Cryogenic Pipe Assembly With Composite Outer Tube and Thermal Isolation

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

The integration of cryogenic fluid pipes into the primary structure of aerospace systems poses challenges due to material-dependent length changes, thermal insulation difficulties at fastening points, and the dual use of pipes for structural support and fluid conduction, which increases heat flow and complicates secure connections.

Innovation Solution

A pipe design comprising a fibre-reinforced polymer outer tube with a gas-proof inner tube and insulation layer, where the outer tube bears structural loads and the inner tube conducts cryogenic fluids, minimizing thermal expansion and heat ingress, with flanges for secure connections and thermal stabilization.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Weight of moving object

If pipes are integrated into the primary structure for structural support, then weight is reduced, but thermal expansion compensation becomes difficult

Engineering Contradiction:
Improvesystem massVSAvoidthermal expansion compensation
Core Design Contradiction:
Weight of moving objectVSEase of operation

Solution Approach 1:

The pipe is divided into two separate tubes: an outer tube for structural support and an inner tube for fluid conduction. This segmentation allows each tube to be optimized for its specific function, with the outer tube providing structural integration and the inner tube handling thermal expansion independently through its own insulation and movement capability.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The inner tube is nested within the outer tube, creating a concentric arrangement where the inner tube can expand and contract independently while remaining constrained by the outer tube. This nested structure enables thermal expansion compensation without compromising the structural integration into the primary system.

Inventive Principle:
Principle #7Nested doll (Nesting)

2Strength

If pipes are used for structural support, then stiffness and stability are improved, but the number of connection points increases leading to augmented heat flow

Engineering Contradiction:
Improvestructural stiffnessVSAvoidheat flow into pipes
Core Design Contradiction:
StrengthVSLoss of energy

Solution Approach 1:

The outer tube is made of fibre-reinforced polymer with different laminate structures in different regions: a first laminate in the centre region and a second laminate in the end region. This local quality variation optimizes structural stiffness where needed while minimizing thermal conductivity at connection points, thereby reducing heat flow into the cryogenic fluid.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The outer tube uses composite fibre-reinforced polymer materials with tailored laminate structures, combining different fibre orientations and material properties to achieve optimal balance between structural stiffness and thermal insulation performance at different locations along the tube.

Inventive Principle:
Principle #40Composite materials

3Temperature

If insulation is added to reduce heat flow, then thermal insulation is improved, but insulation at fastening points becomes difficult due to conductive connections

Engineering Contradiction:
Improvethermal insulationVSAvoidinsulation at fastening points
Core Design Contradiction:
TemperatureVSEase of manufacture

Solution Approach 1:

The pipe system is segmented into an outer structural tube and an inner fluid-conducting tube with insulation between them. This segmentation allows the insulation layer to be effectively placed in the thermal path while fastening points can be attached to the outer tube without compromising insulation, as the inner tube remains thermally isolated.

Inventive Principle:
Principle #1Segmentation

4Strength

If classical metal pipes are used, then structural integration is achieved, but material-dependent length changes require compensators

Engineering Contradiction:
Improvestructural integrationVSAvoidthermal expansion
Core Design Contradiction:
StrengthVSLength of moving object

Solution Approach 1:

The outer tube uses fibre-reinforced polymer with specifically engineered laminate structures that provide low coefficient of thermal expansion in critical directions. By changing the material parameters and fibre orientation, the tube maintains dimensional stability under cryogenic temperature variations while still providing structural support.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The use of composite fibre-reinforced polymer materials allows tailoring of thermal expansion properties through laminate design, achieving low thermal expansion in the longitudinal direction while maintaining structural strength and stiffness for primary structure integration.

Inventive Principle:
Principle #40Composite materials

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 design allows for weight-saving, thermally stable, and structurally efficient integration of cryogenic fluid pipes into aerospace systems, reducing the need for compensators and enhancing durability through minimized thermal expansion and improved connection methods.

Implementation Method 1

an (thermal) insulation layer in-between

Methodology Applied
Scientific EffectThermal insulation: Thermal Insulation

Implementation Method 2

a significant cooling of the pipes occurs during operation. This change in temperature between the state of assembling on the one hand and operating states on the other hand leads to large, material-dependent changes in length

Methodology Applied
Scientific EffectThermal expansion: Thermal Expansion

Data Source

PatentEP4653737A1Pipe for a cryogenic fluid, pipe assembly, and aerospace system with pipe
Publication Date: 2025.11.26 ARIANEGRP GMBH
  • EP4653737A1 patent drawingFigure 1~2b
  • EP4653737A1 patent drawingFigure 3~4
  • EP4653737A1 patent drawing

AI summary

Disclosed is a pipe 100, 100', 1002' for conducting a cryogenic fluid. The pipe comprises a rigid outer tube 10, 10', 102' at least partially made of a fibre-reinforced polymer, a gas-proof inner tube 20, 20', 202' running within the outer tube 10, 10', 102', an insulation layer 30, 30', 302' arranged between the inner tube 20, 20', 202' and the outer tube 10, 10', 102', and at least one flange 40, 40', 402' formed at a respective end of the inner tube 20, 20', 202'. The at least one flange 40, 40', 402' connects the inner tube 20, 20', 202' with the outer tube 10, 10', 102' . Further disclosed are a pipe assembly 1000 comprising at least two such pipes 100, 100', 1002' which are connected or configured to be connected at a respective flange 40, 40', 402' thereof, and an aerospace system comprising at least one such pipe 100, 100', 1002'.