Integrated Compressor Seal Assembly With Reduced Hardware

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Solution Overview

Problem

Centrifugal compressors have hardware components that increase costs, installation complexity, and maintenance challenges, particularly in high-speed and high-pressure applications.

Innovation Solution

The design includes a rotor assembly with multiple lubricant paths and non-planar bearing retainers that allow for adjustable axial positions, and an integral flow control valve in the heat exchanger to reduce hardware and improve assembly and maintenance, with gas and oil seals installed without additional hardware.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If traditional hardware components are used in centrifugal compressors, then sealing and support functions are provided, but device complexity and installation maintenance difficulty increase

Engineering Contradiction:
Improvesealing functionVSAvoidhardware components
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The gas seal and oil seal are merged into a single integrated seal assembly that fits within the rotor assembly bore. The bearing retainers are also integrated to provide both support and retention functions. This consolidation reduces the number of separate hardware components while maintaining all necessary sealing and support functions.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The bearing retainers serve multiple functions: they support the rotor assembly, retain the seals in position, and provide structural support within the gearbox. The integrated seal assembly provides both gas sealing and oil sealing functions simultaneously. This multi-functionality eliminates the need for separate dedicated components for each function.

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

2Temperature

If multiple separate lubricant paths are implemented, then bearing cooling is improved, but device complexity increases

Engineering Contradiction:
Improvelubricant temperatureVSAvoidlubricant path configuration
Core Design Contradiction:
TemperatureVSDevice complexity

Solution Approach 1:

The lubricant delivery system is segmented into multiple separate paths that deliver lubricant to different locations within the bearing assembly. This segmentation allows independent cooling of different bearing zones without requiring a complex integrated system, as each path can be independently configured and maintained.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Different lubricant paths are configured to deliver cooled lubricant to specific local areas of the bearing that require cooling. This localized approach ensures that lubricant temperature is reduced where needed without requiring a complete redesign of the entire lubrication system, maintaining simplicity while achieving temperature control.

Inventive Principle:
Principle #3Local quality

3Adaptability or versatility

If non-planar bearing retainers are used, then axial position adjustability is achieved, but manufacturing complexity increases

Engineering Contradiction:
Improveaxial position adjustmentVSAvoidretainer geometry
Core Design Contradiction:
Adaptability or versatilityVSEase of manufacture

Solution Approach 1:

The bearing retainers are designed with non-planar surfaces that enable dynamic adjustment of the rotor assembly's axial position. The contoured surfaces allow the retainers to be positioned at different axial locations to accommodate varying clearance requirements, providing adaptability while maintaining a relatively simple retainer geometry that can be manufactured using standard machining processes.

Inventive Principle:
Principle #15Dynamics

Data Source

PatentEP3004654B1Centrifugal compressor having seal system and associated assembly method
Publication Date: 2021.11.10 INGERSOLL RAND IND US INC
  • EP3004654B1 patent drawingFigure 1
  • EP3004654B1 patent drawingFigure 2
  • EP3004654B1 patent drawingFigure 3

AI summary

Embodiments of the present disclosure are directed towards a seal assembly including a first seal and a second seal, wherein the first seal and the second seal axially about one another within a retaining bore of a compressor, and cooperatively form an outer radial contour of the seal assembly that is retained by the retaining bore.