Habitat Pressure Control for Modular Spacecraft Compartments

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Solution Overview

Problem

Current habitat control systems in planetary and orbital space vehicles lack efficient and scalable solutions for controlling oxygen and nitrogen partial pressures in various compartments, particularly requiring localized and redundant pressure management for different modules and environments.

Innovation Solution

An environmental control system with high-pressure regulators, sensors, and control boards that adjust oxygen and nitrogen levels within modules, including pressure relief mechanisms, and a supervisory controller for centralized management and redundancy across multiple modules.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If a centralized habitat control system is used for the entire space vehicle, then system complexity is reduced and fewer spare parts are needed, but localized pressure control in individual compartments becomes less efficient and responsive

Engineering Contradiction:
Improvesystem complexityVSAvoidlocalized pressure control
Core Design Contradiction:
Device complexityVSEase of operation

Solution Approach 1:

The system divides the space vehicle into multiple discrete compartments (crew lock chamber, airlock chamber, habitat modules) each with its own localized pressure control capabilities through distributed control panels, while maintaining overall system coordination. This segmentation allows independent control of each compartment's oxygen and nitrogen levels without requiring a fully centralized system.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system combines centralized supervisory control with distributed local control panels. The centralized computer monitors and coordinates overall habitat pressure, while local control panels provide immediate responsive control for specific compartments. This merging of control levels resolves the contradiction by achieving both system-wide simplicity and localized responsiveness.

Inventive Principle:
Principle #5Merging (Combining)

2Ease of operation

If separate control systems are implemented for each compartment to achieve precise localized control, then localized pressure management improves, but the number of spare parts and system complexity increases

Engineering Contradiction:
Improvelocalized pressure controlVSAvoidsystem complexity
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The control system uses universal, identical control panels and sensor packages that can be deployed in any compartment. Each control panel performs the same functions (oxygen control, nitrogen control, pressure monitoring) across different compartments, allowing interchangeability and reducing the variety of spare parts needed while maintaining localized control capability.

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

Solution Approach 2:

The system controls pressure by adjusting the parameters of gas composition (oxygen and nitrogen partial pressures) rather than using mechanically complex pressure regulation mechanisms. This approach simplifies the control system by using electronic control of gas flow and composition to achieve precise pressure management in each compartment.

Inventive Principle:
Principle #35Parameter changes

3Productivity

If high-pressure oxygen and nitrogen supplies are used to control partial pressures in compartments, then efficient gas delivery is achieved, but pressure safety risks and the need for pressure relief mechanisms increase

Engineering Contradiction:
Improvegas delivery efficiencyVSAvoidpressure safety risks
Core Design Contradiction:
ProductivityVSObject-affected harmful factors

Solution Approach 1:

The system incorporates pressure relief solenoid valves that automatically activate when pressure exceeds safe thresholds, preventing dangerous pressure buildup before it can cause harm. Oxygen and nitrogen control boards continuously monitor partial pressures and adjust gas flow to prevent unsafe conditions, applying counter-actions in advance to offset potential harmful effects.

Inventive Principle:
Principle #9Preliminary anti-action

Solution Approach 2:

The system uses intermediate pressure regulation stages and control boards that act as mediators between the high-pressure gas supplies and the compartment environments. These intermediary components gradually reduce and control the pressure, preventing direct high-pressure injection into compartments while maintaining efficient gas delivery through controlled flow regulation.

Inventive Principle:
Principle #24Intermediary (Mediator)

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

Enables precise and redundant control of oxygen and nitrogen levels, emulating sea-level conditions, and ensuring safe and customizable habitat environments in space vehicles, with modular design for scalability and reduced spare parts requirements.

Implementation Method 1

an oxygen high-pressure regulator disposed between the oxygen supply and the first oxygen control board, the oxygen high-pressure regulator configured to reduce a high-pressure oxygen gas to a low-pressure oxygen gas

Methodology Applied
Scientific EffectPressure reduction: Pressure Drop

Implementation Method 2

a nitrogen high-pressure regulator disposed between the nitrogen supply and the first nitrogen control board, the nitrogen high-pressure regulator configured to reduce a high-pressure nitrogen gas to a low-pressure nitrogen gas

Methodology Applied
Scientific EffectPressure reduction: Pressure Drop

Implementation Method 3

an oxygen sensor configured to measure the partial pressure of oxygen within the first module

Methodology Applied
Scientific EffectPressure measurement:

Implementation Method 4

an ambient pressure sensor configured to measure the ambient pressure within the first module

Methodology Applied
Scientific EffectPressure measurement:

Data Source

PatentEP4129836B1Extensible habitat pressure control for planetary and orbital space vehicles
Publication Date: 2024.11.20 BE AEROSPACE INC
  • EP4129836B1 patent drawingFigure 1
  • EP4129836B1 patent drawingFigure 2
  • EP4129836B1 patent drawingFigure 3

AI summary

An environmental control system for a space vehicle includes an oxygen supply (206, 306), a nitrogen supply (208, 308), a first pressure nitrogen supply (312) having a first oxygen control board configured to receive an oxygen gas from the oxygen supply (206, 306) and a first nitrogen control board configured to receive a nitrogen gas from the nitrogen supply (208, 308), and a supervisory controller configured to control the first pressure nitrogen supply (312) and thereby to adjust a partial pressure of oxygen and an ambient pressure of an oxygen/nitrogen gas mixture within a first module.