Turbocharger Bypass Valve Deflector for Thermal Shock Mitigation

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Solution Overview

Problem

The existing closure flaps in bypass ducts of turbocharger turbines are prone to cracking due to thermal shocks, which affects the optimal operation and longevity of the engine, especially when the flap opening is between 2mm to 5mm, leading to suboptimal gas flow direction and potential pressure losses.

Innovation Solution

A closure flap with a deflector on its contact surface, featuring a chamfer or concave rounded corner, is designed to reduce gas flow speed and guide gases more diffusely, minimizing the risk of cracking and maintaining optimal gas distribution, while the deflector extends radially to the valve body in the closed configuration, enhancing the sealing and resistance force.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If the closure flap is opened with a gap of 2mm to 5mm to maintain optimal flow distribution, then engine performance is optimized, but thermal shocks cause cracks to appear in the flap

Engineering Contradiction:
Improveengine performanceVSAvoidflap integrity
Core Design Contradiction:
ProductivityVSReliability

Solution Approach 1:

A deflector element is introduced as an intermediary component between the closure flap and the hot gas flow. This deflector absorbs and redirects the thermal shock and mechanical stress away from the flap, allowing the flap to remain open with a 2-5mm gap for optimal performance while protecting it from cracking caused by thermal shocks

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The deflector is positioned upstream to preemptively intercept and redirect the hot gas flow before it can directly impact the closure flap. This preliminary action prevents the thermal shocks from reaching the flap, eliminating the cracking issue while maintaining the optimal opening gap for engine performance

Inventive Principle:
Principle #10Preliminary action

2Volume of moving object

If the side wall is positioned closer to the inlet chamber to reduce dimensioning constraints, then engine compactness is improved, but gases strike the side wall causing blowtorch effect and potential cracking

Engineering Contradiction:
Improveinlet chamber volumeVSAvoidblowtorch effect
Core Design Contradiction:
Volume of moving objectVSObject-affected harmful factors

Solution Approach 1:

The deflector serves as a mediator between the hot gas flow and the side wall of the inlet chamber. It redirects the gas flow away from the side wall, preventing the blowtorch effect while allowing the side wall to be positioned closer to the inlet chamber, thus reducing the overall engine volume

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The deflector extracts or removes the harmful direct impingement of hot gases on the side wall by redirecting the flow path. This allows the side wall to be repositioned closer to the inlet chamber without exposing it to thermal shock, achieving both compactness and protection from the blowtorch effect

Inventive Principle:
Principle #2Taking out (Extraction)

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 solution effectively reduces the occurrence of cracks and maintains an ideal gas distribution, ensuring optimal engine performance and torque without significant pressure losses, even at varying engine speeds.

Implementation Method 1

A closure flap with a deflector on its contact surface, featuring a chamfer or concave rounded corner, is designed to reduce gas flow speed and guide gases more diffusely

Methodology Applied
Scientific EffectFlow redirection and diffusion:

Data Source

PatentEP2767695B1Valve of a bypass line of a turbocompressor provided with a shutter with deflector
Publication Date: 2017.04.19 RENAULT SA
  • EP2767695B1 patent drawingFigure 1~2
  • EP2767695B1 patent drawingFigure 3~4
  • EP2767695B1 patent drawingFigure 5~6

AI summary

The valve (2) has a cylindrical valve body (4) projecting into an opening of an inlet wall of a gas inlet chamber, and having an oblique opening (5). A closure flap (1) includes a contact surface (3) intended to cooperate with the valve body, so ??as to close the oblique opening of the valve body in a closed configuration of the valve. The closure flap includes a deflector (6) arranged on a portion of an outer periphery of the contact surface, where the deflector is formed by a chamfer including a rectilinear segment having a dimension equal to 2 mm. An independent claim is also included for a power unit of a car.