Aircraft Engine Fuel Pump Bypass for Low-Power Heat Control

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Solution Overview

Problem

Existing fuel systems in turbo engines experience inefficiencies during lower power modes, leading to increased heat generation, fuel congealing, and degradation of thermal management systems due to the fixed speed ratio of boost and main pumps, which results in coke formation and the need for additional cooling systems that add weight and complexity.

Innovation Solution

A hybrid fuel system with an auxiliary electric pump that can be activated during lower power modes to bypass the boost and main pumps, reducing heat generation and eliminating the need for additional cooling systems by operating in multiple modes.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If boost and main pumps operate at fixed speed ratio driven by engine shaft, then fuel flow is maintained during high power modes, but heat generation increases and fuel congealing occurs during lower power modes

Engineering Contradiction:
Improvefuel flow rateVSAvoidfuel temperature
Core Design Contradiction:
ProductivityVSTemperature

Solution Approach 1:

The system transitions from fixed-speed pumps to variable-speed operation by introducing an electric auxiliary pump that can adjust its speed independently. The controller dynamically switches between the mechanical drive system (boost and main pumps driven by engine shaft) and the electric drive system (auxiliary pump), allowing the fuel pumping system to adapt its operating characteristics to match actual engine power requirements and prevent fuel congealing during low-power modes.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The patent replaces the purely mechanical drive system with a hybrid system that incorporates an electric auxiliary pump. During lower power modes, the electric auxiliary pump takes over the fuel pumping function, eliminating the mechanical drive train's fixed speed ratio constraint and allowing for variable speed operation that prevents fuel temperature rise and congealing while maintaining adequate fuel flow.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

2Temperature

If additional cooling systems are added to address heat generation, then fuel temperature control improves, but system weight and complexity increase

Engineering Contradiction:
Improvefuel temperature controlVSAvoidcooling system complexity
Core Design Contradiction:
TemperatureVSDevice complexity

Solution Approach 1:

The patent extracts and eliminates the need for separate cooling systems by addressing the root cause of heat generation - the fixed-speed mechanical pumps that over-pump fuel during low-power modes. By introducing variable-speed control through the electric auxiliary pump, the system prevents excessive heat generation at the source rather than adding cooling systems to manage it, thereby avoiding increased weight and complexity.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The patent converts the harmful effect of heat generation into a beneficial control mechanism. Instead of adding cooling systems to dissipate heat, the controller uses the electrical pump's variable speed capability to match fuel flow demand precisely, thereby preventing heat generation in the first place. This transforms the problem of heat management into a problem of flow control, eliminating the need for thermal management hardware.

Inventive Principle:
Principle #22Blessing in disguise (Convert harm into benefit)

3Loss of energy

If electric auxiliary pump is introduced to bypass mechanical pumps during lower power modes, then heat generation is reduced, but additional component is added

Engineering Contradiction:
Improveheat generationVSAvoidpump system complexity
Core Design Contradiction:
Loss of energyVSDevice complexity

Solution Approach 1:

The electric auxiliary pump serves multiple functions: it provides fuel pumping capability during low-power modes when mechanical pumps are inefficient, enables variable speed control to prevent fuel congealing, and allows the system to operate in hybrid mode combining both mechanical and electric pumping. This multi-functionality justifies the additional component by consolidating several needs into a single device.

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

Solution Approach 2:

The system dynamically discards the mechanical drive train during low-power modes by engaging the electric auxiliary pump instead, recovering the inefficiencies of the mechanical system during these operating conditions. The controller selectively activates the electric pump only when needed, minimizing the operational impact on overall system complexity while maximizing energy efficiency.

Inventive Principle:
Principle #34Discarding and recovering

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 hybrid fuel system prevents fuel congealing and reduces the need for cooling systems, maintaining efficient fuel temperature and improving thermal management without adding significant weight or complexity.

Implementation Method 1

an auxiliary electric pump that can be activated during lower power modes to bypass the boost and main pumps

Methodology Applied
Scientific EffectPump: Pump

Data Source

PatentUS20260085636A1Fuel Systems for Aircraft Engines
Publication Date: 2026.03.26 GENERAL ELECTRIC CO
  • US20260085636A1 patent drawing
  • US20260085636A1 patent drawing
  • US20260085636A1 patent drawing

AI summary

A turbo engine for an aircraft includes a gas turbine engine having a combustion section and a fuel system to provide pressurized fuel to the combustion section. The fuel system includes a fuel tank and a boost pump and a main pump driven by an accessory gearbox that is powered by a shaft of the turbo engine. The boost pump and the main pump are arranged in series. The fuel system also includes an auxiliary pump and a controller to operate the fuel system in (1) a first mode in which the boost pump and the main pump produce pressurized fuel for the turbo engine and the auxiliary pump is deactivated, and (2) a second mode in which the auxiliary pump is activated and produces the pressurized fuel for the turbo engine while bypassing the boost pump and the main pump.