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6S8P Battery Pack Drone BMS Engineering Case
UAV BMS Real Cases
Real Engineering Case Study

6S8P Battery Pack Drone BMS Engineering Case

A detailed analysis of custom BMS integration for a French industrial UAV developer, focusing on resolution strategies for high-current inductive transient suppression.

Phase 01 / Inquiry & Specifications

Background & Initial Project Assessment

In October 2025, AYAATECH received a formal inquiry from a French customer requiring a specialized BMS for their heavy-payload drone. We requested the completion of a detailed project specification form. To ensure system reliability, we recommended a joint debugging phase with their flight control axis, which the customer initially declined as they believed it was unnecessary at the time.

Conclusion: The pre-project engineering assessment confirmed the project was feasible for manufacturing. We provided the final quotation and delivery timeline.
Customer Inquiry Log / France Project Entry
France Customer Inquiry
France Customer Inquiry
Phase 02 / Sourcing Restrictions

Specialized Component & BOM Audits

The customer mandated the use of non-Chinese-manufactured semiconductors and IC components. Furthermore, the design was required to utilize components with high local availability in France to ensure long-term maintenance ease.

Component Specification Record
Component Specs Agreement
Phase 03 / Engineering Design

Technical Support & Schematic Verification

After several months of engineering development, AYAATECH provided full drawing sets and laboratory test reports.

Conclusion: The customer reviewed and accepted the technical drawings and initial validation results.
Technical Engineering Approval Report
Technical Support Record
Phase 04 / Field Testing Incident

Prototype Test Results & Flight Incident

On April 9, 2025, prototype samples were delivered to the customer for assembly testing. Following four months of integration, the customer reported that the drone suffered a mid-flight incident and crashed.

Incident Action: An immediate forensic investigation was launched to determine if the failure was electrical, mechanical, or software-based.
Emergency Flight Incident Notification
Incident Report
Phase 05 / Root Cause Analysis

Forensic Analysis & Circuit Redesign

Post-incident analysis revealed that the drone's specific application and flying axle power requirements created inductive transients that were not fully disclosed during the initial inquiry. The original BMS lacked a hardware pre-discharge circuit to handle these specific back-EMF surges.

Conclusion: Re-design the BMS architecture to include a robust, industrial-grade **Pre-Discharge Protection Circuit** to safeguard against high-throttle transients.
Failure Analysis & Corrective Action Plan
Future Analysis Record
Phase 06 / Ongoing Compliance

Current Testing & Final Certification

We are currently collaborating closely with the customer to conduct rigorous laboratory testing, ensuring full compliance with IEC 62133 and UN38.3 international safety standards.