Drone Landing Guide Structure for Precise Wireless Charging

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Solution Overview

Problem

Conventional drone stations face inefficiencies in charging due to misalignment of the drone's center of resonance with the charging station, leading to reduced charging efficiency and increased charging time, and are prone to external environmental factors like wind and vibration causing the drone to crash or become dislodged.

Innovation Solution

The drone station incorporates a landing guidance instrument with an inclined surface and a guide member to align and secure the drone over a wireless charging instrument, featuring a power transmission coil and a guide member to ensure optimal charging alignment and stability, along with a protective cover for safe landing and takeoff.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If the drone is landed at the drone station using only GPS information, then the landing process is simple, but the center of resonance between the drone station and the drone is not accurately aligned, reducing charging efficiency and increasing charging time

Engineering Contradiction:
Improvelanding process simplicityVSAvoidalignment precision
Core Design Contradiction:
Ease of operationVSManufacturing precision

Solution Approach 1:

The patent introduces an inclined surface as an intermediary mechanical structure between the landing platform and the charging position. This inclined surface acts as a mediator that automatically guides the drone from its GPS-guided landing position to the precise charging position, resolving the contradiction between simple GPS-based landing and precise alignment requirements.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The patent replaces complex active mechanical adjustment systems with a passive inclined surface structure. Instead of using motors, sensors, or active control mechanisms to align the drone, the design uses a fixed inclined surface that passively guides the drone through gravitational force and geometric constraint, simplifying the system while achieving precise alignment.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

2Duration of action of moving object

If the drone is charged at the drone station, then the drone can be recharged, but the drone is out of the charging position or crashes at the drone station due to external environmental factors such as wind and vibration

Engineering Contradiction:
Improvecharging capabilityVSAvoidcharging position stability
Core Design Contradiction:
Duration of action of moving objectVSReliability

Solution Approach 1:

The patent incorporates a guide member positioned beforehand at the charging location to provide pre-positioning and stabilization. This guide member acts as a cushioning mechanism that prevents the drone from deviating from the charging position due to external disturbances like wind and vibration, ensuring reliable charging.

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

Solution Approach 2:

The guide member structure creates a confined spatial envelope that flexibly accommodates the drone while maintaining positional stability. The geometric constraints formed by the guide member provide a stable charging environment that resists external environmental factors.

Inventive Principle:
Principle #30Flexible shells and thin films

3Manufacturing precision

If an inclined surface is added to move the drone to the charging position, then alignment accuracy is improved, but the device complexity increases

Engineering Contradiction:
Improvecharging position alignmentVSAvoidstructure complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The patent divides the landing and charging functions into distinct spatial zones: a landing platform area and a charging position area connected by an inclined surface. This segmentation allows each component to perform its specific function independently, achieving precise alignment without requiring complex integrated systems.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The inclined surface introduces a geometric curvature element that simplifies the transition from landing to charging position. By using a simple inclined plane rather than complex mechanical adjustments, the patent achieves precise alignment through geometric design, reducing overall system complexity.

Inventive Principle:
Principle #14Spheroidality (Curvature)

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

This solution ensures accurate alignment and efficient charging, minimizing charging time and preventing drone separation or crashes due to external factors, thereby maximizing drone operating time and charging efficiency.

Implementation Method 1

a guide member spaced apart from the power transmission coil, and for generating an electromagnetic force to fix the drone positioned on the top of the wireless charging instrument

Methodology Applied
Scientific EffectElectromagnetic force: Lorentz Force

Implementation Method 2

The wireless charging instrument may be formed in a loop shape, and may include: a power transmission coil for wirelessly transmitting a power to the drone positioned on the top

Methodology Applied
Scientific EffectElectromagnetic induction: Electromagnetic Induction

Implementation Method 3

The landing guidance instrument may further include: a vibration member for generating a vibration on a bottom of the inclined surface

Methodology Applied
Scientific EffectVibration: Vibration

Data Source

PatentUS11999477B2Drone station
Publication Date: 2024.06.04 AMOSENSE CO LTD
  • US11999477B2 patent drawing
  • US11999477B2 patent drawing
  • US11999477B2 patent drawing

AI summary

Disclosed is a drone station which allows the center of resonance of a drone to be always accurately aligned regardless of the initial landing position of the drone. The disclosed drone station includes a landing guidance instrument and a wireless charging instrument which is formed on the landing guidance instrument and wirelessly transmits the power to a drone positioned thereon, the landing guidance instrument having an inclined surface which moves the landed drone onto the top of the wireless charging instrument.