Development and Research of High-Enthalpy Multi-Functional Wind Tunnels Using Quasi-Steady MW-Class Arc Heaters
Development and Research of High-Enthalpy Multi-Functional Wind Tunnels Using Quasi-Steady MW-Class Arc Heaters
批准号:
06555294
负责人:
YOSHIKAWA Takao
金额:
$3.26万
依托单位:
依托单位国家:
日本
项目类别:
Grant-in-Aid for Scientific Research (A)
财政年份:
1994
资助国家:
日本
项目状态:
已结题
起止时间:
1994 至 1996
中文摘要
本文介绍了一种用于材料加工和气动加热模拟等的准稳态高焓等离子体风洞。电弧加热器工作电流为3-10 kA,工作气体为Ar、H_2、N_2和NH_3。产生的等离子体特性与静电探针测量。电子温度在50 mm的下游位置处为约5eV,并且离子数密度为10 μ cm<16>-3量级<-3>。结果,在轴上产生了高温、高密度和高速等离子体。针对电弧加热器在陶瓷涂层中的应用,研制了一种阴极覆盖陶瓷材料的烧蚀型电磁加速电弧加热发生器。在5-10 kA的Ar的100次发射操作中,陶瓷盖的烧蚀率范围为1.1至7.5 mg/shot。MPD等离子喷涂结果表明,获得了致密均匀的陶瓷膜,维氏硬度在1200以上。从XPS谱图来看,涂层的Si/Al峰面积比几乎与陶瓷原料相同,Al和Si的价数没有变化。因此,准稳态高焓等离子体发生器被发现具有很高的潜力,材料加工和应用到空气动力学领域。
英文摘要
A quasi-steady high-enthalpy plasma wind tunnel was developed for material processing and aerodynamic heating simulation etc. The arc heater was operated with discharge currents of 3-10 kA with working gases of Ar, H_2, N_2 and NH_3. Generated plasma characteristics were measured with an electrostatic probe. The electron temperature was about 5 eV at a downstream position of 50 mm, and the ion number density was the order of 10^<16> cm^<-3>. As a result, high-temperature high-density and high-velocity plasmas were created on the axis. For applications of the arc heater to ceramic coatings, an ablation-type electromagnetic-acceleration-type arcjet generator with a cathode covered with ceramic materials was developed. In 100-shot operations for Ar at 5-10 kA,the ablation rates of the ceramic covers ranged from 1.1 to 7.5 mg/shot. The MPD plasma spraying showed that a dense uniform ceramic film with above 1200 Vickers hardness was deposited. From the XPS spectra, the peak area ratio of Si/Al for the coating almost equaled that for the raw ceramic material, and the valence numbers of Al and Si did not change. Consequently, the quasi-steady high-enthalpy plasma generator was found to have a high potential for material processing and for applications to aerodynamic areas.
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Kazuhito Komiko: "Optical Measurement and Numerical Analysis of 10-KW-Class Steady-stete Arcjet Howfields" 19th Int. Symp. Space Technol. and Science. a-51. (1994)
Kazuhito Komiko:“10-KW级Steady-stete Arcjet Howfields的光学测量和数值分析”第19届Int。
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Hirokazu Tahara: "Plasma Features in Quasisteady MPD Channels" Proc. 24th Int. Elastic Propulsion Conf.Vol.2. 796-804 (1995)
Hirokazu Tahara:“准稳态 MPD 通道中的等离子体特征”Proc。
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Kazuhito Komiko et al.: "Optical Measurement and Numerical Analysis of 10kW-Class Steady-State Arcjet Flowfields" 19th Int.Symp.Space Technol.and Sci.a-51 (1994)
Kazuhito Komiko 等人:“10kW 级稳态电弧喷射流场的光学测量和数值分析”第 19 届 Int.Symp.Space Technol.and Sci.a-51 (1994)
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Kazunori Mitsuo: "Diognostics and Amalysis of Quasi-Steady One-Dimensional Magnetoplasmadynamic Flowfields" 19th Int. Symp. Space Technol. and Science. a-47. (1994)
Kazunori Mitsuo:“准稳态一维磁等离子体动力流场的诊断和分析”第 19 届 Int。
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Hirokazu Tahara: "Effects of Applied Magnetic Fields on Performance of a Quasisteady Magnetoplasmadynamic Arcjet" J. Propulsion and Power. Vol.11. 337-342 (1995)
Hirokazu Tahara:“应用磁场对准稳态磁等离子动力电弧喷射性能的影响”J.推进和动力。
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共 34 条
A Study on Inverse Calculation of Impact Load and Structural Response Based on the measured Strain
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批准号:23656551
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项目类别:Grant-in-Aid for Challenging Exploratory Research
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资助金额:$2.25万
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财政年份:2011
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Creation of Highly Dense Ceramic Films by Using Magneto-Plasma Dynamic Arc Jets
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财政年份:1999
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Physical Phenomena of Electric Thrusters in Space
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批准号:09044168
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项目类别:Grant-in-Aid for international Scientific Research
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资助金额:$6.14万
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财政年份:1997
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依托单位:
Understanding of Physical Phenomena for Development of Electric Propulsion Systems
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批准号:07305041
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项目类别:Grant-in-Aid for Scientific Research (A)
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资助金额:$14.78万
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财政年份:1995
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负责人:YOSHIKAWA Takao
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依托单位:
Discharge Feature and Acceleration Mechanism of Magnetoplasmadynamic Thrusters
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批准号:04452112
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资助金额:$4.35万
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财政年份:1992
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依托单位:
Operating Characteristics of Low Power Arcjets for Space Propulsion
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批准号:61460079
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财政年份:1986
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负责人:YOSHIKAWA Takao
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依托单位:
海外基金