Shock Absorber Maintenance Apparatus for Automated Gas-Liquid Exchange

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Solution Overview

Problem

Current methods for maintaining aircraft shock absorbers filled with both gas and liquid are laborious, inaccurate, and difficult to automate, requiring jacking up the aircraft and using high-pressure liquid pumps, and are not suitable for shock absorbers with free pistons that separate gas and liquid chambers.

Innovation Solution

A maintenance apparatus and method that uses a liquid reservoir, gas reservoir, and coupling member to create a pressure difference, allowing for automated exchange of liquid and gas within the shock absorber without jacking, using control means and sensing systems to bring the partial volumes of gas and liquid to predetermined target levels, even when the shock absorber is loaded.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the aircraft is jacked up to relieve the shock absorber of its load, then the shock absorber can be maintained, but the process becomes time-consuming and introduces risks

Engineering Contradiction:
Improvemaintenance safetyVSAvoidmaintenance cycle time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The shock absorber maintains itself under load through the automated exchange mechanism. The coupling member and reservoir system enable the shock absorber to exchange liquid and gas phases while remaining in its loaded state, eliminating the need for external jacking operations and allowing self-maintenance during normal operational conditions

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The system prepares for maintenance by establishing the coupling member connection between the shock absorber and reservoirs beforehand. The control means and sensing systems are pre-configured to detect phase boundaries and automatically initiate the exchange process, eliminating the need for preliminary aircraft jacking and manual preparation steps

Inventive Principle:
Principle #10Preliminary action

2Manufacturing precision

If a high-pressure liquid pump is used to supply liquid to the shock absorber, then the liquid level can be corrected, but the device becomes expensive and complex

Engineering Contradiction:
Improveliquid level accuracyVSAvoidmaintenance apparatus complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The system uses pneumatic pressure from the gas reservoir to drive liquid exchange instead of mechanical pumps. The gas phase pressurizes the liquid in the coupling member, forcing it into or out of the shock absorber based on detected needs, achieving precise liquid level control through gas pressure regulation rather than complex hydraulic pumping systems

Inventive Principle:
Principle #29Pneumatics and hydraulics

Solution Approach 2:

The coupling member acts as an intermediary between the shock absorber and the reservoirs. It contains the exchangeable liquid and gas phases and transfers them to/from the shock absorber under controlled pressure, eliminating the need for direct high-pressure pump connections and reducing overall system complexity

Inventive Principle:
Principle #24Intermediary (Mediator)

3Ease of operation

If the shock absorber is maintained while loaded, then the maintenance process is simplified, but the pressure difference between liquid and gas must be maintained

Engineering Contradiction:
Improvemaintenance operation easeVSAvoidpressure control requirement
Core Design Contradiction:
Ease of operationVSStress or pressure

Solution Approach 1:

The sensing system continuously monitors the positions of the free piston and liquid level within the shock absorber. This feedback information is processed by the control means, which automatically adjusts the gas pressure in the coupling member to maintain the correct pressure differential, enabling loaded maintenance while automatically managing pressure control requirements

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system dynamically changes the pressure parameter of the gas in the coupling member based on real-time detection of shock absorber internal conditions. By adjusting gas pressure rather than maintaining fixed pressure, the system adapts to loaded conditions and automatically maintains the necessary pressure difference for proper phase exchange

Inventive Principle:
Principle #35Parameter changes

4Reliability

If a free piston separates the gas and liquid chambers, then the shock absorber functions better, but it becomes impossible to determine if liquid has entered the gas chamber

Engineering Contradiction:
Improveshock absorber performanceVSAvoidphase boundary detection
Core Design Contradiction:
ReliabilityVSDifficulty of detecting and measuring

Solution Approach 1:

The system replaces mechanical inspection methods with sensing systems that detect the positions of the free piston and liquid level. These sensing systems provide electrical or optical signals to the control means, enabling automatic detection of phase boundaries and liquid intrusion without requiring physical access or disassembly of the shock absorber

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

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

Enables efficient, automated, and universally applicable maintenance of shock absorbers, reducing the risk of errors and cycle time, and allowing maintenance under varying loads, including those from weather and ship movements, while protecting free pistons from overloading.

Implementation Method 1

the coupling member causes a pressure difference between the pressure in the liquid reservoir and the pressure in the gas reservoir

Methodology Applied
Scientific EffectPressure difference: Pressure Gradient

Implementation Method 2

the pressure of the gas in the gas reservoir provides a spring action to the pressurized liquid in the liquid reservoir via the coupling member

Methodology Applied
Scientific EffectSpring action: Spring

Implementation Method 3

the gas and the liquid are pressurized during operation, due to the load on the shock absorber

Methodology Applied
Scientific EffectPressurization: Pressurisation

Data Source

PatentUS11260968B2Maintenance apparatus for a shock absorber of a landing gear, and method for maintaining such a shock absorber
Publication Date: 2022.03.01 GKN FOKKER AEROSPACE BV
  • US11260968B2 patent drawing
  • US11260968B2 patent drawing
  • US11260968B2 patent drawing

AI summary

The present invention relates to a maintenance apparatus for a shock absorber of a landing gear, comprising a liquid reservoir which can be connected to an interior space of the shock absorber via a liquid line, a gas reservoir which can be connected to the interior space via a gas line, a coupling member for sealingly coupling the liquid reservoir and the gas reservoir, wherein the maintenance apparatus is configured to allow an exchange to occur of liquid and gas between the liquid reservoir and gas reservoir, respectively, and the interior space, the maintenance apparatus comprising control means for determining that a partial volume of the interior space occupied by the gas reaches a reference level as a result of the exchange and for bringing the partial volume of the interior space of the shock absorber respectively occupied by the gas and the liquid to a target level. The invention also relates to a maintenance method.