Inlet Guide Vane Geometry for Low-Pressure-Loss Flow Control

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing inlet guide vanes in turbo compressors face challenges in manufacturing precision due to curved surface formation difficulties and high pressure loss, especially when molded as cast products, leading to performance deterioration and increased manufacturing costs.

Innovation Solution

The inlet guide vane design features a tapered portion with approaching side surfaces and a parallel portion, allowing for precise machining and reduced pressure loss, enabling adjustment of suction volume and flow direction without disturbing fluid flow, while facilitating easy reference setting and cost-effective manufacturing.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of energy

If the vane body is formed with curved surfaces (aerofoil shape) to reduce pressure loss, then the pressure loss is reduced and flow is not disturbed, but it is difficult to manufacture with high precision due to casting limitations

Engineering Contradiction:
Improvepressure lossVSAvoidmanufacturing precision
Core Design Contradiction:
Loss of energyVSManufacturing precision

Solution Approach 1:

The invention changes the geometric parameters of the vane body from curved surfaces to planar surfaces. Specifically, the side surface on the positive pressure side and the side surface on the negative pressure side are both formed as planar surfaces, which can be precisely manufactured by casting while still achieving the function of guiding fluid flow and reducing pressure loss.

Inventive Principle:
Principle #35Parameter changes

2Ease of operation

If the vane body is formed with curved surfaces (aerofoil shape), then the suction volume and flow direction can be adjusted without disturbing flow, but reference setting becomes difficult during shaft machining

Engineering Contradiction:
Improveflow adjustment capabilityVSAvoidease of manufacture
Core Design Contradiction:
Ease of operationVSEase of manufacture

Solution Approach 1:

The invention changes the surface geometry from curved to planar, making the side surfaces flat and easy to reference during machining operations. The planar surfaces provide stable reference planes for setting the shaft orientation while maintaining the ability to adjust suction volume and flow direction through rotation.

Inventive Principle:
Principle #35Parameter changes

3Ease of manufacture

If the vane body is formed as a flat plate with constant thickness, then manufacturing is easy, but the flow of refrigerant is disturbed and pressure loss becomes large

Engineering Contradiction:
Improveease of manufactureVSAvoidpressure loss
Core Design Contradiction:
Ease of manufactureVSLoss of energy

Solution Approach 1:

The invention modifies the thickness parameter of the vane body by forming it with non-constant thickness. The side surfaces are formed as planar surfaces that are not parallel to each other, creating a varying thickness profile that guides the fluid flow smoothly and reduces pressure loss while remaining manufacturable by casting.

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentUS8181479B2Inlet guide vane, turbo compressor, and refrigerator
Publication Date: 2012.05.22 DAIKIN INDUSTRIES LTD
  • US8181479B2 patent drawing
  • US8181479B2 patent drawing
  • US8181479B2 patent drawing

AI summary

An inlet guide vane is installed at a suction port into which a fluid is sucked by the rotation of an impeller so as to be rotatable about an axis, and is comprised of a rod-like shaft supported by an inner peripheral surface of the suction port so as to be rotatable about the axis, and a plate-like vane body connected to the shaft and provided so as to protrude from the inner peripheral surface of the suction port. The vane body includes a tapered portion formed such that both side surfaces approach each other toward an outer edge of the vane body in its width direction and an outer edge thereof at a tip in the direction of the axis, and a parallel portion arranged on the axis and formed such that both the side surfaces are parallel to each other along the direction of the axis.