Centrifugal Compressor Impeller Flow Splitter Segments
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Solution Overview
Problem
Centrifugal compressor impeller designs face challenges in balancing efficiency and vibration, particularly in open impellers where leakage and potential damage from impeller-to-shroud contact are concerns, and in achieving optimal blade geometry for various applications.
Innovation Solution
The design incorporates a centrifugal compressor impeller with a hub and blades, featuring flow splitter segments that extend between blades and are spaced from the hub and blade tips, allowing for a unitary monolithic casting or separate formation of rings and blades from different alloys, which split the flow and reduce resonant behavior, enabling thinner vanes and higher speed operation.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Ease of manufacture
If open impeller design is used, then ease of manufacture and blade geometry tailoring are improved, but leakage losses and risk of impeller-to-shroud contact increase
Solution Approach 1:
A fluid seal ring is introduced as an intermediary component between the open impeller and the shroud. This seal ring creates a barrier that reduces gas leakage from the high-pressure discharge side back to the suction side, thereby reducing leakage losses while maintaining the open impeller design's manufacturing advantages and geometry flexibility.
2Ease of manufacture
If open impeller design is used, then ease of manufacture and blade geometry tailoring are improved, but risk of impeller-to-shroud contact increases
Solution Approach 1:
The fluid seal ring serves as a protective intermediary that maintains a controlled gap between the impeller and shroud. This prevents direct contact between components, reducing the risk of mechanical damage while allowing the open impeller design to retain its manufacturing simplicity and geometric adaptability.
3Stability of the object's composition
If shrouded impeller is used, then vibration resistance is improved, but manufacturing complexity and cost increase
Solution Approach 1:
The shroud structure is segmented into a fixed shroud and a movable fluid seal ring. The fixed shroud provides the structural framework for vibration resistance, while the separate fluid seal ring can be independently optimized and replaced. This segmentation allows the system to achieve vibration resistance without the full manufacturing complexity of a completely integrated shrouded impeller.
4Strength
If thicker vane structure is used in open impeller, then strength is improved, but efficiency decreases due to increased leakage
Solution Approach 1:
The fluid seal ring acts as a mediator that decouples the relationship between vane thickness and leakage. By providing a sealing barrier near the shroud, the system can use thinner, more efficient vane structures without suffering excessive leakage losses, as the seal ring compensates for the increased clearance associated with thinner vanes.
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
This configuration enhances efficiency, allows for lighter and more efficient vanes, enables higher speed operation, and improves service life by reducing vibration and allowing for tailored blade geometry and manufacturing flexibility.
Implementation Method 1
flow splitter segments that extend between blades and are spaced from the hub and blade tips, allowing for a unitary monolithic casting or separate formation of rings and blades from different alloys, which split the flow and reduce resonant behavior
Data Source
AI summary
A centrifugal compressor impeller (60; 160) has a hub (62; 162) having a gaspath surface (64; 164) extending from a leading end to a trailing end. A plurality of blades (70A, 70B; 170) extend from the hub gaspath surface and each have: a leading edge (72A, 72B; 172); a trailing edge (74A, 74B; 174); a first face (80A, 80B; 180); a second face (82A, 82B; 182); and a tip (78A, 78B; 178). A plurality of flow splitter segments (120, 122; 320, 322) extend between associated twos of the blades and each spaced from both the hub gaspath surface and the tips of the associated two blades.


