Split Range Control for Aircraft Fuel Tank Pressurization

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Solution Overview

Problem

Existing systems for pressurizing aircraft fuel tanks face challenges in rapidly adapting to changing ambient pressures while minimizing weight and maintaining a relative air pressure, as they often require excessive pressurized air and are prone to structural damage due to rapid pressure changes.

Innovation Solution

A system with two regulators and ejectors, along with check valves, that dynamically adjusts airflow to maintain a specified pressure interval by using a first regulator for primary pressure control and a second regulator for high-demand situations, minimizing the need for pressurized air and ensuring system reliability and low weight.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Speed

If a large opening is used for air flow to rapidly change pressure inside the tank, then the speed of pressure adaptation is improved, but the amount of pressurized air required increases significantly

Engineering Contradiction:
Improvespeed of pressure adaptationVSAvoidamount of pressurized air
Core Design Contradiction:
SpeedVSQuantity of substance

Solution Approach 1:

The air flow path is segmented into two separate paths: a first path with a first regulator for normal pressure control, and a second path with a second regulator for rapid pressure equalization. This segmentation allows the system to use a large opening in the second path only when needed for rapid adaptation, while keeping the first path closed during normal operation to minimize pressurized air consumption.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system dynamically switches between two operating modes by controlling two separate regulators. During normal operation, only the first regulator is active with a small opening. When rapid pressure adaptation is needed, the second regulator opens with a large opening. This dynamic switching optimizes both speed and pressurized air usage based on real-time conditions.

Inventive Principle:
Principle #15Dynamics

2Manufacturing precision

If a closed regulating system is used with active regulation on both air inflow and outflow, then the pressure control precision is improved, but the device complexity increases

Engineering Contradiction:
Improvepressure control precisionVSAvoiddevice complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The closed regulating system is segmented into two independent but coordinated regulation paths. The first regulator handles normal pressure control with fine adjustment, while the second regulator handles rapid pressure equalization. This segmentation allows each regulator to be optimized for its specific function, maintaining high precision while managing complexity through functional separation.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system uses partial action by activating only the necessary regulator based on current conditions. During normal operation, only the first regulator is active. During rapid pressure changes, the second regulator is activated in addition to or instead of the first. This partial activation reduces the effective complexity of the system at any given moment while maintaining the capability for high-precision control when needed.

Inventive Principle:
Principle #16Partial or excessive action

3Ease of manufacture

If a static throttling size is used to block outflow, then the ease of manufacture is improved, but the adaptability to varying pressure conditions deteriorates

Engineering Contradiction:
Improveease of manufactureVSAvoidadaptability to pressure conditions
Core Design Contradiction:
Ease of manufactureVSAdaptability or versatility

Solution Approach 1:

While each individual throttling remains static for ease of manufacture, the system achieves adaptability through dynamic control of two separate throttles. The first throttle is optimized for normal operation, while the second throttle is optimized for rapid pressure equalization. The system dynamically switches between these two static configurations based on pressure conditions, achieving both manufacturability and adaptability.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The single adaptive throttle is segmented into two separate static throttles, each optimized for specific operating conditions. This segmentation allows each throttle to be manufactured with fixed dimensions for ease of production, while the system as a whole achieves adaptability through coordinated control of both throttles based on real-time pressure conditions.

Inventive Principle:
Principle #1Segmentation

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 efficiently manages pressure changes with reduced pressurized air usage, maintains system reliability, and minimizes weight, while also preventing tank explosions through a security valve.

Implementation Method 1

using the airflow through the first ejector to suck in additional ambient air through the first ejector and add it to the first airflow into the volume

Methodology Applied
Scientific EffectEjector effect: Venturi Effect

Data Source

PatentEP2744707B1Split range control for pressurisation
Publication Date: 2016.09.28 SAAB AB
  • EP2744707B1 patent drawingFigure 1
  • EP2744707B1 patent drawingFigure 2
  • EP2744707B1 patent drawingFigure 3

AI summary

The invention aims at pressurising a volume (2) that needs to have a relative air pressure, in comparison with an ambient pressure, where the ambient air pressure can change rapidly and with large amplitude and where the access to pressurised air is limited. This is solved by a half open system comprising two parallel regulators (9) and (17) and two ejectors (15) and (19) working according to a split range control principle. When the relative air pressure difference is above a desired value of the second regulator (17), only the first regulator and the first ejector work. When the relative air pressure difference is below the desired value of the second regulator (17), both regulators (9) and (17) and ejectors (15) and (19) work. In this way the pressure inside the volume (2) can adapt rapidly to the changes in the ambient pressure, without leaking too much air during a static condition.