Variable Inlet Guide Vanes Assembly Simplification

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Solution Overview

Problem

Current variable inlet guide vane systems for turbomachines, such as centrifugal compressors, are complex and difficult to assemble and install, necessitating a simpler and faster mounting process.

Innovation Solution

A variable inlet guide vane device comprising a disc-shaped member and an annular member, coaxial and forming a unit with pivotally mounted inlet guide vanes, allowing for easier assembly and testing before mounting in the turbomachine.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If traditional variable inlet guide vane systems are used, then the turbomachine can operate efficiently at different speeds, but the assembly and installation process becomes complex and time-consuming

Engineering Contradiction:
Improveoperating efficiency at different speedsVSAvoidassembly complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The variable inlet guide vane system is divided into multiple independent vanes that can be individually adjusted. Each vane is segmented from the others, allowing independent positioning to optimize airflow at different operating speeds without complicating the overall assembly process

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The inlet guide vanes are designed to be dynamically adjustable during operation. The vanes can change their inclination angle to adapt to varying rotary speeds, maintaining optimal efficiency while using a relatively simple fixed support structure

Inventive Principle:
Principle #15Dynamics

2Adaptability or versatility

If traditional variable inlet guide vane systems are used, then the turbomachine can operate efficiently at different speeds, but the installation time increases

Engineering Contradiction:
Improveoperating efficiency at different speedsVSAvoidinstallation time
Core Design Contradiction:
Adaptability or versatilityVSLoss of time

Solution Approach 1:

The inlet guide vanes are pre-positioned and pre-adjusted during manufacturing to their optimal angles for different operating conditions. This preliminary action eliminates the need for time-consuming field adjustments during installation, allowing quick mounting while preserving the ability to operate efficiently at various speeds

Inventive Principle:
Principle #10Preliminary action

3Productivity

If simplified inlet guide vane assembly is used, then assembly and installation become faster, but the ability to maintain efficiency at varying speeds may be compromised

Engineering Contradiction:
Improveassembly speedVSAvoidefficiency at varying speeds
Core Design Contradiction:
ProductivityVSAdaptability or versatility

Solution Approach 1:

The system uses multiple simple, identical vane segments rather than one complex integrated structure. This segmentation allows rapid assembly while each segment independently maintains its aerodynamic function for efficiency at different speeds

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The vanes incorporate a simple mechanical adjustment mechanism that enables dynamic angle changes during operation. This maintains adaptability to varying speeds while keeping the overall assembly simple and fast to install

Inventive Principle:
Principle #15Dynamics

Data Source

PatentUS20250163825A1Variable inlet guide vanes for a turbomachine, turbomachine including same and method
Publication Date: 2025.05.22 NUOVO PIGNONE TECH SRL
  • US20250163825A1 patent drawing
  • US20250163825A1 patent drawing
  • US20250163825A1 patent drawing

AI summary

The variable inlet guide vane device comprises a disc-shaped member and an annular member coaxial to disc-shaped member and forming a unit therewith. A set of variable inlet guide vanes are pivotally mounted between the disc-shaped member and the annular member. Each variable inlet guide vane comprises a first pivoting pin and a second pivoting pin. The first pivoting pin is pivotally supported by a first bearing housed in the disc-shaped member and the second pivoting pin is pivotally supported by a second bearing housed in the annular member.