Aircraft Air Conditioning Control for Reduced Process Air Demand

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Solution Overview

Problem

Aircraft air conditioning systems face high compressed process air demand, leading to excessive fuel consumption and thermal stresses on the process air source, particularly during rapid temperature changes or extreme ambient conditions, without considering the thermal dynamic behavior of the aircraft region.

Innovation Solution

An aircraft air conditioning system that includes a control unit to regulate the operation of the air conditioning unit based on the difference and change rate of temperatures between the mixed air and the actual aircraft region temperature, reducing the process air demand by adjusting the volume flow of fresh air, and incorporating sensors to monitor and manage these parameters.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If the air conditioning unit operates with high compressed process air demand to meet cooling or heating requirements, then the cooling or heating performance is improved, but the fuel consumption and thermal stresses on the process air source increase

Engineering Contradiction:
Improvecooling or heating performanceVSAvoidfuel consumption
Core Design Contradiction:
TemperatureVSUse of energy by moving object

Solution Approach 1:

The control unit continuously monitors the actual temperature in the aircraft region and the temperature of mixed air, using this feedback to dynamically adjust the operation of the air conditioning unit. This closed-loop control ensures optimal process air demand while maintaining desired temperature conditions, avoiding excessive fuel consumption and thermal stresses.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system dynamically adjusts the volume flow of fresh air based on real-time temperature differences and change rates. By making the air conditioning unit's operation adaptive rather than static, the system optimizes process air demand according to actual thermal conditions, reducing fuel consumption while maintaining cooling or heating performance.

Inventive Principle:
Principle #15Dynamics

2Speed

If the air conditioning unit operates with high compressed process air demand during rapid temperature changes, then the response speed to temperature changes is improved, but the thermal stresses on the process air source increase

Engineering Contradiction:
Improveresponse speed to temperature changesVSAvoidthermal stresses on process air source
Core Design Contradiction:
SpeedVSStress or pressure

Solution Approach 1:

The control unit uses feedback from temperature sensors to monitor both the actual temperature and the rate of temperature change. This enables the system to respond appropriately to thermal dynamics without applying excessive stress to the process air source during rapid temperature transitions.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system changes operational parameters (volume flow of fresh air) based on the detected temperature change rate. By adapting the process air demand to the actual thermal dynamics, the system maintains fast response capability while avoiding excessive thermal stresses during rapid temperature changes.

Inventive Principle:
Principle #35Parameter changes

3Productivity

If the volume flow of fresh air is increased to meet cooling or heating requirements, then the cooling or heating performance is improved, but the process air demand increases

Engineering Contradiction:
Improvecooling or heating performanceVSAvoidprocess air demand
Core Design Contradiction:
ProductivityVSQuantity of substance

Solution Approach 1:

The control unit continuously adjusts the volume flow of fresh air based on feedback from temperature sensors. This ensures that the process air demand matches the actual cooling or heating requirements, maintaining productivity while minimizing the quantity of process air consumed.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system dynamically changes the volume flow parameter of fresh air according to real-time temperature conditions. By optimizing this parameter, the system achieves the required cooling or heating performance with minimal process air demand.

Inventive Principle:
Principle #35Parameter changes

4Device complexity

If the air conditioning unit operates without considering thermal dynamic behavior, then the device complexity is reduced, but the fuel consumption increases

Engineering Contradiction:
Improvecontrol system complexityVSAvoidfuel consumption
Core Design Contradiction:
Device complexityVSUse of energy by moving object

Solution Approach 1:

The control unit implements a feedback mechanism that monitors temperature and temperature change rate, using this information to optimize process air demand. This relatively simple feedback approach significantly reduces fuel consumption without requiring complex control systems.

Inventive Principle:
Principle #23Feedback

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 reduces fuel consumption and thermal stresses on the process air source while maintaining desired cooling or heating performance, by optimizing the air conditioning unit's operation to match the real-time cooling or heating requirements of the aircraft region, thereby extending the lifespan of the process air source.

Implementation Method 1

In the air conditioning unit, the process air, upon flowing through at least one heat exchanger as well as through various compression and expansion units, may be cooled and expanded

Methodology Applied
Scientific EffectHeat exchange: Heat Exchanger

Implementation Method 2

In the air conditioning unit, the process air, upon flowing through at least one heat exchanger as well as through various compression and expansion units, may be cooled and expanded

Methodology Applied
Scientific EffectAdiabatic cooling: Adiabatic Cooling

Data Source

PatentUS10906653B2Aircraft air conditioning system with a reduced process air demand
Publication Date: 2021.02.02 AIRBUS (SAS)
  • US10906653B2 patent drawing

AI summary

An aircraft air conditioning system comprising an air conditioning unit adapted and configured to be supplied with compressed process air and to generate cold fresh air, a mixer adapted and configured to mix the cold fresh air from the air conditioning unit with recirculation air recirculated from an aircraft region to be air conditioned, an air outlet adapted and configured to direct mixed air from the mixer into the aircraft region, a first sensor adapted and configured to detect an actual temperature in the aircraft region, a second sensor adapted and configured to detect a temperature of the mixed air directed into the aircraft region, and a control unit adapted and configured to control an operation of the air conditioning unit in dependence on a difference between the temperature of the mixed air directed into the aircraft region and the actual temperature in the aircraft region.