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DEVICE FOR DEFINITION OF AERODYNAMIC CHARACTERISTICS OF MODEL IN SUPERSONIC WIND TUNNEL

机译:超音速风洞模型气动特性的确定装置

摘要

FIELD: measurement equipment.;SUBSTANCE: invention relates to measurement equipment, in particular - to devices for definition of aerodynamic characteristics of different modification models in a supersonic wind tunnel whereby one defines summary aerodynamic characteristics of a full-scale aircraft travelling at a supersonic speed and may be used in aviation and aerospace industry. In the device for definition of aerodynamic characteristics of a model in a supersonic wind tunnel containing a model with a detachable head part fixed on strain-gage weighers by way of setting it on the conic part and fixed with a nut connected with a holder installed inside the tunnel, a telecommunication station and a control panel. The strain-gage weighers are fixed on an adapter. Outside the latter a circular cavity is arranged with holes in the butt end for flexible hoses connected with the cooling system and grooves for sealing elements positioned inside the shell contacting with the model head and tail parts. The strain-gage weighers are contained inside two cylindrical thermally insulating casings with The front casing mounted on the shell while the rear casing is mounted on the holder at a gap relative to the front one. The cooling system including the flexible hoses, the liquid tank and the pump is mounted inside the tunnel preparatory compartment.;EFFECT: enhanced precision and reliability of measurement of aerodynamic characteristics of a model in a supersonic wind tunnel.;1 dwg
机译:技术领域本发明涉及测量设备,尤其涉及用于定义超音速风洞中的不同修改模型的空气动力学特性的设备,其中,该设备定义超音速飞行的全尺寸飞机的简要空气动力学特性。并可用于航空和航天工业。在用于定义超音速风洞中的模型的空气动力学特性的装置中,该模型包括通过将模型安装在圆锥形部分上并通过与固定在内部的支架相连的螺母来固定的模型,该模型具有可拆卸的头部固定在应变仪秤上隧道,电信站和控制面板。应变计称重器固定在适配器上。在后者的外部设有一个圆形空腔,该空腔的对接端有孔,用于与冷却系统连接的挠性软管,以及用于密封元件的凹槽,该密封元件位于壳体内部,与模型的头部和尾部接触。应变计称量器包含在两个圆柱形的隔热外壳内,前外壳安装在外壳上,后外壳相对于前外壳安装在支架上。包括柔性软管,储液罐和泵在内的冷却系统安装在隧道准备室内。效果:提高了超音速风洞中模型空气动力学特性的测量精度和可靠性; 1 dwg

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