Multi-stage Centrifugal Compressor Drain Flow Path Design

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Solution Overview

Problem

In multi-stage centrifugal compressors, the alignment of drain pipes, suction nozzles, and ejection nozzles can cause interference, leading to increased vibration due to the need for a longer rotor shaft and reduced natural frequency, which may result in resonance during operation.

Innovation Solution

A multi-stage centrifugal compressor design that includes a rotor with impellers in multiple stages, diaphragms with guide flow paths and communication holes, and an axial flow path connecting these holes to form a drain flow path between the suction and ejection nozzles, allowing for fluid discharge without extending the rotor main body, thus avoiding interference between the nozzles.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If drain pipes, suction nozzle, and ejection nozzle are aligned in the axial direction below the casing, then the structure is compact, but interference occurs between these components

Engineering Contradiction:
Improvestructural compactnessVSAvoidcomponent interference
Core Design Contradiction:
Device complexityVSObject-generated harmful factors

Solution Approach 1:

The patent introduces a radial dimension for the drain flow path by forming communication holes through the diaphragm in the radial direction, rather than aligning all components in the axial direction. This dimensional change allows the drain pipe to exit radially from the casing, avoiding interference with the axially-aligned suction and ejection nozzles while maintaining structural compactness

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

2Object-generated harmful factors

If the rotation shaft is lengthened in the axial direction to avoid interference, then component interference is avoided, but the natural frequency of the rotation shaft decreases

Engineering Contradiction:
Improvecomponent interferenceVSAvoidnatural frequency
Core Design Contradiction:
Object-generated harmful factorsVSReliability

Solution Approach 1:

Instead of extending the rotation shaft axially to avoid interference, the patent uses a radial drain flow path that exits through the casing wall. This approach avoids the need for axial extension entirely, thereby maintaining the rotation shaft's natural frequency away from operational resonant frequencies while still achieving component separation

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

3Object-generated harmful factors

If the rotation shaft is lengthened to increase the interval among drain pipes and nozzles, then interference is avoided, but resonation is likely to occur

Engineering Contradiction:
Improvecomponent interferenceVSAvoidvibration and resonance
Core Design Contradiction:
Object-generated harmful factorsVSObject-affected harmful factors

Solution Approach 1:

The patent resolves the interference problem by changing the drain pipe's exit direction from axial to radial. This allows sufficient spacing between all components without extending the rotation shaft axially, thereby avoiding the reduction of natural frequency and preventing resonation and vibration during operation

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

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 design enables the formation of a drain flow path that does not interfere with the suction and ejection nozzles, preventing vibration and resonance by maintaining the rotor's natural frequency away from the rotational frequency, while allowing for efficient fluid discharge without lengthening the rotor main body.

Implementation Method 1

the centrifugal compressor compresses the working fluid in a gas state by utilizing a centrifugal force generated when the impeller rotates

Methodology Applied
Scientific EffectCentrifugal force: Centrifugal Force

Data Source

PatentUS10851803B2Multi-stage centrifugal compressor
Publication Date: 2020.12.01 MITSUBISHI HEAVY INDUSTIES COMPRESSOR CORP
  • US10851803B2 patent drawing
  • US10851803B2 patent drawing
  • US10851803B2 patent drawing

AI summary

A multi-stage centrifugal compressor includes: a rotor including a plurality of impellers disposed in a plurality of stages in an axial direction; a plurality of diaphragms each including a guide flow path that guides a fluid discharged radially outward from one of the impellers to an adjacent impeller on the following stage, and a communication hole extended from a bottom portion of the guide flow path; a casing that accommodates the plurality of diaphragms therein; and an axial flow path that connects the plurality of communication holes to each other. The casing includes a drain flow path disposed only between the communication hole that is the closest to a suction nozzle and the communication hole that is the closest to an ejection nozzle.