Multistage Roots Vacuum Pump Tip Radius Variation

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Solution Overview

Problem

Multistage Roots vacuum pumps face difficulties in achieving high volume ratios without excessively thin rotor components at the exhaust stage, leading to machining and mounting challenges, as well as reduced pumping efficiency due to varying thermal expansions and clearance issues.

Innovation Solution

A multistage vacuum pump design where the tip radius of the rotor components at the exhaust stage is smaller than at the inlet stage, allowing for a high volume ratio of at least 10:1 without reducing rotor thickness to extreme levels, with a progressive reduction in tip radius from inlet to exhaust stages and a pressure relief valve for enhanced operation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Use of energy by moving object

If the volume ratio of the pump is increased to reduce power consumption and generate higher vacuum, then the rotor thickness at the exhaust stage must be reduced, but this makes machining and mounting very difficult and reduces pumping efficiency

Engineering Contradiction:
Improvepower consumptionVSAvoidmachining and mounting difficulty
Core Design Contradiction:
Use of energy by moving objectVSEase of manufacture

Solution Approach 1:

The patent applies local quality by varying the tip radius of rotor components across different stages. The exhaust stage rotor has a smaller tip radius (e.g., 10-20mm) compared to the inlet stage rotor (e.g., 30-50mm), allowing the exhaust stage to achieve the required volume reduction for high vacuum without excessively thinning the rotor thickness. This localized geometric modification enables high volume ratios while maintaining manufacturable rotor thickness.

Inventive Principle:
Principle #3Local quality

2Productivity

If the rotor thickness is reduced to achieve high volume ratio, then the pumping efficiency decreases due to varying thermal expansions and clearance issues, but maintaining thick rotors limits the achievable volume ratio

Engineering Contradiction:
Improvepumping efficiencyVSAvoidvolume ratio
Core Design Contradiction:
ProductivityVSShape

Solution Approach 1:

The patent changes the geometric parameter of tip radius progressively from inlet to exhaust stages. This parameter change allows each stage to have optimized rotor dimensions that maintain adequate thickness for thermal stability and clearance control, while collectively achieving high volume ratio. The progressive reduction in tip radius creates a geometric progression that balances volume reduction with structural integrity.

Inventive Principle:
Principle #35Parameter changes

3Shape

If the tip radius of exhaust stage rotors is reduced to achieve high volume ratio, then the rotor thickness can be maintained at acceptable levels, but the device complexity increases

Engineering Contradiction:
Improvevolume ratioVSAvoiddevice complexity
Core Design Contradiction:
ShapeVSDevice complexity

Solution Approach 1:

The patent segments the rotor assembly into multiple stages with different tip radii. Each stage is designed with appropriate rotor dimensions for its specific pressure and volume requirements. This segmentation allows the system to achieve high overall volume ratio while each individual rotor remains manufacturable and maintainable, distributing the complexity across modular stages rather than requiring one extremely thin rotor.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS8702407B2Multistage roots vacuum pump having different tip radius and meshing clearance from inlet stage to exhaust stage
Publication Date: 2014.04.22 EDWARDS LTD
  • US8702407B2 patent drawing
  • US8702407B2 patent drawing
  • US8702407B2 patent drawing

AI summary

A multistage vacuum pump includes a stator housing a multistage rotor assembly, each stage having intermeshing Roots rotor components, wherein the tip radius of the rotor components at an inlet stage of the pump is larger than the tip radius of the rotor components at an exhaust stage of the pump, wherein a meshing clearance between the rotor components at the inlet stage of the pump is greater than a meshing clearance between the rotor components at the exhaust stage of the pump.