UAV Battery Attachment Detection to Prevent Unsafe Takeoff

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Solution Overview

Problem

Unmanned aerial vehicles (UAVs) often experience battery detachment during flight, leading to potential explosions and making it difficult for manufacturers to analyze and locate the cause of accidents.

Innovation Solution

A battery monitoring method where the battery is communicatively connected to the flight control system, detecting the status of attachment mechanisms before takeoff and sending signals to instruct the flight control system to prevent takeoff if any mechanism is not in place, ensuring secure mounting and preventing accidents.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If the battery is detachably mounted using attachment mechanisms, then the ease of operation is improved, but the reliability deteriorates due to potential battery detachment during flight

Engineering Contradiction:
Improvebattery installation and removalVSAvoidbattery attachment stability
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The system performs preliminary detection of attachment mechanism status before takeoff and continuously monitors during flight. The flight control system checks whether all attachment mechanisms are properly engaged before allowing the UAV to take off, and can trigger emergency return or landing if detachment is detected during flight, preventing catastrophic failures.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The detection module provides real-time feedback on the status of attachment mechanisms to the flight control system. This feedback loop enables the system to monitor whether batteries are securely attached and to take appropriate corrective actions (such as preventing takeoff or initiating emergency procedures) if attachment status changes during operation.

Inventive Principle:
Principle #23Feedback

2Reliability

If real-time monitoring of attachment mechanisms is implemented, then the reliability is improved, but the device complexity increases

Engineering Contradiction:
Improvebattery attachment monitoringVSAvoidmonitoring system structure
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The detection module is integrated into the existing battery and flight control system architecture, serving multiple functions: pre-takeoff attachment verification, in-flight monitoring, and communication with the flight control system. This multi-functionality reduces the need for separate dedicated monitoring components, thereby limiting the increase in device complexity.

Inventive Principle:
Principle #6Universality (Multi-functionality)

3Reliability

If the flight control system prevents takeoff when attachment mechanisms are not in place, then the safety is improved, but the productivity decreases due to delayed flight operations

Engineering Contradiction:
Improveflight safetyVSAvoidtakeoff preparation time
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The system performs attachment status detection as a preliminary check before takeoff is authorized. By automatically verifying attachment status beforehand, the system prevents unsafe takeoffs without requiring manual inspection, thereby minimizing additional preparation time while ensuring safety.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS20240004405A1Battery monitoring method, battery and unmanned aerial vehicle
Publication Date: 2024.01.04 AUTEL ROBOTICS CO LTD
  • US20240004405A1 patent drawing
  • US20240004405A1 patent drawing
  • US20240004405A1 patent drawing

AI summary

A battery is detachably mounted on an unmanned aerial vehicle by using at least one attachment mechanism. The battery monitoring method includes: detecting, by the battery, before the unmanned aerial vehicle takes off, whether the at least one attachment mechanism is in place; and sending, by the battery, a first signal to the flight control system in response to detecting that the at least one attachment mechanism is in place, wherein the first signal is configured to instruct the flight control system to initiate takeoff of the unmanned aerial vehicle; or sending, by the battery, a second signal to the flight control system in response to detecting that at least one of the at least one attachment mechanism is not in place, wherein the second signal is configured to instruct the flight control system to prevent takeoff of the unmanned aerial vehicle.