UAV Rotor Wind Charging for Extended Flight Range

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Solution Overview

Problem

Smaller unmanned aerial vehicles (UAVs) have limited range due to short-lived battery power, restricting their ability for prolonged flights and effective package delivery tasks.

Innovation Solution

A system and method that allows UAVs to recharge their batteries using wind-induced rotation while docked on a host vehicle, involving monitoring battery levels, determining optimal docking locations, and adjusting rotor configurations for efficient charging, enabling extended flight capabilities.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Duration of action of moving object

If smaller UAVs use rechargeable batteries to provide power for flying, then they can accomplish flight tasks, but the battery power is short lived and limited, restricting range and duration of flight

Engineering Contradiction:
Improveflight durationVSAvoidbattery power limitation
Core Design Contradiction:
Duration of action of moving objectVSUse of energy by moving object

Solution Approach 1:

The system performs preliminary action by having the UAV dock with a host vehicle before the battery is completely depleted, allowing the rotor to begin generating electricity in advance. The generator starts charging the battery while the UAV is still docked, ensuring sufficient charge is accumulated before takeoff, thus extending flight duration without waiting for complete battery exhaustion.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The generator acts as an intermediary device that converts mechanical energy from the rotating rotor into electrical energy to recharge the battery. This intermediary mechanism bridges the gap between the limited battery capacity and the extended flight duration requirement, allowing energy transfer from the host vehicle's motion (via rotor rotation) to the battery storage system.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Length of moving object

If the UAV docks on a host vehicle to recharge the battery using wind-induced rotation of the rotor, then the range and duration of flight are extended, but the system complexity increases due to docking mechanisms and rotor configuration control

Engineering Contradiction:
Improverange of flightVSAvoiddocking and control system
Core Design Contradiction:
Length of moving objectVSDevice complexity

Solution Approach 1:

The rotor serves multiple functions: it acts as both a propulsion element during flight and a generator during docking for recharging. This multi-functionality reduces the need for separate dedicated components, thereby managing system complexity while enabling extended range through energy replenishment during docking periods.

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

Solution Approach 2:

The system dynamically adjusts the rotor configuration (blade pitch angle) based on operational mode - optimized for propulsion during flight and optimized for energy generation during docking. This dynamic adaptation allows the same physical component to efficiently perform different functions, reducing the need for additional specialized components and managing overall system complexity.

Inventive Principle:
Principle #15Dynamics

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

Enables UAVs to extend their range and duration of flight by harnessing wind energy for battery recharging, thereby enhancing their operational efficiency and effectiveness in tasks like package delivery.

Implementation Method 1

charging the battery using wind-induced rotation of a rotor of the UAV

Methodology Applied
Scientific EffectWind power: Wind Power

Implementation Method 2

a generator configured to recharge the battery using wind-induced rotation of the rotor

Methodology Applied
Scientific EffectElectromagnetic induction: Electromagnetic Induction

Data Source

PatentUS10120376B2Renewable UAV energy via blade rotation
Publication Date: 2018.11.06 KYNDRYL INC
  • US10120376B2 patent drawing
  • US10120376B2 patent drawing
  • US10120376B2 patent drawing

AI summary

A computer-implemented method includes: monitoring, by a computer device, a charge level of a battery of an unmanned aerial vehicle (UAV); determining, by the computer device and based on the monitoring, the charge level is less than a threshold level; docking the UAV on a host vehicle; charging the battery using wind-induced rotation of a rotor of the UAV while the UAV is docked on the host vehicle; determining, by the computer device, the UAV is moving away from a destination while the UAV is docked on the host vehicle; and undocking the UAV from the host vehicle based on the determining the UAV is moving away from the destination.