Stepped Compressor Seal With Abradable Teeth for Leakage Control

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Solution Overview

Problem

Conventional refrigerant compressors experience significant leakage due to the design of traditional seals, which affects the efficiency and performance of refrigeration systems, particularly in HVAC chiller systems.

Innovation Solution

The implementation of a step seal design in refrigerant compressors, featuring a rotor and stator configuration with angled teeth and abradable portions, which creates recirculation zones and minimizes clearance between components to reduce fluid leakage, utilizing a stepped arrangement and abradable materials to carve tracks and maintain a minimal gap, thereby enhancing sealing efficiency.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of energy

If traditional seals are used in refrigerant compressors, then the structure is simple and ease of manufacture is good, but fluid leakage is significant and efficiency deteriorates

Engineering Contradiction:
Improvefluid leakageVSAvoidseal structure complexity
Core Design Contradiction:
Loss of energyVSDevice complexity

Solution Approach 1:

The seal structure is divided into multiple discrete teeth (first tooth, second tooth, third tooth) arranged in a stepped configuration. Each tooth creates separate sealing zones and recirculation cavities, breaking the continuous leakage path into multiple segments that must be overcome sequentially, thereby reducing total fluid leakage while maintaining manageable structural complexity

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The seal design transitions from a traditional single-plane sealing surface to a three-dimensional stepped structure with teeth extending radially outward at different heights. This dimensional change creates multiple sealing levels and recirculation zones, effectively reducing leakage by forcing fluid to navigate complex multi-level paths rather than flowing directly across a single plane

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

2Loss of energy

If clearance between rotor and stator is increased, then ease of operation and manufacturing tolerance are improved, but fluid leakage increases and efficiency decreases

Engineering Contradiction:
Improvefluid leakageVSAvoidclearance control
Core Design Contradiction:
Loss of energyVSManufacturing precision

Solution Approach 1:

The abradable material is applied locally to specific portions of the stator teeth (first abradable portion, second abradable portion, third abradable portion) rather than uniformly across the entire stator. This localized treatment allows the rotor teeth to carve precise tracking patterns only where needed for sealing, maintaining tight effective clearance in critical areas while preserving manufacturing tolerance in non-critical areas

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The abradable material is pre-applied to the stator teeth surfaces before operation. During initial operation, the rotor teeth automatically carve the required tracking patterns into this pre-applied material, preparing the optimal sealing geometry in advance. This preliminary action ensures that the precise clearance and tracking patterns are established before full operational loads are applied, reducing leakage without requiring extremely tight initial manufacturing tolerances

Inventive Principle:
Principle #10Preliminary action

3Reliability

If abradable material is applied to stator teeth, then sealing effectiveness is improved over time, but manufacturing complexity and cost increase

Engineering Contradiction:
Improvesealing effectivenessVSAvoidmanufacturing process simplicity
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The abradable material on the stator teeth is designed to be self-forming during operation. The rotor teeth automatically carve the required tracking patterns into the abradable material through normal operational contact, without requiring external machining or adjustment. This self-service mechanism allows the seal to automatically optimize its own geometry during operation, improving reliability while avoiding complex pre-machining processes

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The material properties of the stator tooth surfaces are changed by applying abradable material with specific erosive characteristics. This parameter change allows the material to be easily removed by the rotor teeth during operation, forming precise tracking patterns that enhance sealing. The key is selecting abradable materials that balance ease of carving during operation with sufficient durability for long-term service

Inventive Principle:
Principle #35Parameter changes

4Productivity

If stepped seal design with multiple teeth is implemented, then fluid leakage is reduced significantly, but device complexity and manufacturing difficulty increase

Engineering Contradiction:
Improvecompressor efficiencyVSAvoidseal structure complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The stepped seal structure is implemented by nesting multiple teeth of decreasing radial height in sequence (first tooth with greatest height, second tooth with intermediate height, third tooth with least height). Each tooth is nested within the radial space defined by the previous tooth, creating a compact multi-level structure that maximizes sealing effectiveness within the available radial envelope while avoiding excessive overall complexity

Inventive Principle:
Principle #7Nested doll (Nesting)

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 reduces total leakage by 40-80% compared to conventional seals, improving the overall efficiency and performance of refrigerant compressors by passively controlling fluid flow and maintaining effective sealing over time.

Implementation Method 1

the first and second teeth are configured to contact the abradable portion and carve tracks into the abradable portion over time

Methodology Applied
Scientific EffectAbrasion: Abrasion

Data Source

PatentUS11692557B2Step seal for refrigerant compressors
Publication Date: 2023.07.04 DANFOSS AS
  • US11692557B2 patent drawing
  • US11692557B2 patent drawing
  • US11692557B2 patent drawing

AI summary

In some aspects, the techniques described herein relate to a refrigerant compressor, including: a stator; a rotor configured to rotate with respect to the stator; and at least one step seal between the rotor and the stator, wherein the step seal includes a first tooth and a second tooth extending from the rotor toward the stator, wherein a downstream surface of the first tooth and an upstream surface of the second tooth are arranged at an angle relative to one another, wherein the angle is less than 90°.