Engine Bypass Valve Compressor Surge Control

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Solution Overview

Problem

Turbochargers experience surge events due to excessive pressure in the charged air piping, leading to compressor wheel degradation and inefficient operation, particularly during rapid engine unloading conditions.

Innovation Solution

An engine bypass system with a bypass valve that redirects compressed intake air from the compressor outlet to the turbine inlet or exhaust passage, controlling flow to maintain compressor operation within a designated efficiency region and prevent surge.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Power

If the turbocharger operates during rapid unloading events, then power output is maintained, but compressor surge occurs causing degradation

Engineering Contradiction:
Improvepower outputVSAvoidcompressor durability
Core Design Contradiction:
PowerVSReliability

Solution Approach 1:

The engine bypass valve acts as an intermediary component that provides an alternative flow path for compressed air during rapid unloading events. When surge conditions are detected, the bypass valve opens to redirect air away from the compressor outlet, preventing the harmful backflow and surge phenomenon while allowing the turbocharger to continue operating and maintaining power output.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If compressed air is redirected through the bypass passage, then compressor surge is prevented, but system complexity increases

Engineering Contradiction:
Improvecompressor operation stabilityVSAvoidbypass system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The bypass valve and bypass passage are extracted as separate, dedicated components from the main turbocharger assembly. This modular extraction allows the bypass system to be independently designed, installed, and maintained, reducing overall system complexity while providing effective surge prevention. The bypass components can be added to existing turbocharger systems without requiring fundamental redesign.

Inventive Principle:
Principle #2Taking out (Extraction)

3Reliability

If the bypass valve is opened to prevent surge, then compressor operation is protected, but compressed air is wasted

Engineering Contradiction:
Improvecompressor protectionVSAvoidcompressed air waste
Core Design Contradiction:
ReliabilityVSLoss of energy

Solution Approach 1:

The system converts the potentially harmful surge condition into a beneficial control opportunity. By monitoring compressor operation parameters and detecting surge tendencies, the system proactively opens the bypass valve to redirect compressed air, transforming what would be a destructive surge event into a controlled bypass flow that protects the compressor. The compressed air that would have caused surge is instead usefully redirected through the bypass passage to the exhaust or intake manifold.

Inventive Principle:
Principle #22Blessing in disguise (Convert harm into benefit)

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

The engine bypass system effectively prevents compressor surge, maintains compressor efficiency, and reduces peak cylinder pressure, thereby extending turbocharger lifespan and improving engine performance.

Implementation Method 1

an engine bypass valve to control flow through the engine bypass passage

Methodology Applied
Scientific EffectFluid flow control:

Implementation Method 2

Turbochargers function by compressing intake air in a compressor driven by a turbine operated by exhaust gas flow

Methodology Applied
Scientific EffectCompression: Compression

Implementation Method 3

a turbine positioned in an exhaust passage and a compressor positioned in an intake passage

Methodology Applied
Scientific EffectTurbine expansion: Turbine

Data Source

PatentUS10428729B2Systems and method for an engine bypass valve
Publication Date: 2019.10.01 TRANSPORTATION IP HOLDINGS LLC
  • US10428729B2 patent drawing
  • US10428729B2 patent drawing
  • US10428729B2 patent drawing

AI summary

Various systems and methods are provided for controlling operation of a turbocharger compressor. In one example, a system includes a turbocharger including a turbine positioned in an exhaust passage and a compressor positioned in an intake passage, an engine bypass passage having an inlet fluidically coupled to an outlet of the compressor and an outlet fluidically coupled to an inlet of the turbine, an engine bypass valve to control flow through the engine bypass passage, and a controller configured to adjust a position of the engine bypass valve to maintain compressor operation within a designated compressor efficiency region.