Aircraft Engine Load Offloading During Climb for ECS Demand Control

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Solution Overview

Problem

Aircraft engines face significant stress and reduced lifespan due to high demands during flight, particularly during climb phases where high temperatures and loads necessitate efficient management of power consumption to extend engine life without compromising safety or functionality.

Innovation Solution

A method is developed to offload auxiliary loads, such as the Environmental Conditioning System (ECS), by formulating a strategy based on aircraft data models, reducing engine loading when specific conditions are met, such as during climb, by adjusting parameters like bleed air usage and cabin pre-cooling, ensuring no adverse impact on aircraft systems.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Speed

If the engine operates at high power during climb phase to meet aircraft performance demands, then the aircraft can achieve required climb performance and altitude, but the engine temperature increases significantly and engine life is reduced

Engineering Contradiction:
Improveclimb rateVSAvoidengine temperature
Core Design Contradiction:
SpeedVSTemperature

Solution Approach 1:

The system performs pre-cooling of the cabin and other auxiliary systems before the climb phase begins. This preliminary action reduces the thermal load on the engine during climb, allowing the engine to operate at high power for climb performance while generating less heat, thus extending engine life without compromising climb rate.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system extracts and manages thermal loads by separating auxiliary power demands (cabin conditioning, etc.) from the main engine load during climb. By pre-cooling the cabin and using stored cooling capacity, the thermal burden is removed from the engine during the critical climb phase, allowing high power operation without proportional temperature increase.

Inventive Principle:
Principle #2Taking out (Extraction)

2Temperature

If auxiliary loads such as ECS are reduced during climb to extend engine life, then engine temperature and loading are reduced, but cabin comfort and air quality may deteriorate

Engineering Contradiction:
Improveengine temperatureVSAvoidcabin environment quality
Core Design Contradiction:
TemperatureVSReliability

Solution Approach 1:

The system pre-cools the cabin and pre-conditions auxiliary systems before the climb phase when engine loading is high. This preliminary action stores cooling capacity and prepares the cabin environment so that when ECS load is reduced during climb, the cabin remains comfortable and air quality is maintained without requiring continuous high engine power.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system continuously monitors cabin temperature, humidity, and air quality parameters, and adjusts ECS operation accordingly. During climb, the feedback control ensures that ECS load is reduced only to the extent necessary for engine protection while maintaining cabin environment within acceptable limits, thus resolving the contradiction between engine temperature reduction and cabin quality maintenance.

Inventive Principle:
Principle #23Feedback

3Duration of action of stationary object

If a comprehensive model and monitoring system is implemented to manage engine loading, then engine life can be extended through optimized load management, but system complexity increases

Engineering Contradiction:
Improveengine lifeVSAvoidcontrol system complexity
Core Design Contradiction:
Duration of action of stationary objectVSDevice complexity

Solution Approach 1:

The system uses a unified performance model that serves multiple functions: predicting engine temperature, evaluating offloading strategies, and optimizing climb performance. This multi-functional approach consolidates what could be multiple separate complex systems into a single integrated model, extending engine life through comprehensive load management without proportionally increasing system complexity.

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

Solution Approach 2:

The performance model uses historical flight data and engine parameters to automatically evaluate and optimize offloading strategies without requiring extensive manual configuration or complex external control systems. The system self-adjusts based on recorded performance, reducing the need for additional complex monitoring and control infrastructure while still achieving extended engine life through optimized load management.

Inventive Principle:
Principle #25Self-service

Data Source

PatentUS11787553B2Engine loading regulation
Publication Date: 2023.10.17 HAMILTON SUNDSTRAND CORP
  • US11787553B2 patent drawing

AI summary

A method for regulating loading of an aircraft engine providing power to multiple loads, particularly ECS, comprising offloading selected power consuming loads according to a predetermined strategy when predetermined conditions are met.