Aircraft Engine Gas Pipe Damper Segment for Vibration Absorption
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Solution Overview
Problem
Designing gas pipe elements for aircraft engines poses complex challenges due to structural resistance, temperature, pressure, and dynamic structural effects like vibrations, with existing solutions lacking optimal solutions for weight management and efficient energy transfer.
Innovation Solution
The implementation of a damper segment within gas pipes made of metal mesh, featuring a rigid tube with a liner portion and a damper tube that allows for relative movement and vibration absorption, connected via catches and clamps to accommodate dynamic structural changes and energy dissipation.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Strength
If a rigid pipe structure is used to ensure structural resistance and strength, then the pipe can withstand temperature and pressure, but the pipe becomes unable to manage dynamic structural effects such as vibrations
Solution Approach 1:
The pipe is divided into multiple segments (rigid tube and flexible tube portions) that can move relative to each other. The rigid tube provides structural strength while the flexible tube segments absorb vibrations, allowing the system to simultaneously achieve both structural resistance and vibration management capabilities.
Solution Approach 2:
The pipe incorporates a flexible tube portion that can dynamically deform and move relative to the rigid tube in response to vibrations. This dynamic flexibility allows the pipe to adapt to dynamic structural effects while maintaining overall structural integrity through the rigid portions.
2Reliability
If a flexible damper tube is used to absorb vibrations, then the pipe can manage dynamic structural effects, but the structural resistance and strength are reduced
Solution Approach 1:
The pipe system is segmented into rigid tube portions that provide structural strength and flexible tube portions that provide vibration absorption. Each segment performs its specialized function while contributing to the overall system performance, allowing simultaneous achievement of both strength and vibration management.
Solution Approach 2:
Different portions of the pipe have different mechanical properties - the rigid tube portions are designed for strength and structural resistance, while the flexible tube portions are designed for vibration absorption. This local differentiation of material properties allows each portion to optimize its specific function.
3Strength
If traditional pipe designs are used to ensure structural integrity, then the pipe can withstand pressure and temperature, but the weight becomes excessive
Solution Approach 1:
The pipe uses different materials and structures in different portions - rigid tube portions where structural integrity is critical and flexible tube portions where weight reduction is prioritized. This local differentiation allows weight optimization without compromising overall structural integrity.
Solution Approach 2:
The pipe system combines different types of tube materials (rigid and flexible) in a composite structure. This allows the system to leverage the strength of rigid materials where needed and the weight advantages of flexible materials in other portions, achieving optimal balance between structural integrity and weight.
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 configuration enhances structural flexibility and vibration absorption, improving the engine's efficiency and durability by managing dynamic structural effects and energy transfer within the engine's pressurized gas paths.
Implementation Method 1
a damper tube extending between the rigid tube and the distal end, the damper tube being made of a metal mesh
Implementation Method 2
the damper tube having an unsupported length extending between the distal catch and the proximal catch
Data Source
AI summary
The damper segment can be assembled between adjacent segments of a pressurized gas pipe of an aircraft engine. The damper segment can have a proximal end, a distal end, a rigid tube at the proximal end, a damper tube extending between the rigid tube and the distal end, the damper tube being made of a metal mesh, a proximal catch structurally connecting a proximal end of the damper tube to the rigid tube, and a distal catch structurally connected between a distal end of the damper tube and the distal end, the damper tube having an unsupported length extending between the distal catch and the proximal catch, the rigid tube having a liner portion projecting into the distal segment, the liner portion extending internally relative the damper tube.


