Radial Compressor Diffuser With Asymmetric Guide Vanes
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Solution Overview
Problem
Modern turbochargers face resonance vibrations due to the geometrically regular design of compressor rotors and diffuser guide vanes, leading to mechanical damage from high cycle fatigue, as they attempt to balance aerodynamic performance, mechanical utilization, and noise generation.
Innovation Solution
The diffuser guide vanes are positioned with varying angular distances relative to an asymmetrically designed spiral casing, allowing for irregular distribution and alignment with the spiral housing to minimize resonance vibrations.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Ease of manufacture
If the diffuser guide vanes are arranged with regular angular spacing to simplify manufacturing and maintain geometric symmetry, then manufacturing precision and ease of manufacture are improved, but resonance vibrations occur due to excitation of natural modes by the pressure potential field, worsening reliability and mechanical strength
Solution Approach 1:
The patent applies asymmetry by deliberately arranging diffuser guide vanes with non-uniform angular spacing around the circumference. This asymmetric configuration breaks the geometric symmetry that causes resonant vibrations, thereby reducing the excitation of natural modes in the compressor impeller blades while maintaining manufacturing feasibility through precise but varied positioning.
Solution Approach 2:
The patent implements local quality by varying the angular spacing of individual guide vanes according to specific design criteria. Rather than applying a uniform spacing pattern, each guide vane pair is positioned with locally optimized angular distances to minimize resonance vibrations in critical areas while maintaining overall flow symmetry.
2Reliability
If the diffuser guide vanes are arranged with irregular angular spacing to reduce resonance vibrations and improve reliability, then reliability and mechanical strength are improved, but manufacturing precision requirements increase and ease of manufacture deteriorates
Solution Approach 1:
The patent applies asymmetry by deliberately arranging diffuser guide vanes with non-uniform angular spacing around the circumference. This asymmetric configuration breaks the geometric symmetry that causes resonant vibrations, thereby reducing the excitation of natural modes in the compressor impeller blades while maintaining manufacturing feasibility through precise but varied positioning.
3Productivity
If the compressor impeller blades are designed with long, thin geometry to increase specific air flow capacity, then productivity is improved, but the natural modes occur at low frequencies and are easily excited into vibration, worsening reliability and mechanical strength
Solution Approach 1:
The patent converts the harmful resonant vibration problem into a beneficial solution by using the pressure potential field from asymmetrically spaced guide vanes to actively reduce vibrations. The asymmetric arrangement creates a pressure distribution that counteracts the excitation of natural modes in the long, thin impeller blades, transforming the potential harm of blade geometry into a controlled vibration reduction mechanism.
Data Source
Figure 1~4
Figure 2~3
AI summary
Since the angular intervals between two guide vanes (21), which are arranged adjacent, in the diffuser vary along the circumference, the resonant oscillation of the compressor can be reduced.