Modular Aircraft Damper With Replaceable Elastic Member

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Solution Overview

Problem

Maintenance of existing mixed damping devices is challenging due to the physical link between elastic and hydraulic components, leading to costly actions when the elastic members, particularly made of elastomer, reach the end of their limited lifespan.

Innovation Solution

A modular damping device design featuring a hydraulic system and an elastic member operating in parallel, where the elastic member is separate from the hydraulic system, allowing for independent maintenance without disassembling the entire device, and a monitoring system to detect hydraulic fluid leaks.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If elastic members and hydraulic system are physically linked in a mixed damping device, then the device can provide combined elastic and hydraulic damping functions, but maintenance becomes difficult and costly when elastic members reach their limited lifespan

Engineering Contradiction:
Improvedamping function reliabilityVSAvoidmaintenance difficulty
Core Design Contradiction:
ReliabilityVSEase of repair

Solution Approach 1:

The damping device is divided into separate functional modules: an elastic member assembly and a hydraulic system assembly. Each module can be independently maintained or replaced without affecting the other, resolving the maintenance difficulty caused by physical linkage in traditional mixed dampers

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The elastic member is extracted from the hydraulic system as a separate replaceable component. This allows the elastic member to be removed and replaced independently when it reaches the end of its lifespan, eliminating the need to dismantle the entire hydraulic system for maintenance

Inventive Principle:
Principle #2Taking out (Extraction)

2Reliability

If elastic members made of elastomer are used in damping devices, then adequate damping performance can be achieved, but the limited lifespan of elastomer leads to costly maintenance actions

Engineering Contradiction:
Improvedamping performanceVSAvoidelastomer lifespan
Core Design Contradiction:
ReliabilityVSDuration of action of stationary object

Solution Approach 1:

The elastic member is designed as a disposable component with limited lifespan. When it wears out, it can be replaced with a new one without replacing the entire damping device or hydraulic system, reducing maintenance costs despite the limited lifespan of elastomer

Inventive Principle:
Principle #27Cheap short-living objects (Disposable)

Solution Approach 2:

The elastic member is designed to be discarded after reaching its lifespan and can be recovered/replaced independently from the hydraulic system, allowing cost-effective maintenance by only replacing the worn component rather than the entire device

Inventive Principle:
Principle #34Discarding and recovering

3Reliability

If complete dismantling of damping device is necessary to replace elastic member, then proper replacement can be ensured, but maintenance time and costs increase significantly

Engineering Contradiction:
Improvereplacement accuracyVSAvoidmaintenance time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The damping device is segmented into modular assemblies that can be independently accessed and maintained. The elastic member assembly can be removed and replaced without dismantling the hydraulic system, significantly reducing maintenance time while ensuring proper replacement procedures

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

Facilitates easier maintenance by allowing the elastic member to be replaced without opening the hydraulic system, optimizing maintenance actions and reducing costs associated with elastomer lifespan limitations, while ensuring reliable operation through leak detection.

Implementation Method 1

an elastic member (80) which surrounds a projecting part (43) of the rod, the elastic member comprising at least one elastic means interposed between a first armature (81) and a second armature (82)

Methodology Applied
Scientific EffectElasticity: Elasticity

Implementation Method 2

a hydraulic system (30) which comprises an outer casing (31) housing a hydraulic fluid, the hydraulic system comprising a rod movable in translation relative to the sealed outer casing

Methodology Applied
Scientific EffectViscous damping: Viscous Damping

Implementation Method 3

a monitoring system to detect hydraulic fluid leaks

Methodology Applied
Scientific EffectPressure detection: Pressure Gradient

Data Source

PatentEP3130537B1A damper device and an aircraft
Publication Date: 2019.06.12 EUROCOPTER FRANCE SA
  • EP3130537B1 patent drawingFigure 1
  • EP3130537B1 patent drawingFigure 2
  • EP3130537B1 patent drawingFigure 3

AI summary

The present invention relates to a damping device (7) provided with a first connecting member (10), a second connecting member (20), an elastic member (80) and a hydraulic system (30). The hydraulic system (30) comprises an outer casing (31) and a rod (40), said first connecting member (10) being reversibly fixed to the outer casing (31), said elastic member (80) being disposed around a projecting part (43) of the rod (40), said elastic member (80) comprising at least one elastic means (83) interposed between a first armature (81) and a second armature (82), the first armature (81) being reversibly fixed to said outer casing (31), the second armature (82) being translationally fixed to said projecting part (43), said second connecting member (20) being reversibly fixed to said projecting part (43).