Aircraft Power Generation via Air Separation and Turbine Coupling

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Solution Overview

Problem

Current fuel cell technologies for aircraft power generation are in early stages of adoption and require improvements in efficiency and performance to effectively serve as primary or secondary power sources.

Innovation Solution

A system comprising a compressor, air separation module, and hydrogen consuming power generation source, where a nitrogen-enriched air stream from the separation module rotates a turbine, which in turn drives the compressor, and an oxygen-enriched air stream is used by the power generation source, enhancing mechanical and electrical power generation efficiency.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Object-affected harmful factors

If fuel cell technologies are used for power generation, then environmental impact is reduced and fuel burn is reduced, but efficiency and performance need improvement

Engineering Contradiction:
Improveenvironmental impactVSAvoidpower generation efficiency
Core Design Contradiction:
Object-affected harmful factorsVSProductivity

Solution Approach 1:

The system changes the parameter of air composition by separating it into oxygen-enriched and nitrogen-enriched streams. The oxygen-enriched stream is supplied to the fuel cell to improve combustion efficiency, while the nitrogen-enriched stream is used in the turbine to generate mechanical power. This parameter change resolves the contradiction by optimizing both environmental performance and power generation efficiency simultaneously.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The air supply system is segmented into two separate streams: an oxygen-enriched stream for the fuel cell and a nitrogen-enriched stream for the turbine. This segmentation allows each component to receive optimized air composition, improving overall system efficiency while maintaining environmental benefits of fuel cell technology.

Inventive Principle:
Principle #1Segmentation

2Productivity

If air separation module is introduced to produce oxygen-enriched and nitrogen-enriched streams, then power generation efficiency is improved, but device complexity increases

Engineering Contradiction:
Improvepower generation efficiencyVSAvoidsystem complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The system merges the air separation module with the existing compressor and turbine components into an integrated power generation system. By combining these components, the system achieves improved power generation efficiency through oxygen-enriched fuel cell operation and nitrogen-enriched turbine power generation, while the integrated design helps manage the increased device complexity.

Inventive Principle:
Principle #5Merging (Combining)

3Power

If turbine is coupled to compressor to generate mechanical power, then power burden is reduced, but device complexity increases

Engineering Contradiction:
Improvemechanical power generationVSAvoidsystem complexity
Core Design Contradiction:
PowerVSDevice complexity

Solution Approach 1:

The turbine is coupled to the compressor to create a self-service system where the turbine generates mechanical power that drives the compressor. This configuration reduces the external power burden on the system while the integrated coupling manages the added device complexity through coordinated operation of the two components.

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

This configuration improves the efficiency of fuel cell systems by utilizing oxygen-enriched air and nitrogen-enriched air streams to generate mechanical and electrical power, reducing the power burden on the system and expanding the functionality of onboard aircraft systems.

Implementation Method 1

an air separation module configured to receive the pressurized air stream from the first compressor and produce therefrom a nitrogen-enriched air stream and an oxygen-enriched air stream

Methodology Applied
Scientific EffectAir separation:

Implementation Method 2

a turbine configured to receive the nitrogen-enriched air stream from the air separation module and rotate in response to receiving the nitrogen-enriched air stream

Methodology Applied
Scientific EffectTurbine rotation: Turbine

Implementation Method 3

a hydrogen consuming power generation source configured to receive the pressurized oxygen-enriched air stream from the second compressor

Methodology Applied
Scientific EffectFuel cell reaction: Fuel Cell

Implementation Method 4

hydrogen consuming power generation source

Methodology Applied
Scientific EffectCombustion: Combustion

Data Source

PatentUS20240217671A1Systems and methods for power generation and aircraft comprising the same
Publication Date: 2024.07.04 HONEYWELL INTERNATIONAL INC
  • US20240217671A1 patent drawing
  • US20240217671A1 patent drawing
  • US20240217671A1 patent drawing

AI summary

Systems and methods are provided for power generation, for example, onboard an aircraft. The system comprises a first compressor configured to produce a pressurized air stream from a source of air, an air separation module configured to receive the pressurized air stream and produce therefrom a nitrogen-enriched air stream and an oxygen-enriched air stream, a second compressor configured to produce a pressurized oxygen-enriched air stream from the oxygen-enriched air stream, a hydrogen consuming power generation source configured to receive the pressurized oxygen-enriched air stream, and a turbine that is either coupled to the first or second compressor and configured to receive the nitrogen-enriched air stream from the air separation module, rotate in response to receiving the nitrogen-enriched air stream, and thereby cause rotation of the first or second compressor coupled thereto.