Gas Turbine Inlet Filter Bypass for Pressure Drop Control

Solution Overview

Problem

Existing turbine engine filtration systems face disruptions and pressure drops due to excessive dust, debris, and moisture, leading to reduced airflow and potential compressor surges, requiring time-consuming manual filter cleaning and engine shutdowns.

Innovation Solution

A pre-filtration bypass system that uses sensors to detect operating parameters and a controller to actuate a filter assembly between operating and bypass positions, allowing for selective bypassing without manual intervention, thus maintaining engine efficiency and reducing maintenance costs.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the filter assembly operates continuously to remove dust and debris, then air filtration quality is improved, but pressure drop increases and airflow is disrupted

Engineering Contradiction:
Core Design Contradiction:
ReliabilityVSStress or pressure

Solution Approach 1:

The filter assembly is made dynamically switchable between operating and bypass positions through an actuating assembly controlled by a controller. This allows the system to adapt its filtration state based on real-time sensor feedback regarding dust levels, moisture conditions, and pressure drop measurements, optimizing the balance between filtration quality and airflow performance.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system monitors and responds to changes in operating parameters such as pressure drop across the filter, ambient moisture levels, and dust concentration. When parameters indicate excessive loading or adverse moisture conditions, the controller actuates the filter assembly to bypass position, changing the system state to maintain optimal airflow and pressure.

Inventive Principle:
Principle #35Parameter changes

2Reliability

If the filter assembly is routinely cleaned to maintain airflow, then compressor surge is prevented, but engine shutdown time increases

Engineering Contradiction:
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The system employs self-monitoring sensors that detect when filter loading reaches critical levels or when moisture conditions threaten performance. The controller automatically actuates the filter assembly to bypass position or initiates cleaning cycles without requiring manual intervention or engine shutdown, allowing the system to service itself while maintaining continuous operation.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

Sensors continuously monitor operating parameters including pressure drop, dust levels, and moisture content, providing feedback to the controller. This feedback loop enables the controller to make real-time decisions about filter assembly positioning and cleaning timing, preventing compressor surge while minimizing disruptions to engine operation.

Inventive Principle:
Principle #23Feedback

3Reliability

If the filter assembly processes all air flow, then particulate removal is maximized, but moisture-related swelling and ice formation increase

Engineering Contradiction:
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The system monitors ambient moisture levels and filter loading conditions, and when adverse moisture conditions are detected, the controller actuates the filter assembly to bypass position. This parameter-based control prevents moisture from causing contaminant swelling and ice formation while maintaining particulate removal efficiency during favorable conditions.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The controller acts as an intermediary between the sensor data and the filter assembly actuation. It processes information about moisture levels, dust concentration, and pressure drop to determine the optimal filter assembly position, mediating between the need for particulate removal and the risk of moisture-related damage.

Inventive Principle:
Principle #24Intermediary (Mediator)

Data Source

PatentUS8475115B2Pre-filtration bypass for gas turbine inlet filter house
Publication Date: 2013.07.02
  • US8475115B2 patent drawing
  • US8475115B2 patent drawing
  • US8475115B2 patent drawing

AI summary

An inlet filter house is provided for use with a turbine engine including an inlet duct. The inlet filter house is coupled to the inlet duct and includes an inlet hood including a filter assembly selectively positionable between an operating position and a bypass position. An actuating assembly is coupled to the filter assembly to selectively position the filter assembly. A sensor is configured to detect at least one operating parameter. A controller is coupled to the sensor for actuating the actuating assembly based on the at least one operating parameter.