Quasi-three-dimensional automatic measurement system for wind tunnels of atmospheric boundary layer

An atmospheric boundary layer and automatic measurement technology, which is used in measurement devices, aerodynamic tests, and machine/structural component testing. and other problems, to achieve the effect of assembling wind farm impact, low cost, and avoiding energy waste

Active Publication Date: 2012-09-26
HARBIN INST OF TECH
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0013] The purpose of the present invention is to solve the problem that the existing large-scale wind tunnel mobile control equipment has fewer types and complex structures, and most of the automatic equipment is imported from abroad, which is expensive and inconvenient for popularization and application, and most of the self-owned equipment is manually controlled, which cannot be realized. Continuous multi-point measurement and automatic movement of the speed measuring rod, and then provide a quasi-three-dimensional automatic measurement system for the atmospheric boundary layer wind tunnel

Method used

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  • Quasi-three-dimensional automatic measurement system for wind tunnels of atmospheric boundary layer
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  • Quasi-three-dimensional automatic measurement system for wind tunnels of atmospheric boundary layer

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specific Embodiment approach 1

[0022] Specific implementation mode one: combine Figure 1-Figure 6Describe this embodiment, the quasi three-dimensional automatic measurement system of a kind of atmospheric boundary layer wind tunnel of this embodiment includes forward and backward moving device and up and down moving device, and up and down moving device is arranged in the forward and backward moving device,

[0023] The forward and backward movement device comprises a front and rear movement support 1, a first front and rear movement mechanism 2, a second front and rear movement mechanism 3, a sliding mechanism 11, a second front and rear movement gear shaft 28 and two front and rear movement bearing blocks 29, the first front and rear movement mechanism 2 and The second forward and backward moving mechanism 3 is arranged side by side on the forward and backward moving support 1, and the first forward and backward moving mechanism 2 and the second forward and backward moving mechanism 3 all include a forwar...

specific Embodiment approach 2

[0027] Specific implementation mode two: combination image 3 Describe this embodiment, the quasi-three-dimensional automatic measurement system of this embodiment also includes a support frame length adjustment part 30, a measuring rod support mechanism length adjustment part 31 and a plurality of gear shaft length adjustment parts 32, and the support frame length adjustment part 30 is fixed on the The upper end of the forward and backward movement support 1 in the forward and backward movement device, the measuring rod support mechanism length adjustment part 31 is arranged on the up and down movement support 15, and the gear shaft length adjustment part 32 is arranged on the first front and rear movement gear shaft 5, the up and down movement gear shaft 21 and the first On the two forward and backward moving gear shafts 28, and the first forward and backward moving gear shaft 5, the up and down moving gear shaft 21 and the second forward and backward moving gear shaft 28 are...

specific Embodiment approach 3

[0029] Specific implementation mode three: combination figure 2 Describe this embodiment, the quasi three-dimensional automatic measurement system of this embodiment also includes the measuring rod double support structure 33, and the measuring rod double support structure 33 is fixed on the up and down moving support 15, and the measuring rod double support structure 33 comprises the measuring rod support mechanism The length adjusting part 31 and the measuring rod double supporting structure 33 are double supporting structures composed of a streamlined measuring supporting rod and a tensile stress pre-tightening mechanism. With such an arrangement, the stability of the system measurement can be ensured while reducing the resistance of the supporting structure of the measuring rod as much as possible. The other components and connections are the same as those in the first or second embodiment.

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Abstract

The invention provides a quasi-three-dimensional automatic measurement system for wind tunnels of an atmospheric boundary layer, relating to a quasi-three-dimensional automatic measurement system. The quasi-three-dimensional automatic measurement system is used for solving the problems that the continuous multipoint measurement and automatic motion of a velocity rod can not be realized because the existing large-sized wind tunnel mobile control equipment is relatively few in category and complicated in structure, automatic equipment is mostly imported from abroad, high in cost and inconvenient in popularization and application, and own equipment is mostly equipment of manual control. The quasi-three-dimensional automatic measurement system comprises a forward-backward moving device and an upward-downward moving device; the upward-downward moving device is arranged in the forward-backward moving device; a first forward-backward moving mechanism and a second forward-backward moving mechanism are arranged at the two sides of a forward-backward moving bracket in parallel; an upward-downward moving bracket is arranged in the forward-backward moving bracket; and a first upward-downward moving mechanism and a second upward-downward moving mechanism are arranged at the two sides of the upward-downward moving bracket in parallel. Support frame length adjustment members and measuring rod support mechanism length adjustment members are adjustable within a certain range of length and can carry out leveling to a certain degree. The quasi-three-dimensional automatic measurement system is applicable to the automatic measurement of the wind tunnels.

Description

technical field [0001] The invention relates to a quasi-three-dimensional automatic measurement system, in particular to a quasi-three-dimensional automatic measurement system for an atmospheric boundary layer wind tunnel. Background technique [0002] A wind tunnel is a pipeline-shaped experimental device that can artificially generate and control airflow to simulate the flow of gas around objects, measure the effect of airflow on objects and observe physical phenomena. It is the most commonly used and most effective for aerodynamic experiments. Tool of. With the development of industrial aerodynamics, low-speed wind tunnels (wind tunnels whose Mach number M is less than 0.4 in the experimental section of the wind tunnel) are becoming more and more widely used in transportation, housing construction, wind energy utilization, and environmental protection. application. In wind tunnel experiments, the model or object is often fixed in the wind tunnel, the gas flows through t...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M9/06
Inventor 李彪刘京涂世杰尹晓彤贺杰周峰
Owner HARBIN INST OF TECH
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