Pressurized Condenser for Aircraft Fuel Tank Inerting

Solution Overview

Problem

Existing onboard inert gas generating systems for aircraft fuel tanks produce humid oxygen-depleted air, which requires methods to reduce water content to prevent ice formation and ensure safe operation.

Innovation Solution

A system that includes a chemical inert gas generator, a condenser operating at pressures greater than or equal to 2 atmospheres absolute pressure, and a boost compressor with a heat exchanger to produce and dry oxygen-depleted air, using catalytic oxidation, proton exchange membrane, or solid oxide electrochemical devices to reduce water content effectively.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a condenser operates at atmospheric pressure to dry oxygen-depleted air, then the system structure is simple, but ice may form in the protected space

Engineering Contradiction:
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent changes the pressure parameter of the condenser from atmospheric pressure to pressurized operation (greater than or equal to 2 atmospheres absolute pressure). This parameter change raises the dew point temperature, allowing water condensation to occur at higher temperatures that prevent ice formation while maintaining effective drying functionality.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent introduces a pressurized condenser as an intermediary component between the oxygen-depleted air source and the protected space. This intermediary device performs the critical function of removing water vapor through condensation under pressurized conditions, preventing ice formation without requiring complex additional heating or temperature control systems.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If the condenser operates at higher pressure to prevent ice formation, then ice formation is prevented, but the device complexity increases

Engineering Contradiction:
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent modifies the operational parameters of the condenser by operating at pressurized conditions (greater than or equal to 2 atmospheres absolute pressure) rather than atmospheric pressure. This parameter change fundamentally alters the condensation behavior, enabling water removal at temperatures that prevent ice formation while maintaining system safety.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The pressurized condenser system utilizes the inherent properties of pressurized gas condensation to achieve water removal without requiring additional external heating systems or complex temperature control mechanisms. The system leverages the elevated dew point at pressurized conditions to enable self-regulating condensation that prevents ice formation.

Inventive Principle:
Principle #25Self-service

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 system effectively reduces water content in oxygen-depleted air, preventing ice formation and ensuring safe operation by maintaining the air above freezing temperatures, thus enhancing the safety and efficiency of fuel tank inerting.

Implementation Method 1

reducing the water content of the inert gas in the condenser

Methodology Applied
Scientific EffectCondensation: Condensation

Implementation Method 2

The catalytic oxidation unit may operate at a temperature greater than 150° C.

Methodology Applied
Scientific EffectCatalytic oxidation: Catalysis

Implementation Method 3

The pressurized air flow path includes a heat exchanger before the boost compressor and an additional heat exchanger after the boost compressor.

Methodology Applied
Scientific EffectHeat exchange: Heat Exchanger

Data Source

PatentUS11834191B2Pressurized inerting system
Publication Date: 2023.12.05
  • US11834191B2 patent drawing
  • US11834191B2 patent drawing
  • US11834191B2 patent drawing

AI summary

A system and method for providing dried inert gas to a protected space is disclosed.