Multistage Centrifugal Compressor With Mixed-Flow Stage Matching

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Solution Overview

Problem

Centrifugal chillers in refrigeration systems face inefficiencies due to suboptimal design of compressor stages, leading to energy consumption and maintenance challenges, particularly in high-capacity applications where prior systems neglect cumulative benefits of fluid control across stages.

Innovation Solution

A multistage centrifugal compressor assembly with mixed flow impellers and a variable speed drive, featuring a final stage compressor and a non-final stage compressor, where each stage has a mixed flow impeller with constant relative diffusion, optimized for specific speed ranges to achieve efficient operation across a wide capacity range, and a vaneless diffuser with a wall profile matching the impeller hub and shroud, allowing for efficient fluid compression and reduced physical size.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If prior multistage compressor systems are designed with each stage optimized independently, then each stage can perform optimally for its specific conditions, but the cumulative benefits of fluid control across stages are neglected leading to overall system inefficiency

Engineering Contradiction:
Improveoverall system efficiencyVSAvoidfluid control integration
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The patent merges the fluid control functions across multiple compressor stages into an integrated system. The diffuser of a upstream stage is designed to work in conjunction with the impeller of the downstream stage, creating a unified fluid control pathway that optimizes overall system efficiency rather than individual stage performance.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The compressor stages are designed with universal fluid control characteristics where the diffuser structure serves multiple functions: it completes the fluid acceleration from the upstream impeller and prepares the fluid for the downstream impeller. This multi-functional design enables cumulative efficiency benefits across all stages.

Inventive Principle:
Principle #6Universality (Multi-functionality)

2Productivity

If the first stage of a multistage compressor is sized to perform optimally, then the first stage achieves maximum efficiency, but the second (or later) stage is allowed to perform less than optimally

Engineering Contradiction:
Improvestage efficiencyVSAvoidstage matching
Core Design Contradiction:
ProductivityVSAdaptability or versatility

Solution Approach 1:

Each compressor stage is designed with localized quality optimizations tailored to its specific position in the multistage system. The first stage impeller and diffuser are optimized for initial compression conditions, while subsequent stages are optimized for the specific fluid conditions resulting from previous stages, ensuring each stage operates at peak efficiency for its local conditions.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The patent employs parameter changes across stages, where the diffuser outlet parameters (velocity, pressure distribution) of one stage are specifically designed to match the impeller inlet parameters of the next stage. This parameter matching ensures optimal performance at each stage while maintaining cumulative system efficiency.

Inventive Principle:
Principle #35Parameter changes

3Productivity

If centrifugal chillers operate at high capacity, then they meet high cooling demand, but they consume significant energy resources

Engineering Contradiction:
Improvecooling capacityVSAvoidenergy consumption
Core Design Contradiction:
ProductivityVSUse of energy by moving object

Solution Approach 1:

The patent replaces traditional mechanical optimization approaches with a fluid dynamics-based design system. By using computational fluid dynamics and optimized impeller-diffuser geometries, the system achieves higher efficiency at high capacity without relying on mechanical adjustments or additional components that would increase energy consumption.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

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 results in high-performance, efficient operation with constant efficiency across varying capacities, reduced energy consumption, smaller size, lower noise levels, and cost savings by enabling fewer compressors to meet the same capacity requirements, while maintaining reliability and scalability.

Implementation Method 1

Centrifugal compression involves the purely rotational motion of only a few mechanical parts

Methodology Applied
Scientific EffectCentrifugal force: Centrifugal Force

Implementation Method 2

The impeller accelerates the fluid and in turn, increases the kinetic energy of the fluid

Methodology Applied
Scientific EffectKinetic energy conversion:

Implementation Method 3

a vaneless diffuser with a wall profile matching the impeller hub and shroud

Methodology Applied
Scientific EffectDiffusion: Diffusion

Implementation Method 4

The diffuser is designed to follow the impeller hub and shroud meridional profile

Methodology Applied
Scientific EffectKinetic energy to pressure conversion:

Implementation Method 5

a variable speed drive, featuring a final stage compressor and a non-final stage compressor

Methodology Applied
Scientific EffectVariable speed control:

Implementation Method 6

a permanent magnet motor controlled by a variable speed drive

Methodology Applied
Scientific EffectElectromagnetic induction: Electromagnetic Induction

Data Source

PatentUS7856834B2Centrifugal compressor assembly and method
Publication Date: 2010.12.28 TRANE INTERNATIONAL INC
  • US7856834B2 patent drawing
  • US7856834B2 patent drawing
  • US7856834B2 patent drawing

AI summary

A centrifugal compressor assembly for compressing refrigerant in a 250-ton capacity or larger chiller system comprising a motor, preferably a compact, high energy density motor or permanent magnet motor, for driving a shaft at a range of sustained operating speeds under the control of a variable speed drive. Another embodiment of the centrifugal compressor assembly comprises a mixed flow impeller and a vaneless diffuser sized such that a final stage compressor operates with an optimal specific speed range for targeted combinations of head and capacity, while a non-final stage compressor operates above the optimum specific speed of the final stage compressor. Another embodiment of the centrifugal compressor assembly comprises an integrated inlet flow conditioning assembly comprising a flow conditioning nose, a plurality of inlet guide vanes and a flow conditioning body that positions inlet guide vanes to condition flow of refrigerant into an impeller to achieve a target approximately constant angle swirl distribution with minimal guide vane turning.