Steam Condensation for Cabin Pressurization Simulation

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Solution Overview

Problem

Current ground-based pressure chambers for simulating cabin or cargo pressurization/depressurization cycles are costly and energy-intensive, often requiring large and expensive facilities to accurately test high-altitude conditions, which are not adequately represented due to differences in air density and pressure from sea level to high altitudes.

Innovation Solution

A method and system using a condensation chamber with steam to reduce pressure by condensing vapor into a liquid, allowing air to flow in and out to simulate pressurization/depressurization cycles, reducing energy consumption and facility maintenance costs, while providing a realistic test environment.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If traditional ground-based pressure chambers are used to simulate high-altitude conditions, then pressurization/depressurization cycles can be tested, but energy consumption is excessive and facility costs are high

Engineering Contradiction:
Improveaccuracy of high-altitude simulationVSAvoidenergy consumption
Core Design Contradiction:
ReliabilityVSUse of energy by moving object

Solution Approach 1:

The patent uses phase transition of water (liquid to vapor to liquid) to control pressure in the chamber. Water is heated to generate steam that increases pressure, then condensed back to liquid to create vacuum, eliminating the need for energy-intensive mechanical compressors and vacuum pumps

Inventive Principle:
Principle #36Phase transitions

Solution Approach 2:

The system changes temperature parameters to control pressure. By heating water to generate steam and then cooling it to condense, the system achieves pressure control through temperature manipulation rather than mechanical means, significantly reducing energy consumption

Inventive Principle:
Principle #35Parameter changes

2Measurement precision

If altitude chambers are used for full-scale cabin mock-up testing, then realistic high-altitude conditions can be simulated, but facility costs and maintenance expenses are prohibitively high

Engineering Contradiction:
Improveaccuracy of flight condition simulationVSAvoidfacility cost
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent employs water phase transitions (liquid-vapor-liquid) as a cost-effective alternative to expensive mechanical pressure control systems. This natural physical process provides reliable pressurization and depressurization without requiring costly altitude chambers or complex mechanical infrastructure

Inventive Principle:
Principle #36Phase transitions

Solution Approach 2:

The system creates a simplified copy of flight pressure conditions using basic water phase change mechanics, achieving the essential simulation requirement without replicating the full complexity and cost of traditional altitude chambers

Inventive Principle:
Principle #26Copying

3Ease of operation

If mechanical compressors and vacuum pumps are used for pressure control, then pressurization/depressurization can be achieved, but the system is energy-intensive and complex

Engineering Contradiction:
Improvepressure control capabilityVSAvoidenergy consumption
Core Design Contradiction:
Ease of operationVSUse of energy by stationary object

Solution Approach 1:

The patent replaces mechanical compressors and vacuum pumps with a phase transition-based pressure control system. Water heated to steam provides pressurization, and condensed steam creates vacuum, eliminating the need for energy-intensive mechanical equipment while maintaining operational effectiveness

Inventive Principle:
Principle #36Phase transitions

Solution Approach 2:

The system substitutes mechanical pressure control mechanisms with a thermal-phase change based system. Instead of using mechanical compressors and pumps, the patent uses heating and cooling processes to naturally generate pressure differentials through water phase transitions

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

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 approach creates a cost-effective, environmentally friendly, and energy-efficient ground-based test facility that accurately simulates cabin or cargo pressurization/depressurization cycles, allowing for realistic testing of air distribution systems and human thermal comfort under flight conditions, reducing the need for expensive altitude chambers.

Implementation Method 1

A first quantity of steam is inserted into a condensation chamber, and the first quantity of steam is substantially condensed in the condensation chamber

Methodology Applied
Scientific EffectCondensation: Condensation

Data Source

PatentEP2562089B1System and methods for ground-based cabin/cargo pressurization/depressurization
Publication Date: 2019.10.09 THE BOEING CO
  • EP2562089B1 patent drawingFigure 1
  • EP2562089B1 patent drawingFigure 2
  • EP2562089B1 patent drawingFigure 3

AI summary

A system and methods for reducing pressure in an enclosed volume (104) is disclosed. A first quantity of steam (106) is inserted into a condensation chamber (110), and the first quantity of steam is substantially condensed in the condensation chamber. A first quantity of air (102) is extracted from an enclosed volume (104) into the condensation chamber (110).