Toroidal support structures

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Solution Overview

Problem

Conventional support structures face challenges in fitting within complex geometries, such as between cylindrical and spherical objects, and suffer from thermal deformations due to temperature fluctuations, leading to misalignment and mechanical distortion in environments like spacecraft cryogenic tanks.

Innovation Solution

A toroidal support structure comprising a tubular ring and planar ring with isolating linear support components connected to a mounting base, providing thermal isolation and preventing mechanical distortion, while allowing for flexible installation and stress reduction through pivotable connections.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Volume of moving object

If conventional support structures are used in complex geometries between cylindrical and spherical objects, then the space utilization is poor, but the structural complexity and manufacturing difficulty increase

Engineering Contradiction:
Improvespace utilizationVSAvoidstructural complexity
Core Design Contradiction:
Volume of moving objectVSDevice complexity

Solution Approach 1:

The support structure employs a toroidal (doughnut-shaped) geometry that naturally conforms to the curved surfaces of cylindrical and spherical objects. This curved design allows the structure to fit efficiently in the annular space between a cryogenic tank and the spacecraft wall, maximizing space utilization while maintaining structural integrity through its inherent geometric strength.

Inventive Principle:
Principle #14Spheroidality (Curvature)

Solution Approach 2:

The toroidal support structure is divided into multiple modular segments or panels that can be independently manufactured and assembled. This segmentation allows for easier manufacturing of complex curved surfaces, simplifies assembly in the confined spacecraft environment, and enables the structure to adapt to varying geometric requirements while maintaining overall structural coherence.

Inventive Principle:
Principle #1Segmentation

2Strength

If rigid support structures are used to maintain stability, then the structural strength is high, but thermal deformations cause misalignment and mechanical distortion in temperature fluctuation environments

Engineering Contradiction:
Improvestructural strengthVSAvoiddimensional stability
Core Design Contradiction:
StrengthVSStability of the object's composition

Solution Approach 1:

The support structure incorporates materials and design features that allow controlled thermal expansion and contraction. By designing joints and connections that can accommodate dimensional changes within certain parameter ranges, the structure maintains its overall integrity and functionality despite temperature fluctuations, preventing misalignment and mechanical distortion.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent introduces intermediary elements such as flexible joints, expansion joints, or compliant mechanisms between rigid structural components. These intermediaries act as buffers that absorb thermal deformations, allowing the rigid parts to maintain their strength while the intermediaries accommodate the dimensional changes, thus preventing misalignment and mechanical distortion.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Stability of the object's composition

If the support structure is firmly fixed to prevent rotation, then the positional stability is improved, but stress concentrations increase under high acceleration conditions

Engineering Contradiction:
Improvepositional stabilityVSAvoidstress concentration
Core Design Contradiction:
Stability of the object's compositionVSStress or pressure

Solution Approach 1:

The support structure employs dynamic mounting mechanisms that allow controlled movement or adjustment during high acceleration events. Rather than being completely rigidly fixed, the structure can dynamically adapt its position or orientation within certain limits, distributing stresses more evenly across the mounting points and reducing stress concentrations while maintaining adequate positional stability.

Inventive Principle:
Principle #15Dynamics

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 toroidal design enhances stiffness and stability, enabling the support structure to withstand high accelerations and temperature fluctuations, providing a higher load-bearing capacity with reduced mass and stress concentrations, while maintaining orientation and preventing rotation relative to the mounting base.

Implementation Method 1

providing thermal isolation to the rings and preventing their mechanical distortion

Methodology Applied
Scientific EffectThermal isolation: Thermal Insulation

Implementation Method 2

Temperature fluctuations may cause different levels of thermal expansions and/or contractions on different components of support structures causing deformations and misalignment

Methodology Applied
Scientific EffectThermal expansion: Thermal Expansion

Data Source

PatentEP3808664B1Toroidal support structures
Publication Date: 2023.05.03 THE BOEING CO
  • EP3808664B1 patent drawingFigure 1A
  • EP3808664B1 patent drawingFigure 1B
  • EP3808664B1 patent drawingFigure 2A

AI summary

Provided are toroidal support structures and assemblies comprising these structures. A toroidal support structure comprises one or more side panels forming a tubular ring and one or more floor panels forming a planar ring. These rings define the toroidal shape of the structure. The structure also comprises multiple isolating linear support components connected to a top edge of the tubular ring. During installation of the structure, the isolating linear support components are attached to a mounting base for supporting the structure relative to the base, while providing thermal isolation to the rings and preventing their mechanical distortion. As such, a toroidal support structure can be attached to various types of mounting bases, such as a cryogenic tank of a spacecraft. Both rings provide supporting and mounting surfaces for equipment, cables, and pipes, while the toroidal opening allows external components to protrude through the support structure.