Dual Level Pressurization Control for Gas Turbine Fuel Systems

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Solution Overview

Problem

Current gas turbine engine fuel supply systems face challenges in maintaining optimal pump discharge backpressure, leading to difficulties in scheduling priority flow during engine startup, excessive fuel system heat generation, and increased horsepower consumption when supplying fuel to secondary loads.

Innovation Solution

A dual level pressurization control system utilizing a secondary flow control valve and a pressurizing valve with a control pressure select piston and pressure control piston, which adjusts pump discharge backpressure based on whether fuel is being supplied to secondary fuel loads, maintaining different minimum pressure values accordingly.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the minimum pump discharge backpressure is maintained at a higher level to accommodate secondary flow requirements, then the fuel supply to secondary fuel loads is ensured, but the scheduling of priority flow becomes difficult during engine startup

Engineering Contradiction:
Improvefuel supply reliability to secondary loadsVSAvoidpriority flow scheduling capability
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The pressurizing valve is designed with dual pressure settings (first minimum pressure value and second minimum pressure value) that can be dynamically selected based on operational conditions. The control system switches between these pressure levels depending on whether secondary fuel loads are active, allowing the system to adapt its backpressure requirement to current operational needs rather than maintaining a fixed high pressure at all times

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system changes the pressure parameter of the pump discharge backpressure based on the operational state. When secondary fuel loads are not receiving fuel, the system lowers the minimum backpressure from the first value to the second value, enabling easier priority flow scheduling during engine startup while still maintaining sufficient pressure when secondary loads are active

Inventive Principle:
Principle #35Parameter changes

2Reliability

If the minimum pump discharge backpressure is maintained at a higher level to accommodate secondary flow requirements, then the fuel supply to secondary fuel loads is ensured, but excessive fuel system heat is generated

Engineering Contradiction:
Improvefuel supply reliability to secondary loadsVSAvoidfuel system heat
Core Design Contradiction:
ReliabilityVSTemperature

Solution Approach 1:

The system dynamically adjusts the minimum pump discharge backpressure based on whether secondary fuel loads are active. By lowering the pressure requirement to the second minimum value when secondary loads are not operational, the system reduces unnecessary pressurization and the associated heat generation in the fuel system

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The pressure parameter is changed from the first minimum pressure value to the second minimum pressure value based on operational conditions. This parameter change reduces the energy dissipation and heat generation in the fuel system when high pressure is not actually needed for secondary fuel supply

Inventive Principle:
Principle #35Parameter changes

3Reliability

If the minimum pump discharge backpressure is maintained at a higher level to accommodate secondary flow requirements, then the fuel supply to secondary fuel loads is ensured, but horsepower consumption by the fuel pumps increases

Engineering Contradiction:
Improvefuel supply reliability to secondary loadsVSAvoidhorsepower consumption by fuel pumps
Core Design Contradiction:
ReliabilityVSUse of energy by moving object

Solution Approach 1:

The fuel pump system operates with dynamic pressure requirements rather than a fixed high pressure. The control system adjusts the minimum backpressure setting based on whether secondary fuel loads are active, allowing the pump to operate at lower horsepower consumption levels during engine startup when secondary loads are not yet operational

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system changes the pressure operating parameter from the first minimum pressure value to the second minimum pressure value when secondary fuel loads are not receiving fuel. This parameter change directly reduces the horsepower consumption by the fuel pumps while maintaining sufficient pressure when needed

Inventive Principle:
Principle #35Parameter changes

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

The system effectively manages pump discharge backpressure without disrupting priority flow scheduling, reducing fuel system heat, and minimizing horsepower consumption, thereby optimizing fuel supply efficiency.

Implementation Method 1

The control pressure select piston is responsive, at least in part, to fuel pressure at the secondary flow control valve outlet port to move between a first position and a second position

Methodology Applied
Scientific EffectPressure: Pressure Increase

Implementation Method 2

the pressurizing valve, which is typically disposed downstream of the metering valve, functions to maintain a minimum system pressure magnitude in portions of the supply lines. More specifically, the pressurizing valve typically maintains pump discharge backpressure above a minimum pressure magnitude

Methodology Applied
Scientific EffectPressurization: Pressurisation

Data Source

PatentUS7966995B2Dual level pressurization control based on fuel flow to one or more gas turbine engine secondary fuel loads
Publication Date: 2011.06.28 HONEYWELL INTERNATIONAL INC
  • US7966995B2 patent drawing
  • US7966995B2 patent drawing
  • US7966995B2 patent drawing

AI summary

A system and method provide dual level pressurization control of a fuel supply system based on whether fuel is being supplied to one or more secondary fuel loads. Fuel pump discharge backpressure is maintained above either a first minimum pressure value or a lower second minimum pressure value by determining whether fuel is being supplied to one or more secondary fuel loads. The fuel pump discharge pressure is maintained above the first minimum pressure value if it is determined that fuel is being supplied to the one or more secondary loads. The fuel pump discharge backpressure is maintained above the lower second minimum pressure value if it is determined that fuel is not being supplied to the one or more secondary loads.