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UAV Load Test JIG – Whiffletree

The UAV-Lab 500 Static Load Testing System is a comprehensive structural analysis platform designed to test the wings and structural components of UAVs (Unmanned Aerial Vehicles). Utilizing the Whiffletree method, the system distributes loads in a realistic and controlled manner, allowing engineers to verify structural integrity, aerodynamic behavior, and manufacturing quality under static loading conditions. It supports full-scale or model-size UAV parts and integrates sensors, load control, and data acquisition into one synchronized system.

Features

Whiffletree Load Distribution

Uses a multi-point loading mechanism to evenly distribute forces, mimicking aerodynamic pressures.
Adjustable fixtures for custom UAV wing shapes and sizes.

High-Precision Sensors

Strain gauges and LVDT displacement sensors measure deformation and stress.
Load cells (accuracy: ±0.1% FS) and inclinometers (±0.1° accuracy) for real-time data.

Modular Mechanical Frame

15-ton steel frame with CNC-machined components for durability.
Detachable clamping fixtures for flexible test setups.

Advanced DAQ & Software

24-bit ADC with 16-channel data acquisition.
Software analyzes deflection, resonant frequencies, and load limits.

Certification-Ready

Complies with aviation authority standards (e.g., EASA, FAA) for UAV structural testing.

Benefits

Ensures accurate simulation of real-world load distribution on UAV structures
Helps verify design strength, durability, and compliance with certification standards
Detects hidden structural weaknesses and manufacturing defects early
Facilitates material optimization and weight reduction for better UAV performance
Supports scientific research and engineering education on UAV structural mechanics
A modular, flexible system allows easy adaptation to different UAV configurations.

Software