Service Scope
Electrical control, motor, and BMS for low-altitude aircraft such as UAVs and eVTOLs
Testing Standards
RTCA DO-160G
GB/T 38058-2019
GB/T 42590-2023
Testing Items
General tests (e.g., appearance, dimensions, strength, sealing, resistance, etc.), functional performance tests (e.g., back EMF, short-circuit current, peak performance and efficiency within the voltage range, speed-torque characteristics, temperature rise test, etc.), environmental reliability tests (temperature and humidity tests, vibration tests, protection tests, salt spray tests, mold tests, etc.), safety tests (e.g., insulation and withstand voltage tests, safety grounding, protection functions, discharge time, etc.)
Relevant Qualifications
CNAS accreditation
Testing Cycle
Testing duration is determined based on specific test items.
Service Background
With the development of the national economy, the application prospects and commercial value of low-altitude aircraft are becoming increasingly prominent. Currently, the airframes, power and energy systems, and avionics systems of low-altitude aircraft are developing towards higher structural strength and lighter weight, higher power density in power systems, and greater intelligence in avionics systems. This also places higher demands on the rationality of overall aircraft design and material selection, as well as the durability and reliability of components. Therefore, to ensure the successful commercialization of low-altitude aircraft, it is necessary to conduct a series of reliability tests on their electronic control and electric drive systems. This is to verify their safety, meet airworthiness certification requirements, assess their technical reliability and system stability, ensure stable operation in complex environments, support commercial operation and economic viability, establish public trust and industry ecosystem, and verify autonomous flight and emergency response capabilities.
Our Advantages
We can provide one-stop inspection and testing services for electric drive and electronic control assemblies for low-altitude aircraft.
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