Gas-Flotation Ring Balancing with Adjustable Dual Support

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing gas-flotation static balancing devices for rotating ring-shaped parts are limited in balancing wide parts, lack adjustable levelness, have restricted axial positioning, and are unsuitable for heavy parts due to reduced strength and stiffness.

Innovation Solution

An inner-support and gas-flotation static balancing device with a gas-flotation chamber, end cover, support base, and axial positioning mechanisms, featuring a double-supporting mode, adjustable levelness, and dispersed cylindrical gas inlet channels to improve balance precision and adaptability for parts of varying widths and weights.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If a single supporting mode is adopted in gas-flotation support device, then the structure is simple, but the device can only balance short-width parts and cannot adjust levelness

Engineering Contradiction:
Improvesupporting mode structureVSAvoidapplicability to parts of different widths
Core Design Contradiction:
Device complexityVSAdaptability or versatility

Solution Approach 1:

The gas-flotation support device is divided into two independent supporting structures: a first supporting structure for providing upward support force and a second supporting structure for providing side support force. This segmentation allows each structure to specialize in its function, enabling the device to handle parts of various widths while maintaining structural clarity and avoiding excessive complexity.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent transitions from a single supporting mode to a dual-mode supporting system that operates in different spatial dimensions. The first supporting structure operates vertically (upward support), while the second supporting structure operates horizontally (side support). This dimensional expansion enables the device to accommodate parts of varying widths and achieve levelness adjustment.

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

2Device complexity

If an integral working gas cavity is used in gas-flotation support structure, then the structure is simple, but the strength and stiffness are greatly reduced

Engineering Contradiction:
Improvegas cavity structureVSAvoidstrength and stiffness of support structure
Core Design Contradiction:
Device complexityVSStrength

Solution Approach 1:

The integral working gas cavity is divided into multiple separate working gas cavities, each corresponding to different regions of the support structure. This segmentation allows each cavity to be optimized for its specific location, maintaining structural strength and stiffness while still providing the necessary gas-flotation function. The multiple cavities work together to support the part without compromising overall structural integrity.

Inventive Principle:
Principle #1Segmentation

3Device complexity

If gas-flotation support device with single supporting mode is used, then the device structure is simple, but axial positioning range is limited

Engineering Contradiction:
Improvesupport structureVSAvoidaxial positioning range
Core Design Contradiction:
Device complexityVSLength of moving object

Solution Approach 1:

The patent incorporates adjustable axial positioning mechanisms that can dynamically adapt to parts of different lengths. The first and second supporting structures can be independently adjusted along the axial direction, allowing the device to accommodate a wide range of part widths. This dynamic adjustability extends the axial positioning range while maintaining a relatively simple overall structure.

Inventive Principle:
Principle #15Dynamics

4Adaptability or versatility

If existing static balancing device is used for rotating ring-shaped part, then the device can be used with rotors and shaft sleeves, but balancing precision is seriously reduced due to unbalanced masses and friction torque

Engineering Contradiction:
Improvecompatibility with rotors and shaft sleevesVSAvoidbalancing precision
Core Design Contradiction:
Adaptability or versatilityVSMeasurement precision

Solution Approach 1:

The patent employs gas-flotation technology to replace traditional mechanical contact-based supporting methods. By using gas pressure to support the rotating ring-shaped part, the device eliminates direct mechanical contact, thereby reducing friction torque significantly. This pneumatic approach maintains versatility in handling different rotor and shaft sleeve configurations while achieving high balancing precision through minimal friction interference.

Inventive Principle:
Principle #29Pneumatics and hydraulics

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

The device enables precise static balancing of both short and long-width rotating ring-shaped parts with reduced friction torque, improved strength, and adaptability for heavy parts, enhancing the universality and efficiency of the balancing process.

Implementation Method 1

forming a gas film with bearing capacity between the working surface (1-1) of the gas-flotation chamber (1) and an inner surface of the rotating ring-shaped part through the working gas cavity (1-2) and the gas inlet holes (1-4) by external gas supply, so as to enable the rotating ring-shaped part to float

Methodology Applied
Scientific EffectGas flotation: Air Lubrication

Data Source

PatentUS12129890B2Inner-support and gas-flotation static balancing device for rotating ring-shaped part and method of using the same
Publication Date: 2024.10.29 HARBIN INST OF TECH
  • US12129890B2 patent drawing
  • US12129890B2 patent drawing
  • US12129890B2 patent drawing

AI summary

An inner-support and gas-flotation static balancing device for a rotating ring-shaped part and a method of using the same are provided. A bottom end of an end cover is rotatably connected to a top end of a support base. One end, which is away from a working gas cavity, of the gas-flotation chamber is connected to a disc seat through a supporting column. The levelness of the gas-flotation chamber may be adjusted through the supporting column. Two axial positioning mechanisms are respectively mounted on two sides of the gas-flotation chamber in an axis direction. Gas supplied by external air supply may enter the working gas cavity, the cylindrical gas inlet channels, and the gas inlet holes through the gas supply hole, so as to form an gas film with certain bearing capacity between the working surface and the inner surface of the rotating ring-shaped part.