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MPT可靠启动与稳定工作影响因素 被引量:4
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作者 夏广庆 毛根旺 +3 位作者 杨涓 宋军 陈君 何洪庆 《推进技术》 EI CAS CSCD 北大核心 2006年第4期363-367,共5页
为了研制高性能、高可靠MPT,在真空条件下,实验研究了不同推进工质、内导体位置、微波接头灌封材料、探针长度、工质流量和微波输入功率等因素对100W MPT可靠启动和稳定工作的影响。通过实验,分析了MPT主要性能参数如推力、比冲及效率... 为了研制高性能、高可靠MPT,在真空条件下,实验研究了不同推进工质、内导体位置、微波接头灌封材料、探针长度、工质流量和微波输入功率等因素对100W MPT可靠启动和稳定工作的影响。通过实验,分析了MPT主要性能参数如推力、比冲及效率等随工质流量、微波输入功率等参数的变化规律。研究结果可为MPT的性能改进起到重要指导和参考作用。 展开更多
关键词 微波等离子推力器 谐振腔 ^真空实验^+ 性能参数
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Dynamic modeling of a parafoil system considering flap deflection 被引量:3
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作者 Tao Jin Sun Qinglin +1 位作者 Chen Zengqiang He Yingping 《Journal of Southeast University(English Edition)》 EI CAS 2017年第4期416-425,共10页
In order to better study the dynamic characteristics and the control strategy of parafoil systems,considering the effect of flap deflection as the control mechanism and regarding the parafoil and the payload as a rigi... In order to better study the dynamic characteristics and the control strategy of parafoil systems,considering the effect of flap deflection as the control mechanism and regarding the parafoil and the payload as a rigid body,a six degrees-of-freedom(DOF)dynamic model of a parafoil system including three DOF for translational motion and three DOF for rotational motion,is established according to the K rchhoff motion equation.Since the flexible winged paafoil system flying at low altitude is more susceptibleto winds,the motion characteristics of the parafoil system Wth and Wthout winds are simulated and analyzed.Furthermore,the ardropm test is used to further verify the model.The comparison results show that the simulation trajectory roughly overlaps with the actual flight track.The horzontnl velocity of the simulation model is in good accordance with the airdrop test,with a deviation less than0.5m/s,while its simulated vertical velocity fuctuates slightly under the infuence of the wind,and shows a similar trend to the ardrop test.It is concludedthat the established model can well describe the characteristics of the parafoil system. 展开更多
关键词 parafoil system dynamic modeling and simulation fig h t chaacterstic airdrop experiment fap defection
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Vacuum preloading combined electroosmotic strengthening of ultra-soft soil 被引量:22
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作者 彭劼 熊雄 +1 位作者 MAHFOUZ A H 宋恩润 《Journal of Central South University》 SCIE EI CAS 2013年第11期3282-3295,共14页
To assess the effectiveness of vacuum preloading combined electroosmotic strengthening of ultra-soft soil and study the mechanism of the process, a comprehensive experimental investigation was performed. A laboratory ... To assess the effectiveness of vacuum preloading combined electroosmotic strengthening of ultra-soft soil and study the mechanism of the process, a comprehensive experimental investigation was performed. A laboratory test cell was designed and applied to evaluate the vacuum preloading combined electroosmosis. Several factors were taken into consideration, including the directions of the electroosmotic current and water induced by vacuum preloading and the replenishment of groundwater from the surrounding area. The results indicate that electroosmosis together with vacuum preloading improve the soil strength greatly, with an increase of approximately 60%, and reduce the water content of the soil on the basis of consolidation of vacuum preloading, howeve~ further settlement is not obvious with only 1.7 mm. The reinforcement effect of vacuum preloading combined electroosmosis is better than that of electroosmosis after vacuum preloading. Elemental analysis using X-ray fluorescence proves that the soil strengthening during electroosmotic period in this work is mainly caused by electroosmosis-induced electrochemical reactions, the concentrations of Al2O3 in the VPCEO region increase by 2.2%, 1.5%, and 0.9% at the anode, the midpoint between the electrodes, and the cathode, respectively. 展开更多
关键词 vacuum preloading electroosmosis laboratory test ultra-soft soil reinforcement effect X-ray fluorescence reinforcement mechanism
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Laboratory investigation of axisymmetric single vacuum well point
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作者 武文俊 姚磊华 魏英杰 《Journal of Central South University》 SCIE EI CAS CSCD 2016年第3期750-756,共7页
Vacuum well point is a new but faint soft ground treatment method. This work focuses on the consolidation behavior of a reconstituted soft clayey specimen under vacuum well point combined with surcharge loading. The l... Vacuum well point is a new but faint soft ground treatment method. This work focuses on the consolidation behavior of a reconstituted soft clayey specimen under vacuum well point combined with surcharge loading. The laboratory test was conducted through a vacuum-surcharge consolidation apparatus, and the vacuum loading scheme was adopted for vacuum pressure application to investigate the vacuum effect on soil consolidation. In the testing process, some key parameters such as vacuum pressure, pore water pressure and settlement deformation were timely recorded. Furthermore, the water content, void ratio and permeability coefficient of samples collected after loading were measured to reflect the consolidation characteristics. By comparing with the membrane system and membraneless system, something different was found for the vacuum well point method. The results indicate that the consolidation behavior of an axisymmetric single vacuum well point is almost identical to the behavior of vacuum preloading combined with prefabricated vertical drain(PVD), except for the distribution of the vacuum pressure along the well drain due to the structure of the vacuum well point. And the vacuum well point method may be useful for the improvement of soft clayey deposit in a certain depth. 展开更多
