Coordinated Drone Payload Lifting With Real-Time Thrust Adjustment

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Solution Overview

Problem

Current aerial vehicle systems face challenges in efficiently lifting and maneuvering payloads, particularly when payloads vary in size, as they require multiple aircraft, which are costly, risky, and not scalable due to the need for coordinated operation by skilled pilots or operators.

Innovation Solution

A modular UAV system where multiple drones communicate and coordinate with each other to adjust their characteristics, such as thrust and orientation, to manage payloads effectively, allowing for scalable and efficient lifting and maneuvering without the need for external pilots or operators.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Force

If multiple aircraft are used to lift a payload larger than a single aircraft's capability, then the lifting capability is improved, but the operational cost and complexity increase significantly

Engineering Contradiction:
Improvelifting capabilityVSAvoidcoordination complexity
Core Design Contradiction:
ForceVSDevice complexity

Solution Approach 1:

The payload is divided into multiple segments that can be independently lifted by individual aircraft. Each aircraft handles a portion of the total payload, eliminating the need for complex coordination of multiple aircraft around a single large payload. The segments are then transported to the destination and reassembled.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

A centralized control system acts as an intermediary that coordinates the operations of multiple aircraft. This control system manages thrust adjustments, positioning, and synchronization of all aircraft in the formation, reducing the coordination complexity that would otherwise be borne by multiple pilots or operators.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Ease of operation

If multiple aircraft with operators are used to maneuver a payload, then the maneuvering capability is improved, but the operational cost increases due to multiple operators

Engineering Contradiction:
Improvemaneuvering capabilityVSAvoidnumber of operators
Core Design Contradiction:
Ease of operationVSQuantity of substance

Solution Approach 1:

The aircraft are equipped with autonomous navigation and control systems that enable them to maneuver the payload without human operators on board or directly controlling each aircraft. The system automatically adjusts thrust, position, and orientation based on pre-programmed instructions or real-time sensor data, eliminating the need for multiple operators.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

Manual control systems operated by human pilots are replaced with automated flight control systems. These systems use sensors, processors, and actuators to automatically manage aircraft behavior, substituting mechanical human operation with an automated control architecture that can coordinate multiple aircraft more efficiently.

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

3Productivity

If aircraft operate in close proximity to lift a single payload, then the lifting efficiency is improved, but the safety risk increases due to coordinated operation requirements

Engineering Contradiction:
Improvelifting efficiencyVSAvoidsafety risk
Core Design Contradiction:
ProductivityVSReliability

Solution Approach 1:

The aircraft are equipped with sensors that continuously monitor the position, velocity, and orientation of each aircraft and the payload. This data is fed back to the control system in real-time, allowing for automatic adjustments to maintain safe separation distances and proper formation geometry, thereby reducing safety risks while maintaining lifting efficiency.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The control system incorporates safety margins and buffer zones in the coordination algorithms. Before potential conflict situations arise, the system pre-adjusts aircraft positions and velocities to maintain safe separation. Emergency protocols are pre-programmed to automatically activate if anomalies are detected, providing a cushion against safety risks.

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

4Quantity of substance

If a single aircraft is used to lift a payload, then the operational cost is reduced, but the maximum payload size is limited by the aircraft's lifting capability

Engineering Contradiction:
Improvepayload sizeVSAvoidaircraft selection flexibility
Core Design Contradiction:
Quantity of substanceVSAdaptability or versatility

Solution Approach 1:

Large payloads that exceed the capability of a single aircraft are divided into smaller segments that can each be handled by standard-capacity aircraft. This segmentation allows the use of more readily available, less expensive aircraft while still achieving the goal of transporting large overall payloads through coordinated multi-aircraft operations.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system is designed to accommodate various payload sizes and configurations using the same basic multi-aircraft coordination approach. By standardizing the coordination protocol and control architecture, the system can adapt to different payload requirements without requiring specialized aircraft or procedures, enhancing versatility.

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

Data Source

PatentUS20250021111A1Coordinated drone operation
Publication Date: 2025.01.16 UAVPATENT CORP
  • US20250021111A1 patent drawing
  • US20250021111A1 patent drawing
  • US20250021111A1 patent drawing

AI summary

A UAV system comprises a plurality of drones capable of communicating with each other to conduct a coordinated maneuver of a pay load coupled to the plurality of drones. A first drone may detect a change in a payload characteristic of the payload. The first drone may send or receive a communication, wherein the communication concerns an adjustment to be made to a drone characteristic of the first drone in response to the change in the payload characteristic. The first drone may adjust the drone characteristic in accordance with the communication.