Aircraft Ecoecs Ram Air Circuit Energy Recovery

Solution Overview

Problem

Current aircraft environmental control systems face limitations in efficiency regarding engine fuel burn, as traditional methods such as bleed air usage provide only limited improvements.

Innovation Solution

An environmental control system that utilizes a ram air circuit with heat exchangers, a dehumidification system, and compression and expansion devices to mix and process different air mediums, leveraging energy from bleed air, fresh air, and cabin discharge air to enhance efficiency and cabin pressurization and cooling.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If bleed air is used for air conditioning, then cooling performance is achieved, but engine fuel burn efficiency deteriorates

Engineering Contradiction:
Core Design Contradiction:
TemperatureVSUse of energy by moving object

Solution Approach 1:

The system recovers energy from cabin outflow air that would otherwise be discarded, using it to drive a compressor to compress outside air for cabin conditioning, thereby improving fuel efficiency while maintaining cooling performance

Inventive Principle:
Principle #34Discarding and recovering

Solution Approach 2:

The system uses the cabin's own outflow air to provide the driving force for compression, creating a self-sustaining cycle that reduces dependence on external energy sources and improves overall efficiency

Inventive Principle:
Principle #25Self-service

2Use of energy by moving object

If electrical power is used to compress outside air, then fuel burn efficiency improves, but system complexity and power requirements worsen

Engineering Contradiction:
Core Design Contradiction:
Use of energy by moving objectVSDevice complexity

Solution Approach 1:

The system uses pneumatic principles by capturing the pressure energy in cabin outflow air to drive a turbine-compressor system, eliminating the need for electrical compression and reducing system complexity while maintaining fuel efficiency benefits

Inventive Principle:
Principle #29Pneumatics and hydraulics

3Use of energy by moving object

If cabin outflow air energy is used to compress outside air, then fuel burn efficiency improves, but system complexity worsens

Engineering Contradiction:
Core Design Contradiction:
Use of energy by moving objectVSDevice complexity

Solution Approach 1:

The system merges the turbine and compressor into a single integrated device, allowing the outflow air to directly drive the compression of outside air through a combined turbine-compressor assembly, thereby reducing the number of separate components while achieving the desired efficiency improvement

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 system achieves high fuel burn efficiency by effectively mixing and processing various air mediums, optimizing energy use and cooling performance, thereby improving the overall efficiency of aircraft environmental control.

Implementation Method 1

a ram air circuit with a ram air shell having at least one heat exchanger positioned therein

Methodology Applied
Scientific EffectHeat exchange: Heat Exchanger

Implementation Method 2

a compression device arranged in fluid communication with the ram air circuit and the at least one dehumidification system

Methodology Applied
Scientific EffectCompression: Compression

Implementation Method 3

an expansion device arranged in fluid communication with the ram air circuit

Methodology Applied
Scientific EffectExpansion: Adiabatic Cooling

Data Source

PatentUS11192655B2Regenerative system ECOECS
Publication Date: 2021.12.07
  • US11192655B2 patent drawing
  • US11192655B2 patent drawing
  • US11192655B2 patent drawing

AI summary

An environmental control system of an aircraft includes a ram air circuit with a ram air shell having at least one heat exchanger positioned therein, a dehumidification system arranged in fluid communication with the ram air circuit, a compression device arranged in fluid communication with the ram air circuit and the at least one dehumidification system, and an expansion device arranged in fluid communication with the ram air circuit. At least one of the compression device and the expansion device is selectively operable to supplement the ram air within the ram air circuit to meet a demand of the aircraft.