Fuel Cell Exhaust Split Flow for Turbine Pressure Control

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Solution Overview

Problem

Fuel cell systems face challenges in efficiently managing exhaust flows to optimize energy recovery and maintain desired flow rates within the fuel cell assembly.

Innovation Solution

The exhaust system includes a flow device that separates the fuel cell exhaust into two flows, with a turbine configured to extract energy from one portion and an ejector that uses the second flow to create suction on the turbine exhaust, thereby controlling the differential pressure through the turbine.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of energy

If a turbine is used to extract energy from exhaust flow, then energy recovery is improved, but the differential pressure control becomes difficult and complicates the flow management

Engineering Contradiction:
Improveenergy recoveryVSAvoidflow management complexity
Core Design Contradiction:
Loss of energyVSDevice complexity

Solution Approach 1:

The exhaust flow is divided into two separate streams: one stream passes through the turbine for energy extraction, while the other stream bypasses the turbine. This segmentation allows independent control of each stream, enabling the bypass flow to be used for differential pressure control without interfering with the turbine's energy extraction function.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The bypass flow acts as an intermediary medium to control the differential pressure across the fuel cell assembly. By adjusting the flow rate of the bypass stream, the system can regulate the pressure differential without directly interfering with the turbine operation, thus decoupling the energy recovery function from the pressure control function.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Productivity

If the flow device increases the second flow to increase flow through the fuel cell assembly, then the flow rate through the fuel cell is improved, but the exhaust flow to the turbine decreases

Engineering Contradiction:
Improveflow rate through fuel cell assemblyVSAvoidexhaust flow to turbine
Core Design Contradiction:
ProductivityVSQuantity of substance

Solution Approach 1:

The total exhaust flow is segmented into two independent controllable streams. The flow device can increase the second flow (bypass flow) to enhance fuel cell assembly flow rate without significantly impacting the first flow (turbine flow), as the segmentation allows relatively independent adjustment of each stream's flow rate.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system dynamically adjusts the flow distribution between the two streams based on operating conditions. The flow device can modulate the second flow rate dynamically to optimize fuel cell assembly performance, while the turbine continues to receive adequate exhaust flow for energy extraction, with the bypass flow serving to regulate pressure differentials.

Inventive Principle:
Principle #15Dynamics

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 allows for dynamic control of the flow rates through the fuel cell assembly and the turbine, enhancing energy recovery and maintaining optimal operating conditions by adjusting the differential pressure and backpressure.

Implementation Method 1

The ejector is configured to provide a suction on the turbine exhaust using the second flow

Methodology Applied
Scientific EffectSuction: Suction

Implementation Method 2

altering the suction alters a differential pressure through the turbine (e.g., a differential pressure from a turbine inlet to a turbine outlet)

Methodology Applied
Scientific EffectPressure differential control: Pressure Gradient

Implementation Method 3

A turbine of the exhaust system is configured to receive and extract energy from at least a portion of the exhaust flow and discharge a turbine exhaust

Methodology Applied
Scientific EffectEnergy extraction: Turbine

Implementation Method 4

The flow device is configured to substantially separate the fuel cell exhaust into an exhaust flow comprising a first portion of the fuel cell exhaust and a second flow comprising a second portion of the fuel cell exhaust

Methodology Applied
Scientific EffectFlow separation: Flow Separation

Implementation Method 5

The fuel cell assembly is configured to receive a fuel comprising hydrogen and an oxidizing agent comprising oxygen and generate electrical power using the fuel and the oxidizing agent

Methodology Applied
Scientific EffectOxidation: Oxidation

Implementation Method 6

The fuel cell assembly is configured to receive an inlet feed at a fuel cell inlet and discharge a fuel cell exhaust at a fuel cell outlet fluidically coupled to the fuel cell inlet, wherein the inlet feed comprises one of an oxidizing agent or a fuel, and wherein the fuel cell assembly is configured to oxidize the fuel using the oxidizing agent

Methodology Applied
Scientific EffectFuel cell reaction: Fuel Cell

Data Source

PatentEP4542692A1Fuel cell system
Publication Date: 2025.04.23 HONEYWELL INTERNATIONAL INC
  • EP4542692A1 patent drawingFigure 1
  • EP4542692A1 patent drawingFigure 2
  • EP4542692A1 patent drawingFigure 3

AI summary

In some examples, an exhaust system of a fuel cell system includes a flow device configured to discharge a first portion of a fuel cell exhaust as an exhaust flow and a second portion of the fuel cell exhaust as a second flow. A turbine of the exhaust system is configured to receive at least a portion of the exhaust flow and discharge a turbine exhaust. An ejector configured to receive the turbine exhaust at a first inlet and receive the second flow from the flow device. The ejector is configured to provide a suction on the turbine exhaust using the second flow. The exhaust system includes control circuitry configured to cause the flow device to alter the second flow.