Aircraft Hydraulic Actuator Recirculation for Dead Volume Bleeding

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Solution Overview

Problem

Existing aircraft hydraulic actuators suffer from dead volumes that do not refresh hydraulic fluid during normal operation, leading to unpredictable and unreliable hydraulic fluid states and requiring frequent maintenance due to air bubbles.

Innovation Solution

Implementing a hydraulic actuator system with inlet and outlet lines and one-way valves for fluid recirculation, allowing hydraulic fluid to circulate through the actuator, distributing aging more widely and providing self-bleeding mechanisms to remove air bubbles, while using a control valve for selective fluid flow without the need for pumps.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If hydraulic actuators use traditional single-line configurations, then device complexity is reduced, but hydraulic fluid recirculation and thermal management are insufficient

Engineering Contradiction:
Improvehydraulic fluid state predictabilityVSAvoidhydraulic system configuration
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The hydraulic system is segmented into separate inlet and outlet lines, allowing independent control and optimization of fluid flow paths. This segmentation enables the actuator to have dedicated ports for fluid entry and exit, facilitating recirculation while maintaining manageable system complexity through modular line configurations.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The dual-line configuration serves multiple functions simultaneously: it enables hydraulic fluid recirculation through the actuator, provides thermal management by circulating fluid, and maintains system reliability. The same inlet and outlet lines are used for both actuator operation and fluid refreshment, eliminating the need for separate recirculation pumps or valves.

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

2Reliability

If hydraulic actuators have dead volumes, then device complexity is reduced, but hydraulic fluid aging is concentrated and maintenance frequency increases

Engineering Contradiction:
Improvehydraulic fluid state uniformityVSAvoidmaintenance free period
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The hydraulic system implements continuous fluid recirculation through the actuator via the outlet line connecting back to the inlet. This continuous circulation ensures that hydraulic fluid is constantly refreshed throughout the actuator volume, preventing localized aging and degradation. The one-way valves maintain this continuous flow without requiring additional energy input from pumps.

Inventive Principle:
Principle #20Continuity of useful action

Solution Approach 2:

The hydraulic actuator system performs self-maintenance through automatic fluid recirculation. The outlet line and one-way valves enable the system to refresh its own hydraulic fluid without external intervention or additional components. The actuator chamber itself serves as part of the recirculation path, eliminating dead volumes where fluid would stagnate.

Inventive Principle:
Principle #25Self-service

3Temperature

If one-way valves are added to enable fluid recirculation, then hydraulic fluid thermal management is improved, but device complexity increases

Engineering Contradiction:
Improvehydraulic fluid temperatureVSAvoidvalve configuration
Core Design Contradiction:
TemperatureVSDevice complexity

Solution Approach 1:

One-way valves serve as intermediaries that automatically control fluid direction between the inlet and outlet lines. These valves mediate the recirculation flow without requiring active control systems, pumps, or complex valve arrangements. The valves simply respond to pressure differentials, allowing recirculation when appropriate and preventing backflow, thereby simplifying thermal management.

Inventive Principle:
Principle #24Intermediary (Mediator)

4Reliability

If inlet and outlet ports are located on opposite sides of the actuator, then fluid recirculation efficiency is improved, but manufacturing complexity increases

Engineering Contradiction:
Improvefluid recirculation effectivenessVSAvoidactuator internal routing
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The inlet and outlet ports are positioned on opposite sides of the actuator, utilizing spatial dimensionality to create an efficient recirculation path. This opposite-side configuration allows fluid to traverse the entire actuator volume, maximizing thermal exchange and preventing stagnation. The routing leverages the actuator's three-dimensional structure to achieve effective recirculation without excessive internal pathway complexity.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

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

Enhances hydraulic fluid predictability and reliability, reduces maintenance needs, and improves thermal cycling by distributing aging and removing air bubbles, thus ensuring more reliable and efficient operation.

Implementation Method 1

a first one-way valve configured to allow fluid flow along the inlet line in a direction toward the hydraulic actuator

Methodology Applied
Scientific EffectOne-way valve flow control: Valve

Implementation Method 2

a second one-way valve configured to allow fluid flow along the outlet line in a direction away from the hydraulic actuator

Methodology Applied
Scientific EffectOne-way valve flow control: Valve

Implementation Method 3

Fluid recirculation may also provide improved thermal cycling, for example with a reduction in temperature of hydraulic fluid contained within the aircraft system in use

Methodology Applied
Scientific EffectThermal cycling through fluid circulation: Convection

Implementation Method 4

any bubbles of air located within hydraulic fluid contained within the hydraulic actuator in use may be encouraged to move toward the outlet port

Methodology Applied
Scientific EffectBuoyancy: Archimedes' Principle (Buoyancy)

Data Source

PatentUS20250333035A1Aircraft system
Publication Date: 2025.10.30 AIRBUS OPERATIONS LTD
  • US20250333035A1 patent drawing
  • US20250333035A1 patent drawing
  • US20250333035A1 patent drawing

AI summary

An aircraft system is disclosed including a hydraulic actuator, an inlet line for supplying hydraulic fluid to the hydraulic actuator, an outlet line for removing hydraulic fluid from the hydraulic actuator, a first one-way valve configured to allow fluid flow along the inlet line in a direction toward the hydraulic actuator, and a second one-way valve configured to allow fluid flow along the outlet line in a direction away from the hydraulic actuator.