Cold Sprayed Radiation Shielding Composite Layers

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Current radiation shielding technologies are inadequate for effectively protecting space vehicles from galactic cosmic radiation (GCR), which causes significant damage to mission-critical components, leading to costly failures and anomalies in aerospace missions.

Innovation Solution

A lightweight radiation shield is developed using cold spray additive manufacturing (CSAM) to create a layered structure with a refractory metal and an absorbing material, where the refractory layer decelerates high-energy particles, and the absorbing layer retains them, providing enhanced shielding capabilities.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Object-affected harmful factors

If conventional radiation shielding materials are used, then radiation protection is provided, but the shield becomes heavier and thicker

Engineering Contradiction:
Improveradiation protectionVSAvoidshield weight
Core Design Contradiction:
Object-affected harmful factorsVSWeight of stationary object

Solution Approach 1:

The patent applies composite materials by combining multiple layers of different materials (e.g., aluminum, polyethylene, boron nitride, tungsten carbide) to create a radiation shield that provides superior protection per unit weight. The composite structure allows each layer to contribute specific properties: aluminum provides structural integrity and basic shielding, polyethylene offers hydrogen-rich radiation absorption, boron nitride provides neutron capture capability, and tungsten carbide adds high-density radiation blocking. This multi-material approach resolves the contradiction by achieving enhanced radiation protection without proportionally increasing weight.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The patent segments the radiation shield into multiple functional layers, each designed to address specific types of radiation or provide specific protective functions. The layered structure includes outer structural layers, intermediate radiation-absorbing layers, and inner functional layers with specialized materials. This segmentation allows optimization of each layer's thickness and material composition to maximize protection efficiency while minimizing overall weight, directly resolving the contradiction between protection and weight.

Inventive Principle:
Principle #1Segmentation

2Object-affected harmful factors

If conventional radiation shielding materials are used, then radiation protection is provided, but the shield becomes thicker

Engineering Contradiction:
Improveradiation protectionVSAvoidshield thickness
Core Design Contradiction:
Object-affected harmful factorsVSLength of stationary object

Solution Approach 1:

The use of composite materials with high radiation attenuation coefficients (such as tungsten carbide and boron nitride) allows the shield to achieve the required protection level in a thinner configuration. These materials provide superior radiation blocking capability per unit thickness compared to conventional single-material shields, enabling reduced overall thickness while maintaining or enhancing protection effectiveness.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The patent applies local quality by varying the material composition and thickness of different layers based on the specific radiation threats they face. Each layer is locally optimized with materials and dimensions tailored to its position and function within the shield assembly, allowing the overall structure to be thinner while providing adequate protection throughout. This localized optimization prevents the need for uniform thickness increases across the entire shield.

Inventive Principle:
Principle #3Local quality

3Weight of stationary object

If cold spray additive manufacturing is used, then lightweight and effective shielding is achieved, but manufacturing complexity increases

Engineering Contradiction:
Improveshield weightVSAvoidmanufacturing process
Core Design Contradiction:
Weight of stationary objectVSEase of manufacture

Solution Approach 1:

The cold spray additive manufacturing process utilizes parameter changes by controlling particle velocity, temperature, and deposition conditions to achieve dense, adherent coatings of radiation shielding materials. By adjusting process parameters such as gas pressure, particle acceleration velocity, and substrate temperature, the manufacturing system can produce complex lightweight structures with controlled material properties, resolving the contradiction between achieving lightweight design and maintaining manufacturing feasibility.

Inventive Principle:
Principle #35Parameter changes

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 CSAM-based radiation shield is thinner, lighter, and more effective than conventional shields, offering a significant increase in radiation protection while maintaining structural integrity, as demonstrated by Monte Carlo simulations and nanomechanical characterization.

Implementation Method 1

propelling a particulate form of the refractory metal onto a substrate at a velocity resulting in adherence of the propelled metal to the substrate

Methodology Applied
Scientific EffectKinetic adhesion: Impact Force

Implementation Method 2

the refractory layer decelerates high-energy particles

Methodology Applied
Scientific EffectParticle deceleration: Compton Scattering

Implementation Method 3

the absorbing layer retains them

Methodology Applied
Scientific EffectParticle absorption: Absorption (physical)

Data Source

PatentUS11887742B2Cold sprayed radiation shielding
Publication Date: 2024.01.30 WORCESTER POLYTECHNIC INSTITUTE
  • US11887742B2 patent drawing
  • US11887742B2 patent drawing

AI summary

Radiation shield and methods for manufacturing a radiation shield are provided herein, the method includes identifying a substrate for the radiation shield; identifying at least one material for cold spraying on the substrate; applying by cold spray a coating of the at least one material on the substrate thereby obtaining a radiation shield. The radiation shield is lighter, thinner, and more efficient compared to conventional radiation shields.