Cryogenic circuit conditioning system

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Solution Overview

Problem

Cryogenic propellant circuits in aircraft face challenges with humidity and oxygen exposure, leading to potential explosions and equipment deterioration, especially during atmospheric flight phases where traditional conditioning methods are cumbersome and mass-penetrating due to the need for onboard gas storage.

Innovation Solution

A system that extracts nitrogen from outside air using an OBIGGS-type separator and distributes it via a pipe circuit with calibrated orifices to condition cryogenic circuits during flight, eliminating the need for onboard gas storage and reducing mass penalties.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If nitrogen or helium is circulated continuously around cryogenic circuits during atmospheric flight, then the cryogenic circuits are protected from humidity and oxygen exposure, but the mass of the vehicle increases due to onboard gas storage tanks

Engineering Contradiction:
Improveprotection of cryogenic circuitsVSAvoidmass of vehicle
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The system uses the aircraft's own turbojet engine air intake to provide nitrogen for conditioning the cryogenic circuits. The nitrogen is extracted from the ambient air using an OBIGGS (On-Board Inert Gas Generator) system, eliminating the need for separate onboard nitrogen storage tanks. This self-service approach converts the aircraft's propulsion system into a dual-purpose system that also provides inert gas for cryogenic circuit protection.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The turbojet engine's air intake system, originally designed solely for propulsion, is utilized to supply nitrogen for cryogenic circuit conditioning. This multi-functional use of the air intake system eliminates the need for dedicated nitrogen storage infrastructure, reducing vehicle mass while maintaining protection capabilities during atmospheric flight.

Inventive Principle:
Principle #6Universality (Multi-functionality)

2Duration of action of moving object

If nitrogen storage tanks and conditioning gas are carried on board the spaceplane, then in-flight conditioning of cryogenic circuits is enabled, but the dry mass becomes very penalizing

Engineering Contradiction:
Improvein-flight conditioning capabilityVSAvoiddry mass
Core Design Contradiction:
Duration of action of moving objectVSWeight of stationary object

Solution Approach 1:

The system eliminates the need for onboard nitrogen storage tanks by continuously extracting nitrogen from ambient air during flight using the OBIGGS system. The air intake is connected to the turbojet engine's compression system, which pressurizes and delivers the nitrogen to the distribution network, enabling sustained in-flight conditioning without carrying heavy gas storage infrastructure.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The system changes the source of nitrogen from stored onboard reserves to continuous extraction from ambient air. By utilizing the dynamic parameters of flight (airflow through the engine intake, compression pressure), the system maintains nitrogen supply for conditioning without the static mass penalty of storage tanks, enabling duration-based operation proportional to flight time.

Inventive Principle:
Principle #35Parameter changes

3Reliability

If ground-based conditioning circuits are used before takeoff, then cryogenic circuits are protected from humidity and oxygen, but the system becomes complex and disconnected during flight

Engineering Contradiction:
Improveconditioning of cryogenic circuitsVSAvoidconditioning system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The system merges the ground-based conditioning infrastructure with the aircraft's own propulsion system. The OBIGGS system integrates with the turbojet engine's air intake and compression system, allowing the same hardware to provide nitrogen conditioning both on the ground (when connected to ground equipment) and in-flight (using engine-compressed air), thereby simplifying the overall system architecture and eliminating disconnection requirements.

Inventive Principle:
Principle #5Merging (Combining)

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

This solution effectively prevents humidity and oxygen ingress, maintaining equipment integrity and reducing mass by using ambient air nitrogen for in-flight conditioning, thereby enhancing performance and safety without the need for onboard gas storage.

Implementation Method 1

extracts the nitrogen therefrom by means of a nitrogen separator of the OBIGGS type

Methodology Applied
Scientific EffectGas separation:

Implementation Method 2

distributing this nitrogen around said components via a circuit of pipes provided with calibrated orifices

Methodology Applied
Scientific EffectGas flow control:

Implementation Method 3

the humidity of this air freezes at the contact with these circuits

Methodology Applied
Scientific EffectCryogenic cooling: Cryogenics

Implementation Method 4

the oxygen in the air will also be able to liquefy and accumulate

Methodology Applied
Scientific EffectLiquefaction: Condensation

Data Source

PatentEP2948665B1Cryogenic circuit conditioning system
Publication Date: 2020.06.24 ARIANEGRP SAS
  • EP2948665B1 patent drawingFigure 1
  • EP2948665B1 patent drawingFigure 2

AI summary

The subject of the invention is a device for the in-flight conditioning of equipment (6, 7, 8) of cryogenic circuits of an aircraft, which device comprises means for bleeding air from outside the aircraft, means for extracting nitrogen from this air using a nitrogen separator of the OBIGGS type (3) and means (4, 5) for distributing this nitrogen around said equipment. The device notably comprises means for distributing nitrogen around the various pieces of equipment of cryogenic circuits using a system of piping (4) provided with calibrated orifices (5).