Turbocharger Turbine Flow Cross-Section Control for Torque Response
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Solution Overview
Problem
Internal combustion engines experience boost pressure overshoots and delayed torque response during non-stationary operating states due to limitations in existing boost pressure regulators, which affect drivability and torque build-up.
Innovation Solution
A control unit that determines the lower limit of the turbine flow cross-section as a function of engine speed to optimize boost pressure and torque increase, avoiding excessive scavenging gradients and allowing rapid torque build-up without additional sensors.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Stability of the object's composition
If the turbine flow cross-section is limited at the bottom to avoid boost pressure overshoot, then boost pressure stability is improved, but torque build-up speed deteriorates
Solution Approach 1:
The patent applies dynamics by making the turbine flow cross-section adjustable and variable during operation. The control unit dynamically adapts the turbine flow cross-section based on operating conditions (stationary vs. non-stationary states), allowing the system to optimize between stability and response speed depending on the current operational context.
Solution Approach 2:
The patent changes the parameter of turbine flow cross-section to resolve the contradiction. By adjusting this parameter differently in stationary states (to prevent overshoot) versus non-stationary states (to enable rapid torque build-up), the system achieves both stability when needed and rapid response when required.
2Manufacturing precision
If the regulator manipulated variable is limited to reduce overshooting, then boost pressure control precision is improved, but torque response delay increases
Solution Approach 1:
The control unit dynamically adjusts the turbine flow cross-section based on whether the system is in a stationary or non-stationary state. During transient conditions, the system prioritizes rapid torque response over precise boost pressure control, temporarily allowing larger deviations to achieve faster response.
Solution Approach 2:
The control unit anticipates the need for rapid torque build-up in non-stationary states and pre-adjusts the turbine flow cross-section accordingly, rather than waiting for the overshoot to occur and then correcting it.
3Power
If exhaust gas energy is maximally transmitted to the turbine wheel, then turbine power is improved, but scavenging gradient increases causing charge pressure delay
Solution Approach 1:
The patent changes the turbine flow cross-section parameter to balance turbine power generation with scavenging gradient control. By adjusting this parameter, the system optimizes the trade-off between extracting energy from exhaust gases and maintaining adequate charge pressure for rapid torque build-up.
Data Source
AI summary
A turbine flow cross-section of a turbocharger of an internal combustion engine, is set such that a lower limit (TSQ_dyn_min) of a range of settable values of the turbine flow cross-section is determined as a function of an operating parameter of the internal combustion engine in non-stationary operating states. A speed of the internal combustion engine can be used as the operating parameter.


