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SELF-EXCITATION OSCILLATION JET IMPACT NOZZLE FOR COMPLEX FLUID ATOMIZATION

机译:复杂流体雾化的自激振荡射流冲击喷嘴

摘要

A self-excitation oscillation jet impact nozzle for complex fluid atomization comprises a liquid collecting cavity housing (1), a jet faceplate (2) and a resonant cavity housing (4). A screw hole, which is connected to a supplying pipeline, is provided in the upper center of the liquid collecting cavity housing. The liquid collecting cavity housing is coupled with the jet faceplate by a flange and is sealed with a sealing gasket. A hollow cavity between the liquid collecting cavity housing and the jet faceplate is a liquid collecting cavity (12). A frustum cone-like concave space (23) is provided in the bottom center of the jet faceplate. Two or more jet holes are symmetrically arranged perpendicularly to lateral surfaces of the frustum cone-like concave space. The axes of the jet holes make a certain angle with the center axis of the jet faceplate and all of the axes of the jet holes intersect in an intersection which belongs to the center axis of the jet faceplate. Jet-hole inlets (21) which comprise inner screws are provided in frustum cone side surfaces at the upper center of the jet faceplate. A resonant cavity inlet (42) is provided on the resonant cavity housing which comprises outer screws and is coupled with the jet faceplate by the inner screws of the jet-hole inlets, and two or more resonant cavities (41) is formed between the resonant cavity housing and the jet faceplate. The impact nozzle achieves better atomization effect for complex fluid atomization and improves the combustion efficiency and specific impulse of the liquid rocket engine.
机译:一种用于复杂流体雾化的自激振荡射流冲击喷嘴,包括液体收集腔壳体(1),喷射面板(2)和谐振腔壳体(4)。在集液腔壳体的上部中央设有与供给管路连接的螺孔。液体收集腔壳体通过法兰与喷射面板相连,并用密封垫密封。在液体收集腔壳体和喷射面板之间的中空腔是液体收集腔(12)。在喷射面板的底部中央设有截头圆锥形的凹入空间(23)。两个或多个喷射孔垂直于截头锥体圆锥形凹入空间的侧面对称地布置。喷射孔的轴线与喷射面板的中心轴线成一定角度,并且喷射孔的所有轴线在属于喷射面板的中心轴线的相交处相交。在喷射面板的上部中央的平截头圆锥体侧面上设有包括内部螺钉的喷射孔入口(21)。在共振腔壳体上设置有共振腔入口(42),该共振腔入口(42)包括外螺钉并且通过喷射孔入口的内螺钉与喷射面板联接,并且在共振腔之间形成两个或更多个共振腔(41)。腔体外壳和喷嘴面板。该冲击喷嘴对复杂的流体雾化具有更好的雾化效果,并提高了液体火箭发动机的燃烧效率和比冲。

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