较低的供气压力下获得高温(>1300℃)高压(>1MPa)爆震产物,爆震波点火传播速度可达3000m/s,并且具备良好的重复性能,多次点火重复性时间误差小于0.3ms. 展开更多
关键词 液体推进剂火箭发动机 爆震波 点火 点火系统 实验
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液动机引流式液氧煤油运载火箭推力矢量伺服控制系统 被引量:3
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作者 赵迎鑫 陈克勤 +2 位作者 赵守军 刘洪 姜庆义 《导弹与航天运载技术》 CSCD 北大核心 2022年第2期60-64,120,共6页
针对中国新一代系列运载火箭各级液氧煤油发动机的推力矢量控制需求,创新提出了液动机引流式伺服动力能源技术方案,研制了满足中国1200k N和180k N液氧煤油发动机的两型5种规格伺服机构,解决了高可靠系统架构设计、高集成伺服动力能源... 针对中国新一代系列运载火箭各级液氧煤油发动机的推力矢量控制需求,创新提出了液动机引流式伺服动力能源技术方案,研制了满足中国1200k N和180k N液氧煤油发动机的两型5种规格伺服机构,解决了高可靠系统架构设计、高集成伺服动力能源、伺服控制动态特性优化、长时免维护等难题,与国外直接引流式伺服技术方案相比,接口简单,实现了伺服机构与发动机工作介质有效隔离,使用维护性显著提高。产品通过与发动机联合热试车、耐环境、可靠性增长、可靠性强化等试验考核,首次应用于飞行试验,可满足同类液氧煤油发动机运载火箭使用需求。 展开更多
关键词 液动机引流式 伺服机构 液氧煤油发动机
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深海作业平台燃料电池AIP液氧系统供氧仿真分析 被引量:2
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作者 李彬彬 孔昕 +2 位作者 张杰 万江龙 谢仁和 《船海工程》 北大核心 2018年第3期158-163,共6页
针对目前以燃料电池为动力的深海作业平台供氧不稳定,液氧罐压力随着作业工况的不同波动较大,还未考虑燃料电池对液氧罐压力的影响等问题,以某型使用燃料电池为动力的深海作业平台为对象,建立从用氧端到储氧端的液氧系统供氧数学模型,以... 针对目前以燃料电池为动力的深海作业平台供氧不稳定,液氧罐压力随着作业工况的不同波动较大,还未考虑燃料电池对液氧罐压力的影响等问题,以某型使用燃料电池为动力的深海作业平台为对象,建立从用氧端到储氧端的液氧系统供氧数学模型,以Matlab/Simulink软件为平台,根据不同工况下的功率及用氧量的变化,对液氧系统进行动态仿真分析。仿真结果表明,深海作业时,由所需电功率变化引起平台用氧量变化的过程中,仿真过程具有较好的稳定性和动态响应,液氧系统能够根据工况的不同为燃料电池及人员呼吸持续提供氧气,保证10人在水下持续作业20 d以上,可有效满足深海作业平台能够长时间全天候在深海作业的需求。 展开更多
关键词 燃料电池 深海作业平台 液氧系统 仿真 MATLAB/SIMULINK
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双液相体系强化氧传递促进微生物油脂生产 被引量:5
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作者 颜日明 艾佐佐 +3 位作者 汪涯 张志斌 曾庆桂 朱笃 《生物工程学报》 CAS CSCD 北大核心 2013年第4期536-539,共4页
文中通过添加氧载体正十二烷进行双液相发酵来提高发酵性丝孢酵母利用木薯淀粉水解液生产微生物油脂的产量。结果表明,在摇瓶发酵液中添加氧载体,能明显缓解发酵过程中的氧限制程度。在2 L发酵罐中添加1%正十二烷进行双液相高密度发酵,... 文中通过添加氧载体正十二烷进行双液相发酵来提高发酵性丝孢酵母利用木薯淀粉水解液生产微生物油脂的产量。结果表明,在摇瓶发酵液中添加氧载体,能明显缓解发酵过程中的氧限制程度。在2 L发酵罐中添加1%正十二烷进行双液相高密度发酵,其发酵生物量和油脂产量分别达到101.2 g/L和50.28 g/L。气相色谱分析表明,添加了氧载体发酵的微生物油脂中含有更高的饱和脂肪酸含量。 展开更多
