Unmanned Aircraft Hoisting Mechanism for Preflight Package Anchoring

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing unmanned aircraft systems face challenges in easily anchoring packages to linear members during delivery, which affects delivery efficiency.

Innovation Solution

The system includes a hoisting mechanism with a winch to feed out and hoist a flexible linear member, a drop-preventing mechanism to secure the package, and a control device that manages the flight and hoisting operations to ensure easy anchoring and stable delivery.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the aircraft lands to deliver cargo, then the delivery is reliable, but the delivery time increases and requires a flat location with sufficient area

Engineering Contradiction:
Improvedelivery reliabilityVSAvoiddelivery time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The package is anchored to the linear member before the aircraft takes off, so that when the aircraft ascends, the package is automatically lifted along with the linear member without requiring the aircraft to land for delivery

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

A linear member (rope/cable) acts as an intermediary between the aircraft and the package, allowing the package to be transported aerially without the aircraft needing to land or release the package manually

Inventive Principle:
Principle #24Intermediary (Mediator)

2Loss of time

If the aircraft uses a hoisting mechanism to deliver cargo aerially, then the delivery time decreases, but the package anchoring becomes difficult

Engineering Contradiction:
Improvedelivery timeVSAvoidpackage anchoring ease
Core Design Contradiction:
Loss of timeVSEase of operation

Solution Approach 1:

The package is anchored to the linear member before the aircraft takes off, simplifying the anchoring operation that would otherwise be difficult to perform while the aircraft is in flight

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

Instead of attempting to anchor the package to the moving aircraft (difficult), the system inverts the approach by anchoring the package to a stationary linear member that will be lifted by the aircraft's hoisting mechanism

Inventive Principle:
Principle #13The other way round (Inversion)

3Ease of operation

If the linear member is fed out while the aircraft is on the ground, then the package can be anchored easily, but the aircraft cannot take off

Engineering Contradiction:
Improvepackage anchoring easeVSAvoiddelivery efficiency
Core Design Contradiction:
Ease of operationVSProductivity

Solution Approach 1:

The linear member is fed out and the package is anchored before the aircraft takes off, ensuring easy anchoring while maintaining delivery efficiency by avoiding ground-based delivery constraints

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system dynamically manages the linear member length by controlling the hoisting mechanism to feed out the member just enough for anchoring, then retracts it to enable aircraft takeoff and flight

Inventive Principle:
Principle #15Dynamics

4Stability of the object's composition

If the package is anchored close to the aircraft, then the anchoring is stable, but the package cannot be delivered to distant locations

Engineering Contradiction:
Improveanchoring stabilityVSAvoiddelivery distance
Core Design Contradiction:
Stability of the object's compositionVSLength of moving object

Solution Approach 1:

The linear member has different functional zones: a first length portion that maintains stable anchoring close to the aircraft, and a second longer portion that extends to reach distant package locations, with each portion serving its specific function

Inventive Principle:
Principle #3Local quality

Data Source

PatentEP3885259B1Unmanned aerial vehicle system, control device and control method
Publication Date: 2025.09.10 RAKUTEN GROUP INC
  • EP3885259B1 patent drawingFigure 1
  • EP3885259B1 patent drawingFigure 2
  • EP3885259B1 patent drawingFigure 3A

AI summary

The present invention has an object of providing an unmanned aircraft system, control device and control method which can more easily anchor a package to a linear member. An unmanned aircraft system (1) of an embodiment of the present invention includes: an unmanned aircraft (2) including a hoisting mechanism capable of feeding out and hoisting a linear member (31); a flight control unit (61) which causes the unmanned aircraft (2) to take off in a state in which a package (T) anchored to the linear member (31) is arranged on a ground surface; and a hoisting control unit (62) which causes the linear member (31) to be hoisted by the hoisting mechanism (3), after the unmanned aircraft (2) has taken off, in a case of a hoisting condition indicating a state enabling hoisting of the linear member (31) being satisfied.