Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

A method to effectively prolong the flow time of a large-scale free piston high-enthalpy pulsed wind tunnel

A technology with flow time and large size, applied in the field of wind tunnel test, it can solve the problems of short wind tunnel test time, affecting wind tunnel test ability, hidden danger of piston and wind tunnel, etc., so as to prolong the constant pressure driving time and increase the safety margin. amount, the effect of reducing interference

Active Publication Date: 2021-06-11
CHINA ACAD OF AEROSPACE AERODYNAMICS
View PDF8 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

For large-scale free-piston high-enthalpy pulsed wind tunnels, due to the large inner diameter of the shock tube, after the rupture of the diaphragm of the main clamping mechanism, the acceleration of the free piston at the end of the compression tube is too fast, causing safety hazards to the piston and the wind tunnel. Hidden dangers, while reducing the constant pressure driving time of the compression tube, the test time of the wind tunnel is too short, which affects the test capability of the wind tunnel
At present, there is no relevant technology to effectively solve the wind tunnel test capability

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • A method to effectively prolong the flow time of a large-scale free piston high-enthalpy pulsed wind tunnel
  • A method to effectively prolong the flow time of a large-scale free piston high-enthalpy pulsed wind tunnel
  • A method to effectively prolong the flow time of a large-scale free piston high-enthalpy pulsed wind tunnel

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0044] Below in conjunction with accompanying drawing and specific embodiment the present invention is described in further detail:

[0045] The present invention provides a method for effectively prolonging the flow time of a large-scale free-piston high-enthalpy pulsed wind tunnel, and improves the test capability of the wind tunnel by adding a nozzle configuration 3 to the main mantle section 2 and the shock tube 4 . By reducing the flow rate of gas at the end of the compression tube entering the shock tube 4 after the rupture of the main sandwich section 2, the deceleration time of the heavy piston running in the compression tube 1 is prolonged, the constant pressure driving time of the wind tunnel is extended, and the safety margin of the piston operation is increased. to slow down the interference of the expansion wave system generated by the rupture of the main sandwich section 2 on the contact discontinuity, thereby effectively prolonging the running time of the wind tu...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The method for effectively prolonging the flow time of a large-scale free-piston high-enthalpy pulsed wind tunnel involves the technical field of wind tunnel testing; it includes the following steps: step 1, dividing the nozzle configuration into a contraction section AT and an expansion section TF in the axial direction; the contraction section AT and the expansion section TF are connected along the axial direction; the intersection point T is the position of the throat; the position of the throat T is determined; step 2, based on the throat T, the expansion section TF is divided into the first segment TC and the second segment CE and the third segment EF; respectively design the pipeline configurations of the first segment TC, the second segment CE and the third segment EF; step 3, taking the throat T as the benchmark, divide the contraction segment AT into contraction The front section AB and the contraction rear section BT; the pipeline configurations of the contraction front section AB and the contraction rear section BT are respectively designed; the invention effectively prolongs the running time of the wind tunnel flow field; at the same time, the operating state of the wind tunnel can be adjusted by changing the inner diameter of the throat , It is also convenient to replace parts that are partially ablated in the throat due to high temperature.

Description

technical field [0001] The invention relates to the technical field of wind tunnel tests, in particular to a method for effectively prolonging the flow time of a large-scale free piston high-enthalpy pulse wind tunnel. Background technique [0002] The large-scale free-piston high-enthalpy pulsed wind tunnel is one of the main ground simulation devices for studying high-temperature real gas effects, and it has the ability to simulate ultra-high-speed flow. Under the condition of ultra-high-speed flow, the free flow at the nozzle outlet has a scale effect. In order to reduce the influence of the absolute size of the nozzle on the free flow, the size of the nozzle needs to be large enough, and the corresponding size of the shock tube and the size of the compression tube are also large. For large-scale free-piston high-enthalpy pulsed wind tunnels, due to the large inner diameter of the shock tube, after the rupture of the diaphragm of the main clamping mechanism, the accelera...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Patents(China)
IPC IPC(8): G01M9/06
CPCG01M9/065
Inventor 谌君谋陈星毕志献张冰冰李辰孙日明宋可清
Owner CHINA ACAD OF AEROSPACE AERODYNAMICS
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products