Segmented Landing Gear Strut for Damping and Maintenance

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Solution Overview

Problem

Current landing gear struts in air and space vehicles are produced as single pieces, leading to high production costs, potential for entire strut scrapping due to production errors, and complex maintenance processes, as surface treatments are applied to the entire strut for effective damping.

Innovation Solution

The landing gear is designed with two separate struts, where the damping occurs only in one strut, allowing for reduced production costs and easier maintenance by separating the damping part, and using surface treatments only on the damping strut, enabling removability and efficient assembly/disassembly.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the strut is produced as a single piece with surface treatments applied along the opening, then the damping effectiveness is improved, but the production cost increases and the risk of entire strut scrapping due to production errors increases

Engineering Contradiction:
Improvedamping effectivenessVSAvoidproduction cost
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The strut is divided into two separate parts: a first strut and a second strut. The opening is provided only in the second strut, which is the removable part. This segmentation allows surface treatments to be applied only to the second strut where the opening exists, reducing production costs and allowing the first strut to be reused even if the second strut has production errors.

Inventive Principle:
Principle #1Segmentation

2Reliability

If the strut is produced as a single piece with surface treatments applied along the opening, then the damping effectiveness is improved, but the maintenance complexity increases

Engineering Contradiction:
Improvedamping effectivenessVSAvoidmaintenance complexity
Core Design Contradiction:
ReliabilityVSEase of repair

Solution Approach 1:

The strut is divided into a first strut and a second strut that can be removably connected. The opening and damper are located in the second strut, which can be independently removed and replaced. This allows maintenance to be performed on only the second strut without affecting the first strut, significantly reducing maintenance complexity.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The second strut containing the opening and damper is extracted as a separate removable component from the first strut. This extraction allows the damping components to be serviced, inspected, or replaced independently, simplifying maintenance procedures while maintaining damping effectiveness.

Inventive Principle:
Principle #2Taking out (Extraction)

3Reliability

If the entire strut is scrapped due to production errors, then the quality control is maintained, but the production cost increases and waste increases

Engineering Contradiction:
Improvequality controlVSAvoidwaste
Core Design Contradiction:
ReliabilityVSLoss of substance

Solution Approach 1:

The strut is segmented into a first strut and a second strut. Production errors affecting the second strut do not necessitate scrapping the first strut, which can be reused. This reduces material waste while maintaining quality control through selective replacement of only the affected component.

Inventive Principle:
Principle #1Segmentation

4Reliability

If surface treatments are applied to the entire strut, then the damping effectiveness is improved, but the production time and cost increase

Engineering Contradiction:
Improvedamping effectivenessVSAvoidproduction time
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

Surface treatments are applied locally only to the second strut where the opening is provided, rather than to the entire strut assembly. This localized treatment maintains damping effectiveness at the critical location while significantly reducing production time and cost by avoiding unnecessary treatment of the first strut.

Inventive Principle:
Principle #3Local quality

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

This design reduces production costs, minimizes waste, and simplifies maintenance by allowing only the relevant parts to be repaired or replaced, enhancing the efficiency and cost-effectiveness of strut production and maintenance.

Implementation Method 1

a damper provided between the strut and the wheel to move within the opening, which compresses the fluid to damp the shock effects

Methodology Applied
Scientific EffectDamping: Damping

Implementation Method 2

a fluid provided in the opening, which is compressed to provide damping against the shock effects

Methodology Applied
Scientific EffectFluid compression: Compression

Data Source

PatentUS12195173B2Landing gear
Publication Date: 2025.01.14 TUSAS TURK HAVACILIK VE UZAY SANAYII ANONIM SIRKETI
  • US12195173B2 patent drawing
  • US12195173B2 patent drawing
  • US12195173B2 patent drawing

AI summary

A landing gear for an air and/or space vehicle has a body (G); at least one wheel (T) which enables the body (G) to move on the ground; at least one strut (2) located on the body (G); at least one opening (3) forming a space in cylindrical form substantially along the strut (2); a fluid (A) which is located in the opening (3) to provide damping; at least one damper (4) located between the strut (2) and the wheel (T) to move within the opening (3) and which compresses the fluid (A) to provide damping.