共查询到20条相似文献,搜索用时 31 毫秒
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报告了一个用于低频射频天线网络LOFAR的160 Gbit/s 演示平台.文章介绍了LOFAR网络结构以及用于LOFAR长臂的OTDM/WDM系统结构,回顾并探讨了用于实现160 Gbit/s系统的关键技术,并介绍了实验室中实现该160 Gbit/s OTDM/WDM演示平台所采用的技术方案。出于经济性考虑,所有的关键系统功能都采用自己搭建方案. 相似文献
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A Prototype laser forming system 总被引:6,自引:0,他引:6
A non-contact laser forming (LF) demonstrator system was developed to demonstrate the process on a large primitive shape. The research that led to this development is described in this article. A fundamental study was carried out which examined the effects of laser-forming parameters on tokens of an aluminium and a titanium alloy. Energy, geometrical and metallurgical influences were investigated and are summarised here. Results of the study showed that LF of these aerospace materials is possible using a large operating envelope of laser-processing parameters. A range of metallurgical effects resulted on the titanium alloy and these are traced here. Depending on how the energy input was supplied to the plate surface, various geometrical effects resulted. These effects are discussed. Using the knowledge gathered from the fundamental study, a prototype LF system was built. The components of the system and the forming of a primitive shape on it are discussed. Conclusions from the study indicate that the future work lies in the development of the demonstrator for primitive 3-D shapes and the integration of a knowledge-based system. 相似文献
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S. M. Frolov V. S. Aksenov V. S. Ivanov 《Russian Journal of Physical Chemistry B, Focus on Physics》2011,5(4):664-667
A low-frequency demonstrator of the operation process of a pulse-detonation liquid-fuel rocket engine, intended for shaping
the future design of a new type of rocket engines for spacecraft control, is for the first time developed and tested. As a
result, the conditions are determined under which the demonstrator provides reliable deflagration-to-detonation transition
(DDT) in a single-pulse or repetition mode. Because DDT occurs within a very short distance (less than 10 bores of the detonation
tube), the operating frequency of the demonstrator can be substantially increased. 相似文献
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Buczynski R Szoplik T Taghizadeh MR Veretennicoff IP Thienpont H 《Optics letters》2002,27(20):1818-1820
We present a demonstrator photonic system for mathematical morphology image processing. Optically interconnected arrays of differential pairs of optoelectronic transceivers realize morphological erosion and dilation in an 8x8 pixel size image. 相似文献
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利用有机玻璃、排水管、水阀染料容器板等制作了流线演示仪,采用对工作液体染色的方法,避免了工作液体和有色液体的压力差.利用本仪器,对圆形障碍物、流线体和机翼模型周围的流线进行演示,流线稳定、清晰. 相似文献
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本文提供了一个精确设计麦克斯韦速率分布演示仪的理论方法,可以精确计算出伽尔顿模板底部的滑行曲线.以铊原子蒸汽的麦克斯韦速率分布为实例设计演示仪,给出滑行曲线的解析式. 相似文献
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S. M. Frolov V. S. Aksenov V. S. Ivanov I. O. Shamshin 《Russian Journal of Physical Chemistry B, Focus on Physics》2016,10(2):291-297
A demonstrator of a pulse detonation combustion chamber of original design based on a cyclic deflagration- to-detonation transition in a mixture of separately fed liquid hydrocarbon fuel (propane–butane mixture) and air was developed. Fire tests of the demonstrator with an attached air duct, operating frequencies of up to 20 Hz, were performed on a thrust measurement bench. During the tests, wave processes in the gasdynamic duct were monitored and fuel consumption rate and thrust force were measured. At a frequency of operation of the demonstrator within 2–15 Hz, the fuel-based specific impulse was ~1000 s. It is shown that a partial filling of the gasdynamic duct with fuel mixture makes it possible to increase the specific impulse up to ~1100 s. 相似文献
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《Comptes Rendus de l''Academie des Sciences Series IV Physics》2001,2(1):125-135
This paper proposes a design for a space borne demonstrator interferometer with imaging capabilities. This demonstrator would be a first step in the development of an operational astronomical instrument using aperture synthesis.Multiple aperture interferometry is a promising technique for high resolution imaging in space. Indeed the use of modular elements based on optical fibres represents an attractive low cost approach.The instrument is based on the use of independent triplets of telescope linked with optical fibres. For each triplet, only the phase closure of the system is measured. This does not require an accurate cophasing of the apertures and leads to realistic stability and control specifications. The complete instrument is then built by adding the desired number of such triplet modules. The detailed design of one module is described starting at level of the receiving telescopes down to the focal plane where the control of the stability of the optical path differences is performed as well as the scientific observations. The global operation of the system will also be described.We also briefly recall the technology validation activities which have shown on the ground the feasibility and performance of all components of such a systems as well as its end to end validation. 相似文献
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