共查询到20条相似文献,搜索用时 234 毫秒
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由于舰载机在着舰下滑阶段采用的是反区(backside)操纵技术,这种驾驶操纵需要飞行员小量高频地推拉油门,这就要求油门杆操纵力足够小,以满足飞行员精确控制飞行轨迹的需求。介绍了油门助力装置在舰载机着舰下滑过程中的应用,提出了油门助力装置评估的方法。飞行试验结果表明,所提方法能够对油门助力装置给出客观评估,同时对后续其他操纵系统的评估提供参考。 相似文献
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精度是拉索式操纵系统的重要性能指标之一,其高低直接影响发动机的稳态和瞬态性能。介绍拉索 式发动机操纵系统的组成及原理,通过拉索式操纵系统精度试验,从单程精度、回程差和重复性精度三个维度 分析其精度特性;采用单一变量法,通过试验依次分析弹簧力臂和刚度系数、拉索导向套路线布置以及拉索的 长度等对操纵系统精度的影响。结果表明:拉索式操纵系统单程精度绝对值小于5%,在死区外的范围回程差 小于3%,重复性精度小于2%;可通过合理设计拉索长度及弹簧刚度系数缩小死区范围;拉索导向套两端的横 向间距过大会降低操纵系统精度。 相似文献
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某型直升机发动机油门操纵为刚性操纵结构形式,大修时需要对每根拉杆进行检查,检查合格后再装回原机。由于修理资料中没有对每根拉杆的长度进行规定,导致发动机油门操纵调整具有一定难度,且调整周期长。本文根据发动机油门操纵的结构原理,提出了调整方法及要求,并针对调整中出现的故障进行了原因分析和排除方法的介绍。 相似文献
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徐州陆伟铭谢陵李慧颖 《民用飞机设计与研究》2016,(1):72
在侧杆操纵的民机中,侧杆的操纵力需要满足飞行品质以及适航规章的要求,因此必须对侧杆的操纵力进行准确测量。针对侧杆具有的双自由度运动及侧杆表面形态复杂的特性,设计了一套操纵力测量系统。该系统能够精确控制侧杆的运动方向,使侧杆在一个平面内运动,并通过特殊的机制使力传感器与侧杆运动轴线垂直,保证测试的精度。基于LabView 设计了测试软件,能够实时地显示力、位移以及滞环曲线。 相似文献
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Solar Radio Group Utrecht 《Space Science Reviews》1974,16(1-2):45-89
One of the purposes of this paper is to stress the fact that the solar type III radio burst is not the simple phenomenon it is sometimes suggested to be. Therefore we present in sections 1 to 7 its various properties derived from observations of the past 20 years. In Section 2 a few theories invoked to describe the basic features are reviewed. This may serve as an introduction to the subject. 相似文献
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The primary agent for Type Ia supernova cosmology is the uniformity of their appearance. We present the current status, achievements and uncertainties. The Hubble constant and the expansion history of the universe are key measurements provided by Type Ia supernovae. They were also instrumental in showing time dilation, which is a direct observational signature of expansion. Connections to explosion physics are made in the context of potential improvements of the quality of Type Ia supernovae as distance indicators. The coming years will see large efforts to use Type Ia supernovae to characterise dark energy. 相似文献
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《中国航空学报》2023,36(3):96-106
The interactions of oblique/bow shock waves are the key flow phenomena restricting the design and aerothermodynamic performance of high-speed vehicles. Type III and Type IV Shock/Shock Interactions(SSIs) have been extensively investigated, as such interactions can induce abnormal aerodynamic heating problems in hypersonic flows of vehicles. The transition process between these two distinct types of shock/shock interactions remains unclear. In the present study, a subclass of shock/shock interaction configuration is revealed and defined as Type IIIa. Type IIIa interaction can induce much more severe aerodynamic heating than a Type IV interaction which was ever reported to be the most serious in literature. The intense aerodynamic heating observed in this configuration highlights a new design point for the thermal protection system of hypersonic vehicles. A secondary Mach interaction between shock waves in the supersonic flow path of a Type III configuration is demonstrated to be the primary mechanism for such a subclass of shock/shock interaction configuration. 相似文献
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A. D. Fokker 《Space Science Reviews》1963,2(1):70-90
Conclusion We have got a reasonably clear idea of the various forms under which the type IV continuum emission may appear. Also we can imagine what kind of processes come into play during a type IV event. But the insight gained so far applies to the general case. Individual cases are widely different, and we are still far from understanding why a given event behaves as it does. For instance, why are metric responses lacking at a certain big microwave outburst, or why is the decimetric component particularly strong or prolonged on certain occasions? One can imagine that such questions would receive an answer if one were allowed to see the configuration of magnetic lines of force above the activity region !Does the type IV event tell us a fine story of the interplay of energetic particles and streams of particles with coronal magnetic fields ? Maybe the story would be a fine one if the language could be understood. At present we know only a few words of it; for this reason to us the story is very fragmentary. First of all, however, the message should be recorded far more completely than has been done so far. The number of observations that should be made of one and the same event is tremendous; the program comprises:1) spectral observations from 1000 Mc/s down to the lowest frequencies; 2) single frequency observations at a great many wavelengths covering the whole radio spectrum; 3) measurements of polarization and 4) determinations of position and angular extent in at least every octave of the whole radio spectrum.Especially as regards the latter two points, the present situation is still very unsatisfactory, though good work has been done already in Japan. The realization of a complete recording of phenomena during a type IV event calls for a combined effort of several observatories.Very encouraging are the established relations between solar type IV events and terrestrial phenomena. From an analysis of solar cosmic ray events as recorded on several places on the earth, interesting inferences have been drawn regarding the travelling conditions of particles in interplanetary space (cf.
Carmichael, 1962). Likewise, one may expect interesting information on the behaviour of interplanetary particle clouds of solar origin from (interferometric) observations of decametric radio emission on the occasion of type IV events.The occurrence of a major type IV event enables forecasters to predict successfully geomagnetic and ionospheric storms. Type IV events will determine at what times certain space research experiments will be launched in the next solar cycle. One should like to be able to indicate the probability for the occurrence of type IV solar radio flares themselves. It is known that these flares generally occur in complex sunspot groups; but a complex sunspot group does not of necessity imply the occurrence of a type IV flare. Observations of coronal condensations at microwave frequencies with a high resolution interferometer may help sorting out those centres of activity that are most likely to produce type IV flares. 相似文献
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Renishaw公司 《航空制造技术》2009,(20)
TONiC是Renishaw公司推出的新款超小型非接触式光栅,在线性和旋转应用中均可达到10m/s的速度和高至5nm的分辨率.TONiC显著提高了Renishaw现有高速非接触式光栅的性能,同时又进一步改善了信号稳定性和长期可靠性,成本低,简便性无与伦比. 相似文献
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