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A plasma vortex generator-based inward-rotating inlet assembly and control method

A technology of internally rotating inlets and vortex generators, which is applied in the direction of machines/engines, jet propulsion devices, gas turbine devices, etc., can solve problems such as complex configuration, difficulty in design and production, loss of high-quality flow, etc., and achieve anti- The effect of improved reverse pressure gradient capability, improved performance, and improved total pressure recovery coefficient

Active Publication Date: 2021-09-24
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Each of these control methods has certain limitations. For the currently commonly used blowing and deflation control method, the air inlet based on this control method needs to arrange the blowing and deflation structure and the air flow channel, so the configuration is generally more complicated, and the blowing There are certain requirements on the air source during control, and part of the high-quality flow will inevitably be lost during deflation control; for the vortex generator control method, there are certain difficulties in the design and production of the body equipped with the vortex generator; and variable geometry The control method has higher requirements for the design method and processing technology of the intake port

Method used

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  • A plasma vortex generator-based inward-rotating inlet assembly and control method
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  • A plasma vortex generator-based inward-rotating inlet assembly and control method

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Embodiment Construction

[0020] Below in conjunction with accompanying drawing, the present invention is further described.

[0021] Such as figure 1 , 2 As shown in , 3, it is an embodiment of an inwardly rotating inlet assembly based on a plasma vortex generator provided by the present invention. The air inlet assembly includes a body plane 2 and an inward turning air inlet installed on the body plane 2 . The inner turning air inlet includes a lip cover 5, side walls 4 located on both sides of the lip cover, and an internal compression surface 3. The lip cover 5, side walls 4 and the surface of the internal flow channel form an internal flow air channel, and the internal flow air An airflow channel 6 is connected to the rear end of the channel. The inner compression surface 3 is a connection compression surface connecting the surface of the inner flow channel and the body plane 2 (inner compression means that the compression surface is formed by inward compression relative to the body plane). Th...

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Abstract

The invention discloses a plasma vortex generator-based inward-rotating air inlet component and a control method thereof. The assembly includes a machine body plane and an inward turning air inlet body, wherein one or more sets of arc spark discharge plasma vortex generators are arranged at a certain distance upstream along the compression surface below the machine body plane. This method uses the flow vortex formed by the interaction between the plasma jet and the free flow to promote the momentum exchange between the main flow and the low-energy flow in the boundary layer, enhance the ability of the boundary layer to resist the reverse pressure gradient, and reduce the shock wave / boundary layer induced by the downstream internal compression surface. The interference separation zone has a certain delay or inhibition effect, thereby effectively improving the performance of the intake port. Compared with the traditional method, the control method proposed by the present invention does not require additional air source, no flow loss, no additional resistance, and the control method is accurate and efficient, which has great advantages for the wide speed range and integrated design of the internal rotation air inlet. important promotion.

Description

technical field [0001] The invention belongs to the field of supersonic flow control, and in particular relates to an inwardly turning air inlet assembly and a control method for the air inlet assembly. Background technique [0002] With the continuous development of inlet aerodynamic technology, the three-dimensional inwardly turning inlet designed based on the streamline tracing method has gradually attracted the attention of researchers. The compression surface of the inwardly turning inlet is a typical three-dimensional curved surface. The generation of streamlines emanating from a given inlet profile of the inlet is traced in the reference axisymmetric inner cone flow field. Theoretically, the inward turning inlet designed according to streamline tracing can not only obtain high compression efficiency and flow field uniformity by maintaining the three-dimensional compression characteristics of the reference flow field, but also have the design freedom of the shape of th...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F02C7/042F02C7/057
CPCF02C7/042F02C7/057
Inventor 张悦陈亮王子运谭慧俊李鑫郭赟杰王超
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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