Aircraft Engine Gas Pipe Damper Segment for Vibration Absorption
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Solution Overview
Problem
Designing gas pipe elements for aircraft engines poses challenges due to complex structural requirements, including resistance to temperature, pressure, and dynamic effects like vibrations, while also needing to manage weight effectively.
Innovation Solution
Incorporating a damper segment within the 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 using V-Band clamps, bolt and flange connections, or welded connections to accommodate structural and thermal changes.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Strength
If a rigid pipe structure is used to ensure structural resistance, then strength and pressure resistance are improved, but weight increases and vibration management becomes difficult
Solution Approach 1:
The pipe is divided into multiple segments (rigid sections and flexible damper sections) that can be independently designed and assembled. The rigid segments provide structural strength while the flexible segments reduce weight and manage vibrations, allowing each segment to be optimized for its specific function rather than the entire pipe being uniformly rigid
Solution Approach 2:
The flexible damper section uses a thin-walled cylindrical structure with circumferential ridges that provides flexibility and vibration damping while maintaining sufficient structural resistance. This thin-walled design significantly reduces weight compared to a fully rigid pipe while still accommodating thermal expansion and pressure variations
2Strength
If a rigid pipe structure is used to ensure pressure resistance, then strength is improved, but adaptability to thermal expansion and dynamic effects deteriorates
Solution Approach 1:
The pipe transitions from a static rigid structure to a dynamic system with flexible damper sections that can adapt to thermal expansion, pressure variations, and vibrations. The flexible section's circumferential ridges allow controlled deformation and movement, enabling the pipe to accommodate thermal growth and dynamic effects while maintaining pressure containment
Solution Approach 2:
By segmenting the pipe into rigid and flexible sections, the rigid segments maintain pressure resistance while the flexible segments provide adaptability to thermal expansion and dynamic effects, allowing the system to simultaneously achieve both strength and adaptability
3Object-affected harmful factors
If vibration damping components are added to reduce vibrational energy, then vibration control is improved, but device complexity increases
Solution Approach 1:
The vibration damping function is merged into the pipe structure itself through the flexible damper section with circumferential ridges, rather than adding separate external damping components. This integration reduces overall device complexity while still achieving effective vibration control
Solution Approach 2:
The flexible thin-walled cylindrical section with circumferential ridges acts as an inherent vibration damper, absorbing and dissipating vibrational energy through its flexible structure without requiring additional damping components, thus controlling vibrations while maintaining relatively simple construction
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
The solution effectively reduces the transmission of vibrational energy and accommodates thermal and pressure changes, enhancing the structural integrity and efficiency of gas pipe elements in aircraft engines.
Implementation Method 1
a damper tube extending between the rigid tube and the distal end, the damper tube being made of a metal mesh... the damper tube having an unsupported length extending between the distal catch and the proximal catch
Implementation Method 2
the rigid tube having a liner portion projecting into the distal segment, the liner portion extending internally relative the damper tube
Data Source
Figure 1
Figure 2
Figure 3~4
AI summary
The damper segment (32) can be assembled between adjacent segments of a pressurized gas pipe (19, 22) of an aircraft engine (10). The damper segment (32) can have a proximal end (34), a distal end (40), a rigid tube (44) at the proximal end (34), a damper tube (46) extending between the rigid tube (44) and the distal end (40), the damper tube (46) being made of a metal mesh, a proximal catch (52) structurally connecting a proximal end (34) of the damper tube (46) to the rigid tube (44), and a distal catch (52) structurally connected between a distal end (40) of the damper tube (46) and the distal end (40), the damper tube (46) having an unsupported length extending between the distal catch (52) and the proximal catch (52), the rigid tube (44) having a liner portion (50) projecting into the distal segment (42), the liner portion (50) extending internally relative the damper tube (46).