Unlock instant, AI-driven research and patent intelligence for your innovation.

A low-speed wind tunnel model test support device based on internal balance

A model test and support device technology, which is applied in the field of wind tunnel test, can solve the problems that the support rod cannot be applied to the internal balance, cannot meet the requirements of the internal balance test, and cannot be made hollow, and achieves simple appearance, convenient installation, The effect of convenient processing

Active Publication Date: 2018-03-02
LOW SPEED AERODYNAMIC INST OF CHINESE AERODYNAMIC RES & DEV CENT
View PDF8 Cites 2 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the main part of the existing single-point (or two-point) support device - the support rod is designed and manufactured for the external balance, which cannot meet the test requirements of the internal balance, because the interfaces of the two are completely different
The support rod based on the external balance and the hollow design connecting plate inside the model are fixed with the main cylindrical pin, so the head is designed as a square (see figure 1 , figure 2 ); and the support rod based on the internal balance is connected with the balance installed inside the model. Due to the limitation of the volume, strength and rigidity, the balance cannot be made hollow, so the original support rod cannot be applied to the internal model. on the balance

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 low-speed wind tunnel model test support device based on internal balance
  • A low-speed wind tunnel model test support device based on internal balance
  • A low-speed wind tunnel model test support device based on internal balance

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0026] Such as figure 1 , figure 2 As shown, this is a commonly used support pole at present, but the pole is designed for the support of an external balance, so the support head of the support pole adopts a square structure, but this structure cannot be used for an internal balance. for support.

[0027] Such as image 3 Shown is the support strut that the present invention designs, and what upper end adopted is U-shaped structure, and lower end is the same with existing structure. And cylindrical pin holes are set on the two vertical sides of the U-shaped structure for fixed connection.

[0028] Such as Figure 4 As shown, it is the transitional connector designed by the present invention, which is one of the key points of the present invention. This design is adopted to match the U-shaped structure. The transitional connector adopts a cylindrical structure, one end face is open, and the other end face is designed as a flange Structure; cylindrical pin holes are respe...

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 support device for a low-speed wind tunnel model test based on an internal balance, which includes a support rod, and the connecting head of the support rod is a U-shaped structure with an upward opening, and two vertical sides of the U-shaped structure Cylindrical pin holes are respectively provided, and a transition piece is provided in the U-shaped structure, and the transition piece is a cylindrical structure with an opening at one end and a flange structure at the other end, and a cylindrical pin hole is provided on the side of the transition piece , the cylindrical pin passes through the U-shaped structure and the cylindrical hole on the transition piece in turn to fix the transition piece in the U-shaped structure. Adopting the structure of the present invention can satisfy both the use of the internal balance and the use of the external balance. In the wind tunnel test, a set of supporting devices can meet the test requirements of different needs, and there is no need to replace the support due to use during the test. device.

Description

technical field [0001] The invention relates to the field of wind tunnel tests, in particular to a support device for low-speed wind tunnel model tests based on internal balances. Background technique [0002] The 4m×3m wind tunnel is used as the main supporting device for conventional force testing of transport aircraft. It is a single-point (or two-point) supporting device designed based on a tower-type six-component mechanical strain balance. However, according to the needs of the expansion of new aircraft wind tunnel test tasks, the internal balance technology is being developed to form a conventional force measurement test capability that complements the internal and external balances. However, the main part of the existing single-point (or two-point) support device - the support rod is designed and manufactured for the external balance, which cannot meet the test requirements of the internal balance, because the interfaces of the two are completely different. The supp...

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): G01M9/04
Inventor 倪章松李东周晓飞孙传宝刘江涛付华张鹏李圆刘晓林李涵曹尤生万琪明
Owner LOW SPEED AERODYNAMIC INST OF CHINESE AERODYNAMIC RES & DEV CENT