Oil-Free Screw Compressor Shaft Seal Pressure Loss

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing oil-free screw compressors face significant pressure loss issues at the annular space where the atmosphere open hole and communication hole communicate, leading to inadequate prevention of lubricant flow into the rotor chamber during unloading operations.

Innovation Solution

The design includes an inner peripheral annular space on the casing side, with a larger open cross-sectional area than the communication holes, ensuring a wider annular space in the axial direction, which reduces pressure loss and prevents lubricant ingress by satisfying the relationship S1 ≥ ∑S2i, where S1 is the open cross-sectional area of the annular space and S2 is the total area of the communication holes.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If an annular space is formed on the outer peripheral surface of the shaft seal device, then lubricant flow prevention is improved, but pressure loss increases due to small open cross-sectional area

Engineering Contradiction:
Improvelubricant flow preventionVSAvoidpressure loss
Core Design Contradiction:
ReliabilityVSLoss of energy

Solution Approach 1:

The invention relocates the annular space from the outer peripheral surface of the shaft seal device to the inner peripheral surface of the casing, utilizing the radial dimension more effectively. This dimensional relocation allows the annular space to have a significantly larger open cross-sectional area while still preventing lubricant flow into the rotor chamber, thereby resolving the contradiction between lubricant flow prevention and pressure loss reduction

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

2Reliability

If O-rings are disposed on both air seal and visco-seal, then sealing is improved, but axial space is restricted making it difficult to ensure adequate annular space width

Engineering Contradiction:
ImprovesealingVSAvoidaxial space
Core Design Contradiction:
ReliabilityVSLength of moving object

Solution Approach 1:

The invention moves the annular space formation from the axial dimension (outer peripheral surface) to the radial dimension (inner peripheral surface of casing). This dimensional shift allows the annular space to be formed without consuming additional axial space, thereby maintaining adequate width for lubricant flow prevention while preserving sealing effectiveness with the O-rings

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

3Reliability

If communication holes are formed in the shaft seal device, then lubricant flow prevention is improved, but manufacturing complexity increases

Engineering Contradiction:
Improvelubricant flow preventionVSAvoidmanufacturing complexity
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The invention extracts the annular space formation from the shaft seal device and relocates it to the casing. This separation simplifies the shaft seal device manufacturing while the casing can be easily formed with the annular space through standard machining or casting operations, thereby reducing overall manufacturing complexity while maintaining lubricant flow prevention functionality

Inventive Principle:
Principle #2Taking out (Extraction)

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 effectively minimizes pressure loss in the annular space, ensuring the lubricant is not drawn into the rotor chamber during unloading, thereby enhancing the sealing efficiency of the compressor.

Implementation Method 1

When the rotor chamber is brought into a negative pressure state, atmospheric air is introduced into the ventilation gap through the atmosphere open passage thus preventing the lubricant from flowing into the rotor chamber

Methodology Applied
Scientific EffectPressure gradient: Pressure Gradient

Implementation Method 2

this configuration effectively minimizes pressure loss in the annular space, ensuring the lubricant is not drawn into the rotor chamber during unloading

Methodology Applied
Scientific EffectPressure loss reduction: Pressure Drop

Data Source

PatentUS10309402B2Oil-free screw compressor having atmosphere open hole formed in casing and communication hole formed in shaft seal device
Publication Date: 2019.06.04 KOBELCO COMPRESSORS CORP
  • US10309402B2 patent drawing
  • US10309402B2 patent drawing
  • US10309402B2 patent drawing

AI summary

An oil-free screw compressor includes: a casing having a rotor chamber; a bearing supporting rotary shafts of the screw rotors; a shaft seal device including an oil seal portion and an air seal portion; an atmosphere open hole formed in the shaft seal device; at least one communication hole formed in the rotary shaft; and an annular space communicating the atmosphere open hole with the at least one communication hole communicate with each other. The annular space includes an inner peripheral annular space formed on an inner peripheral side of the casing. Assuming an open cross-sectional area of the inner peripheral annular space as S1, a total open cross-sectional area of the communication holes as S2, an open cross-sectional area of the i-th communication hole out of the communication holes as S2i, and the number of communication holes as n (n being a natural number of 1 or more), a following relationship is satisfied.S⁢⁢1≧S⁢⁢2=∑i=1n⁢⁢S⁢⁢2⁢i