Circular Panel Assembly for Rapid In-Orbit Space Station Welding

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Solution Overview

Problem

Current methods for building space stations are time-consuming and costly due to the complexity of assembling them piece-by-piece in orbit, necessitating a more efficient and rapid construction approach.

Innovation Solution

A system comprising multiple modules, including panel dispensing units, welding assemblies, and a ring mobility unit, which align and weld panels to form a torus-shaped or cylindrical space station, utilizing durable materials and automated processes to expedite assembly.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If space stations are assembled piece-by-piece in orbit using traditional methods, then the space station can be built with required structural integrity, but the assembly process takes a great amount of time and money

Engineering Contradiction:
Improveassembly speedVSAvoidassembly time
Core Design Contradiction:
ProductivityVSLoss of time

Solution Approach 1:

The space station is divided into modular panels that can be pre-assembled and then rapidly connected using the circular assembly system. Multiple station-constructing modules work simultaneously on different segments of the space station, enabling parallel assembly operations that dramatically reduce total assembly time while maintaining structural integrity through standardized connection interfaces.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The assembly system transitions from static, sequential assembly to dynamic, circular assembly where multiple modules move continuously around the space station structure. The ring mobility unit enables the assembly system to dynamically reposition and access different sections of the space station simultaneously, transforming the assembly process from a linear sequence to a concurrent circular operation.

Inventive Principle:
Principle #15Dynamics

2Reliability

If traditional piece-by-piece assembly methods are used, then structural integrity can be maintained, but the complexity and cost of the assembly process increases

Engineering Contradiction:
Improvestructural integrityVSAvoidassembly system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

Each station-constructing module is designed as a universal, multi-functional unit that can perform multiple operations including panel positioning, alignment, and welding. The ring mobility unit serves multiple purposes by enabling both transport of modules around the space station and positioning of welding assemblies at different locations. This universality reduces the number of specialized components needed, simplifying the overall system while maintaining reliable assembly operations.

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

Solution Approach 2:

The welding assemblies are designed to automatically position and align themselves with the panels being assembled. The system incorporates self-aligning mechanisms that ensure proper positioning without requiring complex external guidance systems, and the automated welding process maintains consistent quality standards. This self-service capability reduces the need for complex control systems and manual intervention, thereby simplifying the assembly system while ensuring structural integrity.

Inventive Principle:
Principle #25Self-service

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 method significantly reduces the time and cost associated with building space stations by enabling rapid assembly of panels into a ring structure, allowing for quick completion of a habitable space station.

Implementation Method 1

welding assemblies, and a ring mobility unit, which align and weld panels to form a torus-shaped or cylindrical space station

Methodology Applied
Scientific EffectWelding: Welding

Data Source

PatentUS12145752B2Rapid sequential circular assembly system for space station
Publication Date: 2024.11.19 BLINCOW JOHN
  • US12145752B2 patent drawing
  • US12145752B2 patent drawing
  • US12145752B2 patent drawing

AI summary

A rapid sequential circular assembly system for a space station includes a plurality of station-constructing modules arranged in a circular manner that are connected to each other in radial profile so that a torus-shaped space station and/or cylindrical shaped space station can be built with a plurality of panels. Each station-constructing module includes a panel dispensing unit, a panel transporting cart, a first welding assembly, and a second welding assembly. The panel transporting cart is operatively coupled to a pair of rails of the panel dispensing unit, wherein the panel transporting cart travels between a storage compartment of the panel dispensing unit and the second welding assembly. The first welding assembly is connected along the pair of rails, and the second welding assembly is terminally connected across the pair of rails to seam weld each of the panels that are transported from the panel transporting cart.