Wave Spring Biasing in Variable Turbine Geometry Assemblies
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Solution Overview
Problem
Variable turbine geometry assemblies in turbochargers suffer from repeated wear due to vibrations, leading to increased noise, vibrations, and harshness (NVH), as well as functional failures in controlling exhaust gas flow.
Innovation Solution
Incorporation of a wave spring that biases the adjustment ring and vane lever, reducing vibration and wear between components, thereby minimizing noise, vibrations, and harshness, and enhancing the durability and effectiveness of the variable turbine geometry assembly.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Productivity
If a variable turbine geometry assembly is used to control exhaust gas flow, then the turbocharger can efficiently control air intake, but repeated vibrations cause wear on components leading to increased noise and potential failure
Solution Approach 1:
A wave spring is introduced between the adjustment ring and vane lever to cushion vibrations before they cause wear. The wave spring absorbs and dampens vibrational energy, preventing the repeated contact stresses that would otherwise degrade component reliability over time.
Solution Approach 2:
The wave spring acts as an intermediary element between the adjustment ring and vane lever. This intermediate component isolates the two parts from direct vibrational contact, reducing the transmission of harmful vibrations while maintaining the mechanical connection necessary for flow control.
2Productivity
If variable turbine geometry components are subjected to vibrations, then exhaust gas flow can be controlled, but wear increases leading to increased noise and harshness
Solution Approach 1:
The wave spring is positioned to cushion vibrations before they propagate through the variable turbine geometry assembly. By dampening vibrational energy at its source, the wave spring prevents the increased noise and harshness that would otherwise result from repeated component wear.
Solution Approach 2:
The wave spring serves as a vibrational intermediary that breaks the transmission path of harmful vibrations. This intermediate element isolates the adjustment ring and vane lever from direct vibrational coupling, significantly reducing the noise and harshness generated by the assembly.
3Ease of operation
If repeated wear occurs on variable turbine geometry components, then vibrations increase, but this leads to functional failure of exhaust gas flow control
Solution Approach 1:
The wave spring provides beforehand cushioning by continuously dampening vibrations during operation. This prevents the progressive wear that would otherwise occur from repeated vibrational stress, ensuring the flow control functionality remains reliable over extended operation.
Solution Approach 2:
The wave spring intermediary protects the critical flow control components from direct vibrational damage. By isolating the adjustment ring and vane lever through this intermediate element, the system maintains its flow control functionality while reducing the vibrational stress that would lead to failure.
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 wave spring configuration effectively reduces wear and noise, lowers the likelihood of functional failure, and provides a simple, cost-effective solution for maintaining efficient exhaust gas flow control in turbochargers.
Implementation Method 1
a wave spring operably in contact with at least one of the at least one vane lever and the adjustment ring. The wave spring is configured to bias one of the at least one vane lever and the adjustment ring toward the other of the at least one vane lever and the adjustment ring
Data Source
AI summary
A variable turbine geometry assembly for controlling flow of exhaust gas to a turbine wheel of a turbocharger includes an adjustment ring extending about an axis and rotatable about the axis, at least one vane lever coupled to the adjustment ring, and at least one vane coupled to the at least one vane lever. The at least one vane is moveable with respect to the adjustment ring when the adjustment ring rotates about the axis. The variable turbine geometry assembly further includes a wave spring operably in contact with at least one of the at least one vane lever and the adjustment ring. The wave spring is configured to bias one of the at least one vane lever and the adjustment ring toward the other of the at least one vane lever and the adjustment ring.


