Gas Turbine Start Control via Dynamic Mode Selection

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Conventional gas turbine engine start modes often result in incomplete or delayed starts and excessive engine temperature conditions due to inappropriate pilot selection, necessitating a more automatic and autonomous engine control system for selecting the appropriate start mode based on system parameters.

Innovation Solution

An engine system with a controller that evaluates engine system parameters, such as acceleration, to select between windmill and assisted start modes, generating specific acceleration and fuel commands to optimize start operations, thereby reducing pilot workload and improving start efficiency.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If pilot manually selects start mode, then start mode selection is flexible, but start operations may be incomplete or delayed due to inappropriate selection

Engineering Contradiction:
Improvepilot workloadVSAvoidstart completion
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The engine control system automatically selects the appropriate start mode (assisted or windmill) based on real-time evaluation of engine parameters such as air speed and engine temperature, eliminating the need for pilot intervention in mode selection and ensuring optimal start operations

Inventive Principle:
Principle #25Self-service

2Speed

If assisted start mode is used, then engine start speed is increased, but engine temperature may become excessive

Engineering Contradiction:
Improveengine start speedVSAvoidengine temperature
Core Design Contradiction:
SpeedVSTemperature

Solution Approach 1:

The system dynamically adjusts the start mode based on real-time engine conditions. When engine temperature is already high, the system selects windmill start mode instead of assisted start mode, automatically adapting to prevent excessive temperature while still achieving necessary start speed

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The engine control continuously monitors engine parameters including temperature and air speed, using this feedback to determine the appropriate start mode. The system evaluates whether assisted or windmill start is more suitable based on current conditions, creating a closed-loop control that prevents excessive temperature rise

Inventive Principle:
Principle #23Feedback

3Temperature

If windmill start mode is used, then engine temperature is controlled, but start speed may be insufficient

Engineering Contradiction:
Improveengine temperatureVSAvoidengine start speed
Core Design Contradiction:
TemperatureVSSpeed

Solution Approach 1:

The system dynamically switches between windmill and assisted start modes based on real-time evaluation of engine parameters. When wind conditions are insufficient or engine temperature allows, the system transitions to assisted start mode to ensure adequate start speed is achieved

Inventive Principle:
Principle #15Dynamics

4Measurement precision

If automatic engine control is implemented, then start mode selection accuracy is improved, but system complexity increases

Engineering Contradiction:
Improveparameter evaluation accuracyVSAvoidcontrol system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The engine control system performs multiple functions including automatic start mode selection, parameter monitoring, and conditional logic evaluation within a single integrated controller, avoiding the need for separate dedicated systems and managing complexity through functional integration

Inventive Principle:
Principle #6Universality (Multi-functionality)

Data Source

PatentEP2613040B1Engine systems with enhanced start control schedules
Publication Date: 2019.11.06 HONEYWELL INTERNATIONAL INC
  • EP2613040B1 patent drawingFigure 1
  • EP2613040B1 patent drawingFigure 2
  • EP2613040B1 patent drawingFigure 3~4

AI summary

An engine system (100) for starting a gas turbine engine (110) includes a starter (140) coupled to the gas turbine engine and configured to provide torque to the gas turbine engine; and a controller (150) coupled to the starter and configured to evaluate an engine system parameter and to select from a plurality of start modes for starting the gas turbine engine based on the engine system parameter.