Multi-layer metal insulation shunting thermal transfer above 1200°C

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Solution Overview

Problem

Existing thermal protection systems (TPS) struggle to effectively isolate interior systems from extreme thermal environments above 1200°C, while also meeting structural requirements to handle thermomechanical stresses and high shear and tensile loads.

Innovation Solution

The development of an integrated multi-layer metal insulation (MLMI) structure using refractory metal sheet layers separated by skeletal cage framework standoffs, which limits thermal transfer to less than 2.5 W/mK and provides structural support through load-carrying capabilities.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If a single sandwich structure with thermal protective material is used, then thermal insulation is provided, but structural strength to handle thermomechanical stresses above 1200°C is insufficient

Engineering Contradiction:
Improvethermal insulation performanceVSAvoidstructural strength
Core Design Contradiction:
TemperatureVSStrength

Solution Approach 1:

The TPS is divided into multiple discrete layers (outer refractory metal layer, intermediate insulating layer, inner refractory metal layer) separated by crate standoffs. This segmentation allows each layer to be optimized for its specific function: outer and inner layers provide structural strength and high-temperature resistance, while the intermediate layer provides thermal insulation, resolving the contradiction between thermal insulation and structural strength.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The TPS uses composite construction combining different refractory metals (such as niobium, molybdenum, tungsten) with distinct material properties. The outer and inner layers use materials optimized for structural strength and temperature resistance, while the intermediate layer uses materials optimized for low thermal conductivity, creating a composite structure that simultaneously achieves both structural integrity and thermal insulation above 1200°C.

Inventive Principle:
Principle #40Composite materials

2Strength

If refractory metal sheet layers are used to provide structural support, then strength to handle thermomechanical stresses is improved, but thermal conductivity increases above acceptable levels

Engineering Contradiction:
Improvestructural strengthVSAvoidthermal conductivity
Core Design Contradiction:
StrengthVSLoss of energy

Solution Approach 1:

An intermediate insulating layer composed of materials with low thermal conductivity (such as refractory ceramic fibers, aerogels, or insulating ceramics) is introduced between the refractory metal sheet layers. This intermediary layer acts as a thermal barrier that blocks heat transfer while allowing the outer and inner refractory metal layers to provide structural strength, thereby reducing overall thermal conductivity while maintaining structural integrity.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

Different regions of the TPS are assigned different material properties: the outer and inner layers use refractory metals with high strength and temperature resistance, while the intermediate layer uses materials specifically selected for low thermal conductivity. This local differentiation of material quality allows the structure to simultaneously achieve both structural strength and low thermal conductivity, preventing excessive heat transfer while maintaining ability to handle thermomechanical stresses.

Inventive Principle:
Principle #3Local quality

3Force

If crate standoffs with open cells are used for structural support, then load-carrying capability is improved, but convective heat transfer increases

Engineering Contradiction:
Improveload-carrying capabilityVSAvoidconvective heat transfer
Core Design Contradiction:
ForceVSLoss of energy

Solution Approach 1:

The crate standoffs incorporate porous or cellular structures with controlled pore sizes and configurations. These porous materials provide structural strength and load-carrying capability while the pore geometry is designed to disrupt convective airflow patterns. The porous structure creates tortuous flow paths that reduce convective heat transfer efficiency, allowing the standoffs to maintain structural integrity while minimizing convective heat transfer between layers.

Inventive Principle:
Principle #31Porous materials

Solution Approach 2:

The crate standoffs feature curved or rounded cell geometries rather than sharp angular structures. These curved surfaces disrupt laminar flow patterns and reduce convective heat transfer by creating flow separation and recirculation zones within the cellular structure. The curved geometry maintains structural strength while effectively reducing convective heat transfer between the refractory metal layers.

Inventive Principle:
Principle #14Spheroidality (Curvature)

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 MLMI structure effectively isolates interior systems from extreme temperatures, maintaining the innermost layer below 150°F (66°C) even under exposure to temperatures up to 3500°F (1927°C), while providing structural integrity to handle thermomechanical stresses.

Implementation Method 1

Each crate standoff limits thermal transfer from one sheet layer to the next to less than 2.5 W/mK

Methodology Applied
Scientific EffectThermal conduction: Conduction (thermal)

Implementation Method 2

The cells restrict any internal air flow to substantially eliminate convective heat transfer

Methodology Applied
Scientific EffectConvection: Convection

Implementation Method 3

The skeletal cage framework provides load carrying, while also creating a tortuous throughput thermal path that lowers conductive heat transfer to less than 5% of environmental exposure

Methodology Applied
Scientific EffectThermal conduction: Conduction (thermal)

Implementation Method 4

Developing exterior-to-interior temperature gradients in typical hypersonic flight profiles can lead to differential thermal expansion of outer parts of a TPS structure that produce thermomechanical stresses

Methodology Applied
Scientific EffectThermal expansion: Thermal Expansion

Data Source

PatentUS12275214B1Multi-layer metal insulation to shunt thermal transfer from external environments above 1200° C
Publication Date: 2025.04.15 PEREGRINE FALCON CORP
  • US12275214B1 patent drawing
  • US12275214B1 patent drawing
  • US12275214B1 patent drawing

AI summary

An integrated multi-layer metal insulation structure thermally isolates an interior system from external environments more than 1200° C. Three or more refractory metal sheet layers are separated from one another by respective standoffs, where refractory metal comprises any elemental or alloy metal with a melting point more than 1600° C. Each standoff is in the form of a skeletal cage framework of refractory metal ribs with cells between the ribs. Successive interlayers are offset from one another to shunt the heat transfer laterally at each sheet layer. The ribs may have cutouts and the cells may be partially open. Each crate standoff limits thermal transfer from one sheet layer to the next to less than 2.5 W/mK, including the cells restricting air flow to substantially eliminate convective heat transfer and the skeletal cage framework creating a tortuous thermal path that lowers conductive heat transfer to less than 5% of environmental exposure.Conductive transfer can be lowest for the innermost interlayer forming a thermal gate.