Centrifugal compressor part load control algorithm for improved performance

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Centrifugal compressors face challenges in maintaining flow stabilization and efficiency across a wide range of volumetric flow rates, particularly at part load, due to narrow operating ranges and high surge margins, which lead to instability, noise, and reduced performance.

Innovation Solution

A compressor system with adjustable guide vanes and a variable geometry diffuser, controlled by a predetermined algorithm that adjusts diffuser positions based on actual lift and guide vane positions to optimize performance and efficiency at both full and part loads, while monitoring for surge conditions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If variable diffusers are adjusted according to a fixed relationship between inlet guide vane and diffuser to achieve highest surge margin, then surge margin is improved, but efficiency at part load deteriorates

Engineering Contradiction:
Improvesurge marginVSAvoidefficiency at part load
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The patent implements dynamic adjustment of diffuser vane position based on real-time operating conditions (suction pressure, discharge pressure, motor current) rather than a fixed relationship. The microprocessor continuously calculates optimal diffuser position using surge margin equations and adjusts vanes dynamically to maintain both high surge margin and efficiency across varying load conditions.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system changes the control parameter from a fixed geometric relationship to a dynamic parameter based on pressure differential and motor current. The diffuser vane position is adjusted as a function of operating parameters (suction pressure, discharge pressure, current) to optimize both surge margin and efficiency at different load points.

Inventive Principle:
Principle #35Parameter changes

2Productivity

If compressor is designed for maximum volumetric flow rate, then full load performance is improved, but flow stability at low volumetric flow rates deteriorates

Engineering Contradiction:
Improvefull load performanceVSAvoidflow stability at low flow rates
Core Design Contradiction:
ProductivityVSStability of the object's composition

Solution Approach 1:

The diffuser vane position is dynamically adjusted based on actual operating conditions rather than being fixed for maximum flow. At low flow rates, the system automatically positions diffuser vanes to maintain stable flow patterns, preventing reversal and surge while preserving the compressor's full load capability.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system uses feedback from pressure sensors and current measurements to continuously monitor operating conditions and adjust diffuser vane position accordingly. This closed-loop control ensures flow stability at low rates while maintaining full load performance through real-time adaptation.

Inventive Principle:
Principle #23Feedback

Data Source

PatentUS10544801B2Centrifugal compressor part load control algorithm for improved performance
Publication Date: 2020.01.28 CARRIER CORP
  • US10544801B2 patent drawing
  • US10544801B2 patent drawing
  • US10544801B2 patent drawing

AI summary

A compressor system having a centrifugal compressor, controller and an interface is disclosed. The compressor includes adjustable guide vanes and a variable geometry diffuser. The controller is in electrical communication with each of the guide vanes and diffuser so as to monitor and adjust positions thereof in accordance with a predetermined control algorithm. The control algorithm is implemented in accordance with a method of controlling the centrifugal compressor. The method adjusts the position of the diffuser based on the actual lift, guide vane position and predetermined relationships between diffuser position and reference lift.