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An active drag-reduction system and a method of reducing drag experienced by a vehicle

机译:主动减阻系统和减少车辆经历的阻力的方法

摘要

It is desirable to minimise all forms of trailing vortices from a moving vehicle, whether they are from turbulent form drag of a vehicle or from vortex drag. Wingtip vortices on aircraft can persist for relatively long times (of the order of several minutes after the passage of an aircraft) which can cause danger to other aircraft, in particular around airfields where time must be left between subsequent take-offs and/or landings on a given runway for such vortices to dissipate. According to a first aspect of the present invention, there is provided an active drag-reduction system having first (22) and second (24) fluid outlets located on a vehicle (10) adjacent to a low pressure (drag) region (12), wherein fluid ejected from the second fluid outlet (24) is at a higher pressure / ejection velocity than from the first fluid outlet (22). Turbulent and/or low pressure regions adjacent to vehicles are not uniform, but rather have a varying intensity. For instance, the centre of a region may have a lower pressure and/or more turbulent nature than the periphery of the region. In this way, therefore, the present invention allows the system of the present invention to inject relatively higher pressure air (or relatively higher speed air) into the relatively lower pressure / more turbulent part of the low pressure / turbulent region, and relatively lower pressure air (or relatively lower speed air) into the relatively higher pressure / less turbulent part of the low pressure / turbulent region, compared to each other.
机译:希望使来自移动车辆的所有形式的尾随涡流最小化,无论它们来自车辆的湍流形式的阻力还是来自涡流的阻力。飞机上的翼尖涡流可能会持续较长时间(飞机通过后几分钟),这可能对其他飞机造成危险,特别是在飞机场周围,在随后的起飞和/或着陆之间必须留出时间在给定的跑道上消散这种涡流。根据本发明的第一方面,提供了一种主动减阻系统,该主动减阻系统具有位于车辆(10)上的邻近低压(阻力)区域(12)的第一(22)和第二(24)流体出口。 ,其中从第二流体出口(24)喷射的流体具有比从第一流体出口(22)更高的压力/喷射速度。与车辆相邻的湍流和/或低压区域不是均匀的,而是具有变化的强度。例如,区域的中心可以具有比区域的外围更低的压力和/或更湍流的性质。因此,以这种方式,本发明允许本发明的系统将相对较高压力的空气(或相对较高速度的空气)注入到较低压力/较低湍流区域的较湍流部分和相对较低压力中彼此相比,空气(或速度相对较低的空气)进入低压/湍流区域的相对较高压力/较少湍流的部分。

著录项

  • 公开/公告号AU2016421471A1

    专利类型

  • 公开/公告日2019-04-18

    原文格式PDF

  • 申请/专利权人 OGAB LIMITED;

    申请/专利号AU20160421471

  • 发明设计人 ELOGAB OSAMA;ELOGAB HATEM;

    申请日2016-09-05

  • 分类号B62D37/02;

  • 国家 AU

  • 入库时间 2022-08-21 11:56:41

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