Variable-Pitch Blade Control for Engine Actuator Wear Reduction

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Solution Overview

Problem

Existing turbine engines experience wear issues due to frequent and rapid adjustments in operating conditions, particularly during steady-state operations, leading to premature degradation of actuators and effectors.

Innovation Solution

Implementing a controller that switches between normal and wear reduction modes, temporarily locking primary actuators and utilizing secondary effectors to manage small signal changes, thereby reducing wear and prolonging the life cycle of engine components.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If frequent and rapid adjustments in operating conditions are made during steady-state operations, then engine responsiveness and adaptability are improved, but actuator and effector wear increases

Engineering Contradiction:
Improveengine responsivenessVSAvoidactuator and effector wear
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

The control system dynamically switches between normal operating mode and wear reduction mode based on detected operating conditions. In wear reduction mode, the system dynamically adjusts the bandwidth of control loops and limits the rate of change of effector positions, providing time-varying control characteristics that reduce wear during steady-state operations while maintaining responsiveness when needed

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system changes control parameters such as bandwidth and rate limits based on operating conditions. During wear reduction mode, the bandwidth of the effector control loop is reduced and rate limits are applied, transforming the control system's behavior from high-frequency responsive to low-frequency wear-minimizing, thereby resolving the contradiction between responsiveness and wear

Inventive Principle:
Principle #35Parameter changes

2Duration of action of stationary object

If primary actuators are locked to reduce wear, then component lifespan is extended, but engine control flexibility decreases

Engineering Contradiction:
Improvecomponent lifespanVSAvoidengine control flexibility
Core Design Contradiction:
Duration of action of stationary objectVSAdaptability or versatility

Solution Approach 1:

The system dynamically adjusts effector bandwidth based on operating mode. In wear reduction mode, bandwidth is reduced to minimize actuator activity and extend component lifespan, while in normal mode, full bandwidth is restored to maintain complete control flexibility, allowing the system to adapt between these conflicting requirements

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The control system introduces an intermediary layer that mediates between the locked effector state and the control demand. This intermediary adjusts the bandwidth and rate limits to allow sufficient control authority for necessary adjustments while filtering out high-frequency commands that would cause wear, thus balancing lifespan extension with control flexibility

Inventive Principle:
Principle #24Intermediary (Mediator)

Data Source

PatentUS12595767B2Systems and methods for engine wear reduction
Publication Date: 2026.04.07 GENERAL ELECTRIC CO
  • US12595767B2 patent drawing
  • US12595767B2 patent drawing
  • US12595767B2 patent drawing

AI summary

An engine may include a processor communicatively coupled to a pitch actuator configured to affect a pitch of a plurality of variable pitch blades and a secondary thrust effector device. The processor is configured to change the pitch of the plurality of variable pitch blades via the pitch actuator in response to changes in a target engine parameter a normal operating mode, detect a trigger condition for a wear reduction mode, and switch from the normal operating mode to the wear reduction mode, wherein in the wear reduction mode, the pitch of the plurality of variable pitch blades is maintained at a first angle, and the secondary thrust effector device is controlled in response to the changes in the target engine parameter.