Integrated Charge Gas Compression Train for Ethylene Without Gearbox

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Solution Overview

Problem

Current ethylene charge gas compression trains are bulky, costly, and unreliable due to the presence of a gearbox and separate casings for low-pressure and high-pressure compressors, which increases the footprint and maintenance needs.

Innovation Solution

Directly coupling a steam turbine to a group of low-pressure compressors and integrating them in a common casing, eliminating the need for a gearbox and reducing the overall size and complexity of the compression train.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Speed

If a gearbox is used to couple the steam turbine to the compressors, then the rotation speed can be increased to 5000 RPM, but the device complexity and footprint increase

Engineering Contradiction:
Improverotation speedVSAvoidcomplexity
Core Design Contradiction:
SpeedVSDevice complexity

Solution Approach 1:

The patent removes the gearbox from the system entirely, directly coupling the steam turbine to the compressors. This extraction of the intermediate mechanical transmission component eliminates the associated complexity, maintenance needs, and space requirements while the turbine itself operates at the required high rotation speed to drive the compressors directly

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The patent merges the steam turbine and compressors into a single integrated assembly where the turbine shaft is directly connected to the compressor shafts. This direct coupling eliminates the need for separate gearbox housing, mounting structures, and alignment mechanisms, thereby reducing device complexity and footprint

Inventive Principle:
Principle #5Merging (Combining)

2Adaptability or versatility

If separate casings are used for low-pressure and high-pressure compressors, then each compressor can be optimized independently, but the footprint and device complexity increase

Engineering Contradiction:
ImproveoptimizationVSAvoidfootprint
Core Design Contradiction:
Adaptability or versatilityVSArea of stationary object

Solution Approach 1:

The patent combines multiple compressor stages (both low-pressure and high-pressure compressors) into a single common casing. The compressors are arranged radially or axially around a shared drive mechanism, allowing them to share common structural support, sealing systems, and maintenance access points. This integration reduces the overall footprint by eliminating redundant casing walls, mounting flanges, and alignment features that would be required for separate casings

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The common casing serves multiple functions simultaneously: it houses both low-pressure and high-pressure compressors, provides structural support for all rotating elements, contains the sealing systems for multiple compression stages, and facilitates unified maintenance access. This multi-functionality reduces the total component count and space requirements compared to separate dedicated casings for each compressor

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

3Power

If a gearbox is used in the compression train, then power transmission is achieved, but reliability decreases due to additional failure points

Engineering Contradiction:
Improvepower transmissionVSAvoidreliability
Core Design Contradiction:
PowerVSReliability

Solution Approach 1:

The patent eliminates the gearbox from the power transmission system, creating a direct-drive configuration where the steam turbine shaft is mechanically coupled directly to the compressor shafts. This removal of the gearbox eliminates gear teeth, bearings, lubrication systems, and coupling mechanisms that are potential failure points, thereby significantly improving system reliability while maintaining full power transmission capability through direct mechanical connection

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The patent merges the power transmission function directly into the rotational coupling between the turbine and compressors. The turbine shaft and compressor shafts are aligned and connected through a common bearing support structure, eliminating the need for intermediate power transmission components. This integrated power transmission path reduces the number of moving parts and potential failure modes while maintaining efficient torque and power delivery

Inventive Principle:
Principle #5Merging (Combining)

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 reliability, reduces costs, and minimizes space usage while maintaining efficient compression performance, achieving higher rotating speeds and pressures without the need for a gearbox, thus improving the overall system reliability and efficiency.

Implementation Method 1

a steam turbine (2), a first compressor (60), a second compressor (61) and a third compressor (62) arranged on the same shaft line

Methodology Applied
Scientific EffectSteam turbine: Turbine

Implementation Method 2

The first compressor (60) receives an input gas flow at a first input pressure (e.g., 1.5-2 bar) and outputs a first output flow at a first output pressure (e.g., 2.5-4 bar)

Methodology Applied
Scientific EffectCompression: Compression

Data Source

PatentUS10724439B2Charge gas compression train for ethylene
Publication Date: 2020.07.28 NUOVO PIGNONE SPA
  • US10724439B2 patent drawing

AI summary

A charge gas compression train for ethylene including a first compressor including a first group of compression stages, a second group of compression stages, and a third group of compression stages. The first group of compression stages includes an outlet configured to be connected to a first intercooler inlet. The second group of compression stages includes a second compressor inlet configured to be connected to a first intercooler outlet, and a second compressor outlet configured to be connected to a second intercooler inlet. The third group of compression stages includes a third compressor inlet configured to be connected to a second intercooler outlet. The first, the second, and the third group of compression stages are integrated in a first common casing and operate at the same rotation speed. The first compressor includes a plurality of unshrouded and shrouded impellers, where an unshrouded impeller is positioned upstream to a shrouded impeller.