Variable Inlet Device Semi-Cylindrical Shells Compressor Flow

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Solution Overview

Problem

Existing compressor systems with adjustable inlet guide vanes suffer from reduced efficiency at high engine loads due to flow restriction, even in the open position, and experience increased turbocharger lag and fuel consumption at low engine loads, limiting boost pressure rise at low speeds.

Innovation Solution

A variable inlet device (VID) comprising semi-cylindrical shells pivotable about hinges within the compressor's inlet conduit, adjusting between open and closed positions to minimize or maximize flow restriction based on engine load and speed, optimizing airflow and efficiency across a range of operating conditions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If traditional adjustable inlet guide vanes are used, then flow can be restricted at low loads to prevent surge, but flow is still restricted at high loads reducing compressor efficiency

Engineering Contradiction:
Improvesurge preventionVSAvoidcompressor efficiency
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The inlet guide vanes are divided into multiple independent segments that can be controlled separately. This allows different portions of the airflow to be restricted or opened independently, enabling surge prevention at low loads while maintaining high flow capacity at high loads, thus resolving the contradiction between reliability and productivity.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The inlet guide vanes transition from a static or uniformly adjustable configuration to a dynamic multi-position system. The vanes can be positioned in multiple discrete locations (fully open, partially open, fully closed) based on operating conditions, allowing the system to adapt behavior to match the contradiction requirements across different load ranges.

Inventive Principle:
Principle #15Dynamics

2Productivity

If inlet guide vanes are positioned to maximize flow, then high end efficiency improves, but flow restriction occurs at low loads causing increased turbocharger lag

Engineering Contradiction:
Improvehigh end efficiencyVSAvoidturbocharger lag
Core Design Contradiction:
ProductivityVSLoss of time

Solution Approach 1:

The system dynamically adjusts the inlet guide vane positions based on engine operating conditions. At high loads, vanes are positioned to maximize flow and efficiency. At low loads, vanes are positioned to restrict flow and prevent surge, eliminating turbocharger lag. This dynamic adaptation resolves the contradiction between productivity and time loss.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system changes the geometric parameters of the inlet flow passage by adjusting vane positions. Different vane angles and opening areas are selected based on operating conditions, optimizing the balance between flow capacity and surge prevention to resolve the contradiction between high end efficiency and transient response.

Inventive Principle:
Principle #35Parameter changes

3Device complexity

If fixed inlet guide vanes are used, then device complexity is minimized, but compressor efficiency is reduced across all operating conditions

Engineering Contradiction:
Improveinlet guide vane mechanismVSAvoidcompressor efficiency
Core Design Contradiction:
Device complexityVSProductivity

Solution Approach 1:

The inlet guide vane assembly is segmented into multiple independently controllable sections. This segmentation enables the system to achieve variable geometry functionality without requiring a completely complex mechanism, as each segment can be adjusted independently to optimize efficiency at different operating points.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system introduces dynamic adjustability to the inlet guide vanes, allowing them to change position based on operating conditions. This dynamic capability significantly improves compressor efficiency across the operating range while the mechanism complexity remains manageable through modular design and controlled actuation of individual vane segments.

Inventive Principle:
Principle #15Dynamics

Data Source

PatentUS10190487B1Systems and methods for a bi-valved variable inlet device
Publication Date: 2019.01.29 FORD GLOBAL TECH LLC
  • US10190487B1 patent drawing
  • US10190487B1 patent drawing
  • US10190487B1 patent drawing

AI summary

Methods and systems are provided for a variable inlet device of a compressor. In one example, a compressor may include the variable inlet device arranged within an inlet conduit of the compressor. The variable inlet device may be adjustable to control the gas flow through the compressor, the variable inlet including a pair of semi-cylindrical shells that are pivotable, about a set of hinges, between an open and closed position.