关键词 正十二烷 氧载体 双液相发酵 微生物油脂 发酵性丝孢酵母
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发动机试验液氧贮箱放气系统动态特性研究 被引量:1
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作者 徐鸿鹏 张志涛 +2 位作者 唐斌运 刘涛 董红兵 《火箭推进》 CAS 2018年第5期71-76,共6页
在液氧/煤油火箭发动机地面试验中,为得到液氧贮箱放气系统放气流量与放气阀门动作的响应特性,从而控制箱压的下降速率,验证液氧煤油发动机在低入口压力条件下的工作适应性,对液氧贮箱放气系统的动态特性进行了研究。建立了液氧贮箱二... 在液氧/煤油火箭发动机地面试验中,为得到液氧贮箱放气系统放气流量与放气阀门动作的响应特性,从而控制箱压的下降速率,验证液氧煤油发动机在低入口压力条件下的工作适应性,对液氧贮箱放气系统的动态特性进行了研究。建立了液氧贮箱二维计算模型,结合试验数据,对低温贮箱内气枕空间的非稳态换热过程进行研究,确定放出气体温度以及相应状态。应用CFD的动网格技术,建立二维计算模型,对放气系统阀门的开关动态特性与过流流量特性进行综合分析,获得了不同通径放气管路的放气流量与箱压的计算关联式,基于理想气体状态方程,完善了箱压计算理论模型。应用该模型量化分析箱压下降速率,为计算箱压控制的准确时间节点提供了操作参考。 展开更多
关键词 液氧贮箱 放气系统 动态特性 数值模拟 箱压控制
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泵压式氢/氧液体火箭发动机质量分析 被引量:3
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作者 凌桂龙 张黎辉 唐家鹏 《火箭推进》 CAS 2007年第1期1-6,共6页
在文献资料研究的基础上,根据泵压式氢/氧液体火箭发动机的实际特点,考虑发动机性能参数及结构尺寸等影响因素,利用理论推导、统计学及面密度等方法建立发动机质量模型。通过对SSME、RD-0120等8台氢/氧发动机质量的计算,验证了质量模型... 在文献资料研究的基础上,根据泵压式氢/氧液体火箭发动机的实际特点,考虑发动机性能参数及结构尺寸等影响因素,利用理论推导、统计学及面密度等方法建立发动机质量模型。通过对SSME、RD-0120等8台氢/氧发动机质量的计算,验证了质量模型的合理性。为发动机在系统方案论证时,其质量、性能等参数的估算和优化奠定了基础。 展开更多
关键词 航空 航天推进系统 氢/氧液体火箭发动机 涡轮泵 质量模型
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基于AMESim的液氧供应系统启动特性分析 被引量:2
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作者 朱旺 高婉丽 +1 位作者 杨思锋 刘瑞敏 《低温工程》 CAS CSCD 北大核心 2019年第2期60-65,共6页
为研究液氧供应系统启动阶段的压力平稳性,使用AMESim对液氧加注启动阶段平稳性进行了仿真,比较了设立启动容器和不设启动容器两种情况下液氧加注启动阶段的压力、流速的稳定性,通过仿真分析了启动容器设立的位置对加注流量稳定性的影... 为研究液氧供应系统启动阶段的压力平稳性,使用AMESim对液氧加注启动阶段平稳性进行了仿真,比较了设立启动容器和不设启动容器两种情况下液氧加注启动阶段的压力、流速的稳定性,通过仿真分析了启动容器设立的位置对加注流量稳定性的影响。通过对某型号动力系统试验液氧加注泄出系统进行仿真,将仿真结果与试验数据对比,验证了仿真过程中使用孔板替代发动机模拟负载的正确性与使用AMESim软件进行液氧供应系统仿真的合理性。经仿真分析,设立启动容器可使启动阶段压力震荡时间缩减至设立前的四分之一,设立启动容器后可明显减小启动阶段产生的压力凹坑,启动容器与负载端的距离为启动段平稳性的主要影响因素。 展开更多
关键词 液体火箭 液氧供应系统 启动容器 试验 AMESIM 平稳性
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