UAV Payload Retention Mechanism for Midair Delivery Sway

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Solution Overview

Problem

Existing unmanned aerial vehicle systems that use a single linear member for payload delivery are prone to payload sway due to wind or unexpected loads, which can lead to the linear member severing or disconnecting from the payload during flight.

Innovation Solution

An unmanned aerial vehicle equipped with a winding machine, a fall prevention mechanism, and a connection detection unit that holds the payload even if it becomes disconnected from the linear member, preventing unintentional falling by immobilizing the payload against the vehicle body and using a control system to manage the delivery process.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If a single linear member is used to hold the delivery target during flight, then the device complexity is reduced, but the reliability of payload delivery deteriorates due to sway and potential severance

Engineering Contradiction:
Improvestructure complexityVSAvoidpayload delivery reliability
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

The payload support system is segmented into multiple independent linear members (first linear member and second linear member) instead of using a single linear member. This segmentation allows the payload to be supported by multiple attachment points, reducing the risk that failure of one member will cause payload loss, while distributing the mechanical loads more evenly during flight operations.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent implements a fall prevention mechanism that is activated beforehand to catch the payload if a linear member fails. The control device monitors the flight state and payload position continuously, and when abnormal sway or potential severance is detected, the fall prevention mechanism is preemptively activated to prevent payload loss, cushioning against the worst-case scenario before it occurs.

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

2Loss of time

If the aerial vehicle stays in midair for delivery, then the loss of time is reduced compared to landing, but the payload may sway due to wind or vehicle movement causing harmful effects

Engineering Contradiction:
Improvedelivery timeVSAvoidpayload sway
Core Design Contradiction:
Loss of timeVSObject-affected harmful factors

Solution Approach 1:

The control device implements a feedback control system that continuously monitors the payload position and flight state, and adjusts the aerial vehicle's position and the linear member lengths in real-time to compensate for sway. The system receives feedback about payload deviation from the intended delivery position and actively corrects it by adjusting rotor speeds or linear member lengths, maintaining stable payload delivery during midair operations.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The patent employs dynamic adjustment of the linear member lengths using winding machines that can rapidly pay out or retract the members. This dynamic capability allows the system to respond to changing flight conditions, wind gusts, or payload sway by adjusting the member lengths in real-time, dissipating sway energy and maintaining stable payload positioning during midair delivery operations.

Inventive Principle:
Principle #15Dynamics

Data Source

PatentEP3929081B1Unmanned aerial vehicle, aerial vehicle control system, and transport method
Publication Date: 2025.01.15 RAKUTEN GROUP INC
  • EP3929081B1 patent drawingFigure 1
  • EP3929081B1 patent drawingFigure 2
  • EP3929081B1 patent drawingFigure 3

AI summary

The present invention is intended to provide an unmanned aerial vehicle capable of preventing unintentional falling of a delivery target. An unmanned aerial vehicle 1 according to an aspect of the present invention includes: an aerial vehicle body 2 capable of flying; a winding machine 3 provided to the aerial vehicle body 2 and capable of winding and unwinding a linear member 31 an end of which is connectable to a delivery target T; and a fall prevention mechanism 4 provided to the aerial vehicle body 2 and capable of holding the delivery target T disconnected from the linear member.