关键词 soft ground vacuum consolidation vacuum well point systems vacuum pressure
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An introduction to the novel vacuum plume effects experimental system 被引量:4
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作者 CAI Guo Biao LING Gui Long HE Bi Jiao 《Science China(Technological Sciences)》 SCIE EI CAS CSCD 2016年第6期953-960,共8页
This paper introduces a newly developed vacuum Plume effects Experimental System(PES) used for plume effect tests of rocket engines and vacuum heat tests of satellites. The design level, manufacturing technique, and t... This paper introduces a newly developed vacuum Plume effects Experimental System(PES) used for plume effect tests of rocket engines and vacuum heat tests of satellites. The design level, manufacturing technique, and testing capabilities of the PES have reached a highly advanced level at home and abroad. The PES mainly consists of a vacuum chamber, vacuum acquisition system, nitrogen system, helium system, and parameter measurement system. A breakthrough was obtained on the Large Scale Cryo-Pumping System, which was based on a combined liquid nitrogen and liquid helium heat sink. An internal cryopump with a limiting temperature of 4.2 K and an efficient absorption area of 305 m2 was developed. The absorption capability of the cryopump was above 7×107 L/s. Vacuum plume tests were performed in the temperature ranges of ambient temperature, liquid nitrogen, and liquid helium. The experimental results showed that the plume test capability of PES is higher than that of similar foreign equipment STG and CHAFF-4. For 2 g/s and 117 N rocket engines, the dynamic vacuum degree of environment was 8.0×10?4 Pa(approximately 137 km height) and 1.1×10?2 Pa(approximately 106 km height), respectively. 展开更多
关键词 vacuum plume effect liquid nitrogen heat sink liquid helium heat sink plume absorption pump
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A Mechanical and Experimental Study on the Heat Loss of Solar Evacuated Tube 被引量:1
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作者 赵惠忠 刘震炎 +3 位作者 张敏 黄晨 王丽慧 邹志军 《Journal of Shanghai Jiaotong university(Science)》 EI 2009年第1期52-57,共6页
The experimental system of heat loss of all-glass evacuated solar collector tubes(evacuated tube) is firstly designed and constructed,which uses electric heater as thermal resource.The equilibrium temperatures are les... The experimental system of heat loss of all-glass evacuated solar collector tubes(evacuated tube) is firstly designed and constructed,which uses electric heater as thermal resource.The equilibrium temperatures are less than±1℃during the test.and the temperature differences of up/middle/low node in the tube are less than 1℃,3℃,and 7℃respectively.The heat loss of evacuated tube increases about 2.7%with vacuum state of 0.01--1 mPa,and it has the best performance at tube temperature of 20--280℃.The invalidation tube(>200 mPa) has the biggest heat loss that increases linearly with the tube temperature.The evacuated tubes with the vacuum of 0.01-1 mPa are suitable for most solar adsorption refrigeration. 展开更多
关键词 all-glass evacuated solar collector tube adsorption refrigeration vacuum state heat loss equilibrium temperature
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Analysis of X(5568) as Scalar Tetraquark State in Diquark-Antidiquark Model with QCD Sum Rules
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作者 王志刚 《Communications in Theoretical Physics》 SCIE CAS CSCD 2016年第9期335-339,共5页
In this article, we take the X(5568) as the diquark-antidiquark type tetraquark state with the spin-parity J^P= 0^+, construct the scalar-diquark-scalar-antidiquark type current, carry out the operator product expansi... In this article, we take the X(5568) as the diquark-antidiquark type tetraquark state with the spin-parity J^P= 0^+, construct the scalar-diquark-scalar-antidiquark type current, carry out the operator product expansion up to the vacuum condensates of dimension-10, and study the mass and pole residue in details with the QCD sum rules. We obtain the value M_X =(5.57 ± 0.12) Ge V, which is consistent with the experimental data. The present prediction favors assigning the X(5568) to be the scalar tetraquark state. 展开更多
关键词 tetraquark states QCD sum rules
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Experimental and Stowing/Deploying Dynamical Simulation of Lenticular Carbon Fiber Reinforced Polymer Thin-Walled Tubular Space Boom 被引量:2
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作者 李瑞雄 陈务军 付功义 《Journal of Shanghai Jiaotong university(Science)》 EI 2012年第1期58-64,共7页
The stowing and deploying experiment was conducted for three 700 mm long thin-walled tubes,and the structural behavior characteristics parameters were measured clearly,including strain,deformation and wrapping moment.... The stowing and deploying experiment was conducted for three 700 mm long thin-walled tubes,and the structural behavior characteristics parameters were measured clearly,including strain,deformation and wrapping moment.3D finite element models(FEM)were built subsequently and explicit dynamic method was used to simulate the stowing and deploying of the lenticular carbon fiber reinforced polymer(CFRP)thin-walled tubular space boom,which was designed as four-ply(45°/-45°/45°/-45°)lay-up.The stress and energy during the wrapping process were got and compared with different wrapping angular velocity,the reasonable wrapping angular velocity and effective method were conformed,and structural behavior characteristics were obtained.The results were compared and discussed as well,and the results show that the numerical results by 0.628 rad/s velocity agree well with the measured values.In this paper,the numerical procedure and experimental results are valuable to the optimization design of CFRP thin-walled tubular space boom and future research. 展开更多
关键词 lenticular carbon fiber reinforced polymer thin-walled tube space boom explicit method stowing and deploying wrapping moment
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