A micro-vortex generating device with airflow auxiliary control

An auxiliary control and generating device technology, applied in transportation and packaging, through generation of vortex, supersonic aircraft, etc., can solve the problems of narrow applicable working conditions, unsatisfactory control effect, and inability to change the design shape, etc., to achieve extended application Working conditions and the effect of simplifying the structure of the device

Active Publication Date: 2021-11-16
CHINA ACAD OF AEROSPACE AERODYNAMICS
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  • Abstract
  • Description
  • Claims
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AI Technical Summary

Problems solved by technology

[0005] The technical problem solved by the invention is: Aiming at the problems in the current prior art that the micro-vortex generators of traditional supersonic aircraft have a narrow range of applicable conditions, cannot change the design shape, and have unsatisfactory control effects, a micro-vortex generator for airflow-assisted control is proposed. Vortex generator

Method used

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  • A micro-vortex generating device with airflow auxiliary control
  • A micro-vortex generating device with airflow auxiliary control
  • A micro-vortex generating device with airflow auxiliary control

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Embodiment Construction

[0022] A micro-vortex generating device with airflow auxiliary control, comprising a high-pressure air supply circuit, an airflow auxiliary control device, a microvortex generator 14, and a supersonic controlled surface 13. An aerodynamic configuration geometrically similar to the micro-vortex generator 14 is formed on the supersonic controlled surface 13, and the aerodynamic configuration is coupled with the micro-vortex generator 14 to enhance the flow control effect.

[0023] Wherein, the high-pressure gas supply circuit includes the gas storage cavity air inlet 1 , the gas storage cavity induction pipe 2 and the gas storage cavity 3 . The auxiliary airflow control device is composed of oblique slot air inlet, oblique slot air guide pipe, solenoid valve and oblique slot. The oblique slot air inlet includes No. Air hole 9, rear air intake hole 10 of the No. 2 oblique seam; the air duct of the oblique seam includes the front air pipe 4 of the No. 2 oblique seam, the front air...

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Abstract

A micro-vortex generating device with airflow auxiliary control, which mainly includes a high-pressure air supply circuit, an airflow auxiliary control device, a microvortex generator (14), and a supersonic controlled surface (13). The aerodynamic configuration similar to that of the micro-vortex generator is formed on the supersonic controlled surface. By controlling the solenoid valve, this aerodynamic configuration can be changed, and the control effect of the micro-vortex generator can be improved through airflow assistance. At the same time, it is extremely It greatly broadens the applicable working conditions of the micro vortex generator.

Description

technical field [0001] The invention relates to a micro-vortex generating device for airflow auxiliary control, which belongs to the field of supersonic aircraft control. Background technique [0002] Complicated flow separation generally exists in the internal and external flow fields of supersonic vehicles. This phenomenon leads to a sharp increase in wall turbulence and viscous dissipation, leading to adverse consequences such as increased drag, reduced lift, and premature stall. The nearby flow field is distorted, the total pressure recovery drops, the engine does not start, etc. Therefore, searching for an efficient and stable flow separation technology has become one of the important topics in the current high-speed aircraft technology research. [0003] Because of its simple structure and good control effect, the micro-vortex generator has become the most common technology in supersonic flow control. The micro-vortex generator will form a series of vortex ring struc...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C23/06B64C30/00
CPCB64C23/06B64C30/00Y02T50/10
Inventor 赵永胜杨辉魏兴吴军飞
Owner CHINA ACAD OF AEROSPACE AERODYNAMICS
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