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Un ejecteur haute frequence de matieres granulaires A high frequency ejector for granular solids.

机译:用于颗粒状固体的高频喷射器。

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摘要

This study addresses the design challenges of a proposed Micro Pulse Detonation Engine (MPDE), a micropropulsion system devised to meet the needs of smallsats. It focusses in particular on one subsystem of the proposed MPDE, the explosive delivery system, hereafter refered to as an ejector of granular materials.;This study has three major goals: (1) evaluate different ways of building ejectors of granular materials in space, (2) propose a design for an ejector of granular materials that could eventually be used to achieve ejection rates of 10 kHz, and (3) evaluate the new designs performance.;We thus begin by reviewing devices that have been built or proposed in the past for ejecting granular materials. Finding them lacking for the objectives of the present project, we evaluate several other different ways of achieving granule ejection in the zero gravity environment of space, based on other previous work with granular materials generally.;We conclude that the artificial gravity induced within a spinning apparatus provides for many of the design requirements in a way that none of the other options do. We then go on to discuss the novel challenges a rotating ejector of solids faces, and propose a way of overcoming them. We present the design of the simplest concept we could come up with to achieve controlled ejection from the rotating device.;Finally, the performance of this system is evaluated experimentally, using glass ballotini as the granular material. We find that we are able to demonstrate an ejection rate of 50 ejections per second with the device rotating at 10 rotations per second, with the possibility of attaining even higher ejection rates at higher rotational velocities. We conclude that this device demonstrates that there is a very great likelihood that future designs based closely on it will be able to achieve the desired 10 kHz ejection rate, which is the highest ejection rate at which the proposed MPDE can operate while remaining in the higher efficiency vacuum mode.;Keywords: propulsion, detonation, thruster, satellite, ejection, granular flow, mechanical' ejector.
机译:这项研究解决了拟议中的微脉冲爆震引擎(MPDE)的设计挑战,该引擎设计用于满足小型卫星的需求。它特别关注拟议的MPDE的一个子系统,即炸药输送系统,以下简称为颗粒物质的喷射器。该研究的三个主要目标是:(1)评价在空间中构建颗粒物质喷射器的不同方法, (2)提出了一种可用于最终实现10 kHz喷射速率的粒状材料喷射器的设计,并且(3)评估了新设计的性能。因此,我们首先回顾了已在制造或建议中使用的设备过去用于喷射粒状材料。发现它们缺乏本项目的目标,我们根据以前对粒状材料所做的其他工作,评估了在零重力空间环境中实现颗粒喷射的其他几种不同方法。我们得出结论,纺丝过程中产生的人工重力设备以其他任何选择都无法满足的方式提供许多设计要求。然后,我们继续讨论旋转固体喷射器所面临的新颖挑战,并提出克服这些挑战的方法。我们提出了最简单的概念设计,可以实现从旋转设备中进行受控喷射。最后,使用玻璃ballotini作为颗粒材料,通过实验评估了该系统的性能。我们发现,当设备以每秒10转的速度旋转时,我们能够证明每秒50次喷射的喷射速率,并且有可能在更高的旋转速度下获得更高的喷射速率。我们得出的结论是,该器件表明,很有可能未来基于它的设计将能够实现所需的10 kHz发射速率,这是建议的MPDE可以在保持较高频率的同时运行的最高发射速率。高效真空模式。关键词:推进,爆轰,推进器,卫星,喷射,颗粒流,机械式喷射器。

著录项

  • 作者

    Jensen, Michael.;

  • 作者单位

    Universite de Sherbrooke (Canada).;

  • 授予单位 Universite de Sherbrooke (Canada).;
  • 学科 Engineering Aerospace.;Engineering Mechanical.
  • 学位 M.Sc.A.
  • 年度 2012
  • 页码 106 p.
  • 总页数 106
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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