Multi-Stage Turbocharger Thermal Bypass for Catalyst Light-Off

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Solution Overview

Problem

Dual-turbocharging systems face challenges in providing immediate catalyst light-off at engine startup due to thermal losses in exhaust gas, leading to delayed catalyst activation and increased costs and complexity with separate catalytic converters.

Innovation Solution

A multi-stage turbocharging system with a high pressure (HP) and low pressure (LP) turbine, featuring a valve assembly that allows exhaust gases to bypass both turbines directly to the catalytic converter, utilizing a Regulated Two Stage (R2S) valve and a warm-up valve to control exhaust flow, ensuring immediate catalyst light-off and maintaining optimal temperature.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Power

If exhaust gases pass through both turbine stages to provide high boost, then engine power is improved, but exhaust gas temperature decreases significantly causing delayed catalyst light-off

Engineering Contradiction:
Improveengine powerVSAvoidexhaust gas temperature
Core Design Contradiction:
PowerVSTemperature

Solution Approach 1:

The exhaust flow path is segmented into multiple routes: a primary path through both HP and LP turbines for power generation, and a bypass path that allows selective diversion of exhaust gases around the turbines to maintain high temperature for catalyst light-off. This segmentation enables independent control of power generation and thermal management functions.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

A bypass valve assembly acts as an intermediary device that mediates between the exhaust gases and the turbine stages. By opening or closing the bypass path, the valve assembly controls whether exhaust gases flow through the turbines (for power) or bypass them (for heat preservation), thus resolving the temperature-power conflict.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Loss of time

If a bypass path is added to enable direct exhaust flow to catalyst, then catalyst light-off is improved, but device complexity increases

Engineering Contradiction:
Improvecatalyst light-off timeVSAvoidexhaust flow control system
Core Design Contradiction:
Loss of timeVSDevice complexity

Solution Approach 1:

The bypass valve assembly is merged with the existing turbocharger housing and exhaust manifold structure. The bypass path utilizes available space within the turbocharger assembly, integrating the thermal management function into the power generation component rather than adding a completely separate system.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The bypass valve assembly serves multiple functions: it controls exhaust flow distribution between turbines and bypass path, manages catalyst temperature, and can potentially control boost pressure. This multi-functionality reduces the need for additional dedicated components for thermal management.

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

3Speed

If turbine size is reduced to decrease lag, then transient response is improved, but mass flow capacity at high engine speed decreases

Engineering Contradiction:
Improveturbo response speedVSAvoidexhaust mass flow capacity
Core Design Contradiction:
SpeedVSQuantity of substance

Solution Approach 1:

The turbine system is segmented into two independent turbine stages (HP and LP turbines) with different size characteristics. The HP turbine can be optimized for low-inertia fast response, while the LP turbine provides additional flow capacity at high engine speeds. This segmentation allows each turbine to be sized appropriately for its operating range.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system dynamically switches between different turbine configurations using the bypass valve assembly. At low speeds, exhaust flows through both turbines for maximum boost. At high speeds, the bypass valve can open to divert excess exhaust flow, preventing turbine overload and maintaining optimal operating conditions while preserving the ability of smaller turbines to respond quickly.

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

Facilitates immediate catalyst light-off at engine startup, reduces thermal losses, and is cost-effective and space-efficient by ensuring high exhaust gas temperature reaches the catalyst, while maintaining boost performance through controlled valve operation.

Implementation Method 1

bypassing the HP and LP turbines with the result that the exhaust gas temperature is maintained at a level sufficient to achieve immediate light-off of the catalyst

Methodology Applied
Scientific EffectThermal energy conservation:

Implementation Method 2

catalytic aftertreatments can be used to meet emission standards. The pollutant-converting catalysts typically require a minimum temperature to start up and work effectively

Methodology Applied
Scientific EffectCatalysis: Catalysis

Data Source

PatentEP2271832B1Multi-stage turbocharging system with thermal bypass
Publication Date: 2015.11.04 BORGWARNER INC
  • EP2271832B1 patent drawingFigure 1
  • EP2271832B1 patent drawingFigure 2
  • EP2271832B1 patent drawingFigure 3

AI summary

A two-stage turbocharging system with a high pressure (HP) turbine and a low pressure (LP) turbine, the HP turbine having an inlet and an outlet and the LP turbine having an inlet and an outlet, as well as E-HP exhaust piping adapted for fluidly connecting an engine to said HP turbine inlet, HP-LP exhaust piping fluidly connecting said HP turbine outlet to said LP turbine inlet, LP-A exhaust piping fluidly connecting said LP turbine outlet to an aftertreatment device, and branched bypass piping having an inlet and first and second branches, each branch having an outlet, with the inlet being fluidly connected to the E-HP exhaust piping, with the first branch outlet being fluidity connected to the LP turbine inlet, with the second branch outlet being fluidly connected to the aftertreatment device, and with an R2S valve in said first branch and a warm-up valve in said second branch. By opening of the valve, exhaust gas can bypass both the HP and LP turbines and flow to the catalytic converter. In a preferred embodiment of the invention, the R2S valve and the warm-up valve are integrated into a single exhaust flow control unit.