Thruster Battery Module for Suspended Load Motion Control

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing systems for controlling suspended loads, such as those lifted by helicopters or cranes, face challenges in managing unstable motion like yaw, pendular motion, and horizontal translation, which can lead to hazardous conditions and operational delays due to their reliance on carrier-based countermeasures that are inadequate and costly.

Innovation Solution

A suspended load control system (SLCS) that includes thrusters and a battery module, securely attached to the load or its holding structure, uses vector thrust forces to independently control the load's motion, including yaw and horizontal translation, allowing for precise positioning and obstacle avoidance.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If carrier-based countermeasures are used to control suspended load motion, then the load can be controlled, but the system becomes costly and inadequate

Engineering Contradiction:
Improveload control effectivenessVSAvoidsystem cost and complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The invention extracts the load control function from the carrier system and implements it independently on the load itself through the SLCS. The thrusters and battery module are mounted directly on the load, enabling autonomous control of yaw, pendular motion, and horizontal translation without relying on complex carrier-based countermeasures.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The SLCS acts as an intermediary system between the load and the carrier, providing independent motion control. The thrusters generate forces that directly affect the load's motion, while the battery module provides the necessary power, serving as a self-contained control system that mediates between the load and external environmental forces.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Productivity

If traditional hoist systems are used, then loads can be suspended, but unstable motion causes hazardous conditions and operational delays

Engineering Contradiction:
Improveoperational efficiencyVSAvoidunstable motion and hazards
Core Design Contradiction:
ProductivityVSObject-affected harmful factors

Solution Approach 1:

The SLCS applies preliminary anti-action by using thrusters to counteract unstable motion forces before they can cause hazardous conditions. The system continuously generates compensating forces to oppose yaw, pendular motion, and horizontal translation, preventing these harmful motions from developing into dangerous conditions that would delay operations.

Inventive Principle:
Principle #9Preliminary anti-action

Solution Approach 2:

The system employs feedback control where sensors detect the load's motion state and the control system adjusts thruster output accordingly. This closed-loop control continuously monitors and corrects unstable motion, maintaining load stability and preventing hazardous conditions while improving operational efficiency.

Inventive Principle:
Principle #23Feedback

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

The SLCS enhances safety and operational efficiency by dynamically controlling the load's position and orientation independently of the carrier, reducing risks and costs associated with traditional methods.

Implementation Method 1

uses vector thrust forces to independently control the load's motion, including yaw and horizontal translation

Methodology Applied
Scientific EffectThrust force: Rocket

Implementation Method 2

A suspended load control system (SLCS) that includes thrusters and a battery module

Methodology Applied
Scientific EffectBattery energy storage: Battery (electricity)

Data Source

PatentUS20250011139A1Thruster and battery module for suspended load control apparatuses, systems, and methods
Publication Date: 2025.01.09 VITA INCLINATA IP HOLDINGS LLC
  • US20250011139A1 patent drawing
  • US20250011139A1 patent drawing
  • US20250011139A1 patent drawing

AI summary

Load control apparatuses, systems and methods to control a location, orientation, or rotation of a suspended load by imparting thrust vectors to the suspended load or to a structure that holds the load. The load control apparatuses, systems and method may comprise a thruster and battery module, wherein the thruster and battery module comprises a thruster and a battery pack.