In December 2024, DUT partnered with a major airline to measure fuselage strain and deformation during a complete flight cycle. Using the RU-846 Rugged Data Recorder, the test captured real-world stress data at 32 critical points to validate design safety and structural integrity.

Discover how a wireless dynamic strain test system enabled accurate data collection during extreme rocket launch conditions in 2024.

In May 2024, engineers conducted landing and water impact tests on a new-generation manned spaceship to capture detailed strain and vibration data for mission safety.

Multi-point engine vibration test captures triaxial acceleration data to support structural optimization and fault detection using DE-944.

Pipeline pressurization test captures multi-directional strain data to validate design and safety using RE-Series DAQ.

High-altitude drop test validates spacecraft recovery system with RE-Series data acquisition.

In August 2024, the 601 engine test bed was upgraded with DE-918 for precise multi-parameter monitoring and reliable engine verification.

In July 2024, a modal test of an engine rotor was conducted using the DE-924U system. Fourteen measurement points captured vibration responses to identify natural frequencies, damping ratios, and mode shapes, validating rotor design and mitigating resonance and fatigue risks.

In June 2024, a modal test of a rudder actuator surface was conducted using the DE-928U system. Multi-input excitation and high-speed synchronous acquisition captured natural frequencies, damping ratios, and mode shapes, validating structural models and mitigating resonance risks for flight safety.

In June 2024, the Aero Engine Turbine Research Institute conducted pulsation testing on an aircraft engine using the DE-928U system. Multi-dimensional vibration, pressure, and speed data validated engine reliability, identified excitation sources, and ensured compliance with military performance standards.

In June 2024, an engine research institute performed ignition tests on a specific engine model to analyze its dynamic behavior under startup conditions. Using the customized DE-944 Dynamic Signal Test and Analysis System, the project measured pulsating pressure, vibration acceleration, and rotational speed, delivering critical insights for engine design optimization and operational reliability.

How an aviation institute achieved precise, real-time multi-parameter testing and monitoring for Il-76 aircraft engines using Dynatronic’s advanced acquisition system.

How engineers validated the new manned spaceship’s recovery capsule with advanced sensors and rugged data acquisition systems during landing and water impact tests.

A military research institute adopted the DEWEsoft DE-928U system to accurately simulate and analyze the extreme landing impacts experienced by airdropped supplies.

In March 2024, a research institute conducted vibration damping tests for precision equipment using RE-846U, demonstrating significant attenuation, resonance suppression, and engineering applicability for high-precision device transport.

In March 2024, an airline conducted engine blade modal testing with DE-924U, analyzing natural frequencies, mode shapes, and resonance risks. Results support fatigue life prediction, predictive maintenance, and next-generation turbine blade design validation.

Flight load testing of the AG600 aircraft evaluated structural stability under water-takeoff, landing, and in-flight maneuvers. Data from 18 SE-98 systems and over 2,000 strain gauges validated design models and ensured compliance with safety standards.

Rocket sled track testing evaluated modal dynamics, impact shocks, and thermal-strain behavior. Data from RE-846U and RU-846 systems established design baselines for safety, performance, and next-generation material improvements.

The SE-98 system supports 16,000-channel full-scale structural testing at CASI, providing precise strain, displacement, load, and thermal measurements for both static and fatigue evaluations of aircraft airframes.

Controlled drop tests were performed to evaluate the shock absorption performance of aircraft landing gear airbags using a multi-channel dynamic measurement system.