Self-healing Shield for Spacecraft Using Dilatant Fluid and Spheroids

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Solution Overview

Problem

Current shielding technologies for spacecraft are ineffective against high-velocity particles (HVPs) as they fail to provide self-healing capabilities, are not replaceable, and are too heavy for launch into space.

Innovation Solution

A self-healing shield panel composed of an exterior and interior layer with a cavity containing a dilatant fluid and spheroids, where the spheroids move to plug puncture holes caused by HVP impacts, utilizing synthetic fibers and polyethylene glycol or polypropylene glycol as the dilatant fluid, and connected by synthetic fibers or mesh members for assembly.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If traditional shielding materials are used to protect spacecraft from HVPs, then protection capability is provided, but the shield lacks self-healing capability and becomes permanently damaged after penetration

Engineering Contradiction:
Improveself-healing capabilityVSAvoidshield structure complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The shield enables self-healing by incorporating spheroids that automatically migrate to puncture sites and dilatant fluid that autonomously solidifies upon impact, allowing the shield to repair itself without external intervention or complex control systems

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The shield utilizes the parameter change of the dilatant fluid, which transitions from liquid to solid state upon impact, enabling the fluid to automatically plug puncture holes and restore shield integrity without additional mechanical components

Inventive Principle:
Principle #35Parameter changes

2Reliability

If heavy shielding materials are used to ensure adequate protection from HVPs, then protection capability is improved, but the weight increases making launch into space difficult

Engineering Contradiction:
Improveprotection capabilityVSAvoidshield weight
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The shield combines lightweight synthetic fiber layers with a cavity containing spheroids and dilatant fluid, creating a composite structure that provides effective HVP protection while maintaining low weight for space launch

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The shield uses hydraulic principles by incorporating dilatant fluid that responds to impact pressure, allowing the fluid to automatically migrate and plug puncture holes without requiring heavy mechanical actuators or pressurized systems

Inventive Principle:
Principle #29Pneumatics and hydraulics

3Duration of action of stationary object

If the shield is designed to withstand multiple HVP impacts, then durability is improved, but the complexity of the shielding structure increases

Engineering Contradiction:
Improveshield durabilityVSAvoidshielding structure complexity
Core Design Contradiction:
Duration of action of stationary objectVSDevice complexity

Solution Approach 1:

The shield is pre-configured with spheroids positioned within the cavity and dilatant fluid ready to respond, enabling immediate self-healing action upon impact without requiring complex sensing or control systems to initiate the repair process

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The shield extracts the healing function from complex mechanical systems and implements it through simple passive elements (spheroids and dilatant fluid) that automatically respond to damage, reducing overall structural complexity while maintaining durability

Inventive Principle:
Principle #2Taking out (Extraction)

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 shield effectively disperses and absorbs kinetic energy from HVPs, allowing the shield to self-heal and maintain protection, with the ability to withstand multiple impacts and be easily replaced, while being lightweight enough for space launch.

Implementation Method 1

a dilatant fluid and a plurality of spheroids arranged in the dilatant fluid to absorb kinetic energy from an HVP

Methodology Applied
Scientific EffectDilatant: Dilatant

Implementation Method 2

the motions of the spheroids are dampened by the shear thickening of the dilatant fluid

Methodology Applied
Scientific EffectShear thickening: Shear Thickening

Implementation Method 3

the plurality of spheroids is able to close or 'plug' the puncture hole such that the shield 'self-heals' when punctured by HVP impact

Methodology Applied
Scientific EffectKinetic energy absorption: Impact Force

Data Source

PatentUS11623769B2Self-healing shield configured to protect an environment from high velocity particles
Publication Date: 2023.04.11 OLAFSRUD ANDREAS
  • US11623769B2 patent drawing
  • US11623769B2 patent drawing
  • US11623769B2 patent drawing

AI summary

A self-healing shield panel for protecting a spacecraft against High Velocity Particles (HVPs). The self-healing shield includes an exterior layer and an interior layer connected to define a cavity which contains a dilatant fluid with a plurality of spheroids. The kinetic energy from HVP impact is dispersed by the plurality of spheroids and absorbed by the dilatant fluid. The plurality of spheroids within the cavity move to block a puncture hole in the shield.