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

Supersonic wind tunnel propeller numerical model measurement and verification system and control method thereof

A technology for verifying systems and numerical models. It is used in measurement devices, aerodynamic tests, and testing of machine/structural components. It can solve the problems of inability to simulate propellers of different specifications, interference of propellers in supersonic wind tunnels, and high manufacturing costs. , to achieve the effect of simple structure, excellent performance conditions and low manufacturing cost

Active Publication Date: 2020-09-25
INST OF ENGINEERING THERMOPHYSICS - CHINESE ACAD OF SCI +1
View PDF9 Cites 6 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The present invention aims at the above-mentioned deficiencies existing in the existing analog dynamic measurement system, and provides a supersonic wind tunnel propeller numerical model measurement and verification system, which solves the problem that the existing analog dynamic measurement system has complex structure, high manufacturing cost, and cannot simulate A variety of propellers with different specifications, poor comprehensiveness and other technical problems, at the same time, a control method is provided, which solves the technical problem that the error generated by a single measurement system will interfere with the propeller test in a supersonic wind tunnel

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
  • Supersonic wind tunnel propeller numerical model measurement and verification system and control method thereof
  • Supersonic wind tunnel propeller numerical model measurement and verification system and control method thereof
  • Supersonic wind tunnel propeller numerical model measurement and verification system and control method thereof

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0032] Such as Figure 1-2 As shown, a supersonic wind tunnel propeller numerical model measurement verification system, the measurement verification system includes:

[0033] Different specification propeller multifunctional measuring device 1, described different specification propeller multifunctional measuring device 1 comprises box-type six-component balance 14, drive shaft 16, and described box-type six-component balance 14 is provided with servo motor 13, and described servo motor 13 The output shaft is connected to the drive shaft 16 through a spline, and the drive shaft 16 is surrounded by a torque speed sensor 17, and the front end of the drive shaft 16 is connected to propellers 15 of different specifications through flanges;

[0034] PLC control unit 2, data acquisition module 3 and PC 4, the PC 4 is used to control the PLC control unit 2 to drive the servo motor 13 in the propeller multifunctional measurement device 1 of different specifications to provide the req...

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 invention relates to the technical field of supersonic wind tunnel propeller power measurement test verification. The invention particularly relates to a supersonic wind tunnel propeller numericalmodel measurement and verification system and a control method thereof. A torque and rotating speed integrated sensor and a box type six-component balance are combined to measure performance parameters of a servo motor and a propeller, parameters such as propeller tension, lift force, torque, rotating speed (a servo motor and a propeller) and vibration are obtained in real time and sent into a real-time analysis system, a closed-loop design verification model of the torque, the bending moment of the balance, the rotating speed of the propeller and the rotating speed of the motor is formed, and the interference influence of errors generated by a single measurement system on a supersonic wind tunnel propeller test is avoided. A vibration sensor is used for monitoring and measuring the system state in real time, dangerous state points in the test process are avoided, the whole system is placed in a high-altitude environment simulation cabin, the whole structure is vertically installed onthe windward side of the center of a wind tunnel test section, and the system is applied to tests of propellers of different specifications in a supersonic wind tunnel in the high-altitude environment.

Description

technical field [0001] The invention relates to the technical field of supersonic wind tunnel propeller dynamic measurement test verification, in particular to a supersonic wind tunnel propeller numerical model measurement verification system and a control method thereof. Background technique [0002] At present, there is no supporting equipment for power acquisition in the high-altitude environment, and it is impossible to obtain performance parameters such as propeller pull, lift, torque, rotational speed (servo motor, propeller), and vibration for real-time evaluation of propellers of different specifications in the high-altitude environment. Therefore, it is urgent to provide a simulation The device can be placed on the ground to simulate the high-altitude environment and simulate the propeller power of the aircraft. [0003] However, only a small number of analog dynamic measurement systems that have appeared so far have complex structures and high manufacturing costs, ...

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
IPC IPC(8): G01M9/08G01M9/06G01M9/04
CPCG01M9/08G01M9/04G01M9/062Y02T90/00
Inventor 郭玉超阮昌龙王月孙为全李德彬李庆海李富才王勋王文志于磊辉
Owner INST OF ENGINEERING THERMOPHYSICS - CHINESE ACAD OF SCI
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

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com