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

Six-component ring type wind tunnel balance

A wind tunnel balance and six-component technology, applied in measuring devices, instruments, aerodynamic tests, etc., can solve problems such as asymmetric deformation of balance measurement components, affecting test force measurement accuracy, and asymmetric forward and reverse force measurement , to achieve the application value of large projects, improve the quality of wind tunnel tests, and achieve good symmetry of force and deformation

Pending Publication Date: 2020-08-11
INST OF HIGH SPEED AERODYNAMICS OF CHINA AERODYNAMICS RES & DEV CENT
View PDF0 Cites 10 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The traditional six-component ring wind tunnel balance is formed by punching holes on the basis of conventional balances. It adopts a multi-section series rod structure, and the balance structure is asymmetrical. When the size of the middle hole of the balance is large, the rigidity of the upper and lower ends of the balance has a large difference. , when the balance is under load, the deformation of the balance measuring element is asymmetrical, and the local stress is large, resulting in a large overall deformation of the balance, low strength, large interference load from other components, and there are certain problems such as positive and negative force asymmetry, which affect the test. Force measurement accuracy

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
  • Six-component ring type wind tunnel balance
  • Six-component ring type wind tunnel balance
  • Six-component ring type wind tunnel balance

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0036] In the description of the present invention, it should be noted that unless otherwise specified and limited, the terms "installation", "connection" and "connection" should be understood in a broad sense, for example, it can be a fixed connection or a detachable connection. Connected, or integrally connected; it can be mechanically connected or electrically connected; it can be directly connected or indirectly connected through an intermediary, and it can be the internal communication of two components. Those of ordinary skill in the art can understand the specific meanings of the above terms in the present invention based on specific situations.

[0037] The present invention will be further described below in conjunction with accompanying drawing:

[0038] Such as Figure 1-Figure 7 As shown, a six-component ring wind tunnel balance includes a balance resistance measurement section 3, one side of the balance resistance measurement section 3 is provided with a balance ...

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 discloses a six-component ring type wind tunnel balance. The balance comprises a balance resistance measuring section, one side of the balance resistance measuring section is provided with a balance cantilever connecting section used for connecting a force measuring model or part; a balance fixed connection section is arranged on the other side of the balance resistance measurement section, a balance front measurement section used for measuring force is arranged between the balance resistance measurement section and the balance cantilever connection section, and a balance rear measurement section used for measuring force is arranged between the balance resistance measurement section and the balance fixed connection section. According to the invention, the limitation of a traditional rod-type wind tunnel balance structure is broken through; a four-face symmetrical structure is adopted, the stress deformation symmetry is good, the anti-interference capacity is high, the bending moment bearing capacity and the temperature characteristic are high, deformation is smaller, the strength is higher, the measurement accuracy is higher under the same output condition, the wind tunnel test quality can be improved, and the engineering application value is high.

Description

technical field [0001] The invention relates to the technical field of wind tunnel test model resistance measurement, in particular to a six-component ring type wind tunnel balance. Background technique [0002] The wind tunnel balance (referred to as the balance) is the key measuring device in the wind tunnel force test, which is used to measure the magnitude, direction and action point of the aerodynamic load (force and moment) acting on the model. When involving jets, propellers, etc., which require central ventilation or installation of rotating shafts, due to the limitation of model space, the balance can only use a ring structure. The traditional six-component ring wind tunnel balance is formed by punching holes on the basis of conventional balances. It adopts a multi-section series rod structure. The balance structure is asymmetrical. When the size of the middle hole of the balance is large, the rigidity of the upper and lower ends of the balance has a large differenc...

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 Applications(China)
IPC IPC(8): G01M9/06
CPCG01M9/062
Inventor 潘华烨熊能林俊熊健郭秋亭田培洲谢斌范长海苗磊杨洪胜杜宁刘志勇
Owner INST OF HIGH SPEED AERODYNAMICS OF CHINA AERODYNAMICS RES & DEV CENT
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