Composite Fluid Conduit End Geometry for Impact-Protected Seal Grooves

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Composite fluid transfer conduits, such as aircraft fuel pipes, are vulnerable to impact damage at the seal groove, particularly at high angles, leading to cracks and compromised structural integrity.

Innovation Solution

The design incorporates a transition surface configured to direct impact forces radially inward of the circumferential groove, using tapered or convex curved surfaces to absorb forces away from the seal seat, combined with a raised rib for visual impact indication.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If the seal groove is formed from composite material, then cost effectiveness is improved, but vulnerability to impact damage increases

Engineering Contradiction:
Improvecost effectivenessVSAvoidvulnerability to impact damage
Core Design Contradiction:
Ease of manufactureVSReliability

Solution Approach 1:

The patent applies beforehand cushioning by providing a metallic end portion at the axial end of the composite conduit. This metallic portion acts as a protective cushion that absorbs impact forces before they reach the vulnerable composite seal groove. The metallic end portion is specifically designed to be more impact-resistant than the composite material, thereby protecting the seal groove from damage during handling and installation while maintaining the cost-effectiveness of using composite material for the seal groove geometry.

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

2Weight of moving object

If the seal groove geometry is made thin to reduce weight, then weight is reduced, but structural integrity under impact is compromised

Engineering Contradiction:
ImproveweightVSAvoidstructural integrity under impact
Core Design Contradiction:
Weight of moving objectVSStrength

Solution Approach 1:

The patent applies composite materials by combining metallic material for the end portion with composite material for the main conduit body and seal groove. This composite construction allows the thin-walled composite seal groove to maintain its weight advantage while the metallic end portion provides the necessary impact resistance. The two materials work together to achieve both weight reduction and structural integrity under impact conditions.

Inventive Principle:
Principle #40Composite materials

3Reliability

If the conduit is made fully composite, then corrosion resistance is improved, but impact resistance at the seal groove is reduced

Engineering Contradiction:
Improvecorrosion resistanceVSAvoidimpact damage
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The patent applies local quality by using different materials at different locations of the conduit. The metallic end portion is specifically placed at the location most susceptible to impact damage (the axial end where handling occurs), while the main body and seal groove use corrosion-resistant composite material. This localized material selection allows the conduit to exhibit both corrosion resistance overall and impact resistance at the critical end portion.

Inventive Principle:
Principle #3Local quality

Data Source

PatentEP4253816B1Composite fluid transfer conduit
Publication Date: 2026.01.28 CROMPTON TECH GROUP
  • EP4253816B1 patent drawingFigure 1
  • EP4253816B1 patent drawingFigure 2
  • EP4253816B1 patent drawingFigure 3

AI summary

A composite fluid transfer conduit (100) is provided. The conduit includes a first end portion (110), a second end portion (120) and a main body portion (140) between the first and second end portions. At least one of the first and second end portions is an end portion (110) comprising a circumferential groove (102) in a radially outer surface of the fluid transfer conduit, an axial end face (104), and a transition surface (106) between the axial end face and the circumferential groove. The transition surface is configured such that, for any angle of impact of the end portion (110) with a planar impact surface (20), a resultant impact force on the end portion is directed away from the circumferential groove.