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81.
裂纹对叶片固有频率影响的分析 总被引:2,自引:1,他引:2
给出了一种两条横向裂纹对叶片弯曲固有频率影响效果的分析方法。考虑的两种裂纹为周期载荷作用下产生的双面裂纹和脉冲载荷作用下产生的单面裂纹。分析中假设裂纹为沿叶宽等深度扩展的开口裂纹,同时将叶片看成无扭曲的短形等截面悬臂梁。结果表明,单纯选用固有频率识别裂纹参数,会过低估计裂纹严重程度;在可考察的裂纹深度范围内,单面和双面裂纹对固有频率的影响效果不显著。 相似文献
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S. M. Krimigis D. G. Mitchell D. C. Hamilton S. Livi J. Dandouras S. Jaskulek T. P. Armstrong J. D. Boldt A. F. Cheng G. Gloeckler J. R. Hayes K. C. Hsieh W.-H. Ip E. P. Keath E. Kirsch N. Krupp L. J. Lanzerotti R. Lundgren B. H. Mauk R. W. McEntire E. C. Roelof C. E. Schlemm B. E. Tossman B. Wilken D. J. Williams 《Space Science Reviews》2004,114(1-4):233-329
The magnetospheric imaging instrument (MIMI) is a neutral and charged particle detection system on the Cassini orbiter spacecraft designed to perform both global imaging and in-situ measurements to study the overall configuration and dynamics of Saturn’s magnetosphere and its interactions with the solar wind, Saturn’s atmosphere, Titan, and the icy satellites. The processes responsible for Saturn’s aurora will be investigated; a search will be performed for substorms at Saturn; and the origins of magnetospheric hot plasmas will be determined. Further, the Jovian magnetosphere and Io torus will be imaged during Jupiter flyby. The investigative approach is twofold. (1) Perform remote sensing of the magnetospheric energetic (E > 7 keV) ion plasmas by detecting and imaging charge-exchange neutrals, created when magnetospheric ions capture electrons from ambient neutral gas. Such escaping neutrals were detected by the Voyager l spacecraft outside Saturn’s magnetosphere and can be used like photons to form images of the emitting regions, as has been demonstrated at Earth. (2) Determine through in-situ measurements the 3-D particle distribution functions including ion composition and charge states (E > 3 keV/e). The combination of in-situ measurements with global images, together with analysis and interpretation techniques that include direct “forward modeling’’ and deconvolution by tomography, is expected to yield a global assessment of magnetospheric structure and dynamics, including (a) magnetospheric ring currents and hot plasma populations, (b) magnetic field distortions, (c) electric field configuration, (d) particle injection boundaries associated with magnetic storms and substorms, and (e) the connection of the magnetosphere to ionospheric altitudes. Titan and its torus will stand out in energetic neutral images throughout the Cassini orbit, and thus serve as a continuous remote probe of ion flux variations near 20R
S (e.g., magnetopause crossings and substorm plasma injections). The Titan exosphere and its cometary interaction with magnetospheric plasmas will be imaged in detail on each flyby. The three principal sensors of MIMI consists of an ion and neutral camera (INCA), a charge–energy–mass-spectrometer (CHEMS) essentially identical to our instrument flown on the ISTP/Geotail spacecraft, and the low energy magnetospheric measurements system (LEMMS), an advanced design of one of our sensors flown on the Galileo spacecraft. The INCA head is a large geometry factor (G ∼ 2.4 cm2 sr) foil time-of-flight (TOF) camera that separately registers the incident direction of either energetic neutral atoms (ENA) or ion species (≥5∘ full width half maximum) over the range 7 keV/nuc < E < 3 MeV/nuc. CHEMS uses electrostatic deflection, TOF, and energy measurement to determine ion energy, charge state, mass, and 3-D anisotropy in the range 3 ≤ E ≤ 220 keV/e with good (∼0.05 cm2 sr) sensitivity. LEMMS is a two-ended telescope that measures ions in the range 0.03 ≤ E ≤ 18 MeV and electrons 0.015 ≤ E≤ 0.884 MeV in the forward direction (G ∼ 0.02 cm2 sr), while high energy electrons (0.1–5 MeV) and ions (1.6–160 MeV) are measured from the back direction (G ∼ 0.4 cm2 sr). The latter are relevant to inner magnetosphere studies of diffusion processes and satellite microsignatures as well as cosmic ray albedo neutron decay (CRAND). Our analyses of Voyager energetic neutral particle and Lyman-α measurements show that INCA will provide statistically significant global magnetospheric images from a distance of ∼60 R
S every 2–3 h (every ∼10 min from ∼20 R
S). Moreover, during Titan flybys, INCA will provide images of the interaction of the Titan exosphere with the Saturn magnetosphere every 1.5 min. Time resolution for charged particle measurements can be < 0.1 s, which is more than adequate for microsignature studies. Data obtained during Venus-2 flyby and Earth swingby in June and August 1999, respectively, and Jupiter flyby in December 2000 to January 2001 show that the instrument is performing well, has made important and heretofore unobtainable measurements in interplanetary space at Jupiter, and will likely obtain high-quality data throughout each orbit of the Cassini mission at Saturn. Sample data from each of the three sensors during the August 18 Earth swingby are shown, including the first ENA image of part of the ring current obtained by an instrument specifically designed for this purpose. Similarily, measurements in cis-Jovian space include the first detailed charge state determination of Iogenic ions and several ENA images of that planet’s magnetosphere.This revised version was published online in July 2005 with a corrected cover date. 相似文献
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某产品一号肋锻件筋条高、隔框多,形状复杂,工艺成型困难。本文论述了该锻件的成型工艺方法,包括设备选择、模具设计、锻造工艺、热处理等。 相似文献
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讨论了少烟丁羟合推进剂高压下侵蚀燃烧与装药装填密度的关系,给出了计算变截面装药气流速度方程,总结了在此推进剂在P≥15.0MPa下侵蚀燃烧规律,为装药设计提供了依据。 相似文献
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介绍了一种以超纯水为电解液的电解加工工艺方法,即超纯水电解加工技术.研究了阳离子交换膜在超纯水中的水解离机理及工作特性,分析其在超纯水电解加工过程中的作用机理,并进行了水解离试验研究.结果表明:电流密度达到了3.7 A/cm^2,电场强度约为2 MV/m,已进入微细电解加工去除材料要求范围,为超纯水微细电解加工的应用奠定了基础. 相似文献
89.
基于VXI总线和虚拟仪器技术,研制开发了用于外场的模拟式电子控制器检测软件,并对软件开发的过程和要求进行了分析,重点解决了程序设计中的需求分析和模块化设计问题。 相似文献
90.
数控展成电解加工的阴极结构及流场研究 总被引:1,自引:0,他引:1
介绍了应用数控展成电解在整体叶轮毛坯上开槽时的流场特点,讨论了阴极结构对加工间隙内流场的影响规律,并相应对阴极的结构设计提出了一些建议。 相似文献