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PROPULSION NOZZLE FOR THE EXPANSION OF A SUPERSONIC GAS JET

机译:超音速喷气发动机膨胀的推进喷嘴

摘要

The nozzle (21) has a skirt (27) in which a gas jet (25) is released before being ejected towards a surrounding medium (55) outside the skirt along an axis (X) of the nozzle. A channel (29) conveys fluid close to its free end (32). A collection unit formed of chute (33) and walls, collects the fluid e.g. hydrogen, around the skirt. A channel (29) emerges in the unit. Discharge unit formed of circumferential deflecting wall (41), half-cup (47), expansion chamber and inlet, discharges the collected fluid in the form of supersonic fluid flow (57) accelerated along a direction following the axis.
机译:喷嘴(21)具有裙部(27),在沿着喷嘴的轴线(X)朝向裙部外部的周围介质(55)喷射之前,在其中释放出气体射流(25)。通道(29)在其自由端(32)附近输送流体。由溜槽(33)和壁形成的收集单元收集例如液体。氢气,围绕裙子。通道(29)出现在设备中。由周向偏转壁(41),半杯(47),膨胀室和入口形成的排放单元以沿沿着轴线的方向加速的超音速流体流(57)的形式排放收集的流体。

著录项

  • 公开/公告号EP2209981B1

    专利类型

  • 公开/公告日2017-03-08

    原文格式PDF

  • 申请/专利权人 CENTRE NATIONAL DETUDES SPATIALES;

    申请/专利号EP20080853466

  • 发明设计人 BOCCALETTO LUCA;

    申请日2008-11-06

  • 分类号F02K9/97;F02K9/82;F02K9/88;

  • 国家 EP

  • 入库时间 2022-08-21 14:06:04

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