UAV Landing Stand with Electromagnetic Capture and Docking

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Solution Overview

Problem

Current systems for unmanned aerial vehicle (UAV) landing and launch lack efficient and safe mechanisms for precise alignment, secure capture, and integrated refueling/recharging processes, leading to potential damage and operational inefficiencies.

Innovation Solution

The development of a stand system equipped with vertical lift shafts, inertial measurement units, and advanced sensors for navigation, along with a network of stands for coordinated UAV operations, including drone domes for secure landing and launch zones, and integrated charging and refueling systems.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a stand system with vertical lift shafts and capture mechanisms is used for UAV landing and launch, then precise alignment and secure capture are achieved, but device complexity increases

Engineering Contradiction:
Improvesecure captureVSAvoiddevice complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent replaces complex mechanical capture mechanisms with electromagnetic coupling systems. The stand uses electromagnetic fields to capture and hold the UAV, eliminating the need for intricate mechanical clamps, shafts, and physical locking mechanisms while achieving secure and reliable capture.

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

Solution Approach 2:

The patent introduces electromagnetic fields as an intermediary between the stand and UAV. This intermediary enables energy and force transfer without direct mechanical contact, simplifying the overall system while maintaining secure capture and alignment capabilities.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Measurement precision

If advanced sensors and inertial measurement units are integrated for precise alignment, then navigation precision is improved, but device complexity increases

Engineering Contradiction:
Improvealignment precisionVSAvoiddevice complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent integrates inertial measurement units and sensors that serve multiple functions: navigation, alignment, and positioning. This multi-functionality reduces the need for separate specialized systems, thereby improving measurement precision while limiting the increase in overall device complexity.

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

Solution Approach 2:

The UAV's onboard sensors and inertial measurement units enable the vehicle to autonomously determine its position, orientation, and alignment with the stand. This self-service capability eliminates the need for complex external alignment systems, improving precision without proportionally increasing complexity.

Inventive Principle:
Principle #25Self-service

3Productivity

If integrated refueling and recharging systems are implemented, then operational efficiency is improved, but device complexity increases

Engineering Contradiction:
Improveoperational efficiencyVSAvoiddevice complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The patent combines refueling and recharging operations into a single integrated docking process. The UAV simultaneously receives fuel and electrical power when docked with the stand, eliminating the need for separate refueling and recharging systems and procedures, thereby improving operational efficiency while managing complexity.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The electromagnetic coupling system serves as an intermediary that facilitates both fuel transfer and electrical power transfer during the docking operation. This unified intermediary mechanism enables integrated refueling and recharging through a single docking interface, improving productivity without requiring multiple separate systems.

Inventive Principle:
Principle #24Intermediary (Mediator)

Data Source

PatentUS12012221B2Methods and apparatus for unmanned aerial vehicle landing and launch
Publication Date: 2024.06.18 AIROGISTIC L L C
  • US12012221B2 patent drawing
  • US12012221B2 patent drawing
  • US12012221B2 patent drawing

AI summary

An unmanned aerial vehicle (UAV), a stand for launching, landing, testing, refueling and recharging a UAV, and methods for testing, landing and launching the UAV are disclosed. Further, embodiments may include transferring a payload onto or off of the UAV, and loading flight planning and diagnostic maintenance information to the UAV.