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E-mail
gaoshengkeji@163.com
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Phone
18128028677
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Address
101, Building 2, No. 6 Songbailang Xinyuan 1st Road, Dalang Town, Dongguan City, Guangdong Province
Dongguan Gaosheng Electronic Precision Technology Co., Ltd
gaoshengkeji@163.com
18128028677
101, Building 2, No. 6 Songbailang Xinyuan 1st Road, Dalang Town, Dongguan City, Guangdong Province
Mobile wind field simulation deviceBreaking through the limitations of traditional wind tunnel equipment fixed structures, adopting a movable design, equipped with professional locking mechanisms and angle adjustment devices, the equipment position and air outlet angle can be quickly adjusted according to experimental needs. The system is equipped with multiple standard wind farm modes and supports user-defined wind farm parameters. Complex wind farm conditions can be quickly set through an intuitive upper computer software interface or CSV data table. Widely used in aerospace, fluid mechanics, aerodynamics and other fields, it is an ideal experimental platform for conducting wind field related research.
Main technical parameters:
technical category |
parameter item |
Detailed Specifications |
fan performance |
wind speed range |
3-30m/s (adjustable) |
control system |
Control method |
Overall control of upper computer software and CSV table single fan control |
communication protocol |
EtherCAT Gigabit Ethernet (latency<1ms) |
|
power configuration |
Power supply specifications |
48V DC power supply |
protection function |
Triple protection against overvoltage, overcurrent, and overheating |
|
mechanical structure |
frame material |
aviation aluminum profile |
Mobile Design |
Heavy duty universal wheel |
|
Tilt angle adjustment |
Adjustable from 0 ° to 90 ° |
|
environmental adaptability |
Operating Temperature |
-10°C-50°C |


This device is suitable for wind resistance performance testing of civil light and small rotary wing unmanned aerial vehicles (with takeoff weight between 0.25 kg and 150 kg). It can simulate dynamic fluid wind fields under different wind speed states and wind speed arrays to study the flight status of the aircraft under different complex wind speed and turbulence conditions.
Mobile wind field simulation deviceTechnical aspects:
1. Breakthrough innovative design (compared to traditional wind tunnels):
The core innovation lies in the movable design, which breaks through the limitations of the fixed structure of traditional wind tunnel equipment. This makes wind field simulation no longer limited to specific laboratory environments, greatly enhancing the flexibility and applicability of equipment.
2. High flexibility and convenience:
Equipped with professional locking mechanisms and angle adjustment devices, it can quickly adjust the equipment position and air outlet angle to meet the requirements of different experimental locations and environments. This greatly improves testing efficiency and the ability to adapt to complex experimental requirements.
3. Intelligent wind farm generation capability:
The system is equipped with multiple standard wind farm modes to simplify the basic testing process.
Support user-defined wind field parameters, with high customization capabilities, capable of generating complex wind field conditions that meet specific research needs (such as gusts, turbulence, variable wind direction, wind speed, etc.).
4. Efficient and convenient operating system:
Wind field setting and control can be completed through an intuitive upper computer software interface or CSV data table, greatly simplifying the configuration process of complex wind fields and improving the convenience and efficiency of experiments.
5. Widely applicable:
Its technical design makes it widely used in core research fields such as aerospace, fluid mechanics, aerodynamics, etc., which require high wind field environments, making it an ideal experimental platform.
Specially solved the problem of wind resistance performance testing in the drone industry, providing key technical support for its development.
Meet the standards:
GB 42590-2023 "Safety Requirements for Civil Unmanned Aerial Vehicle Systems";
GB/T38930-2020 "Wind resistance requirements and test methods for civil light and small unmanned aerial vehicle systems";
GB/T 38058-2019 "Test Methods for Civil Multi rotor Unmanned Aerial Vehicle Systems".