Dry-Break Refueling Coupling for Pressure and Gravity Filling

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Solution Overview

Problem

Existing refueling couplings do not efficiently facilitate both pressure and gravity refueling without fuel leakage, particularly in scenarios where the transition between refueling methods is not seamlessly managed.

Innovation Solution

A refueling coupling design featuring a displaceable dry-break member with a manually removable subsidiary member for gravity refueling, utilizing a bayonet fitting or screw threads, and a tether to prevent loss, ensuring fluid-tight sealing and easy manual handling.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a subsidiary displaceable member is used to close the aperture for gravity refueling, then fuel leakage is prevented during pressure refueling, but the device complexity increases due to additional components

Engineering Contradiction:
Improvefuel leakage preventionVSAvoidnumber of components
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The subsidiary displaceable member is integrated with the dry-break member through a pivotal connection, allowing both components to work together as a unified sealing system. The member is carried by the dry-break member and pivots on a pin, combining the sealing functions of both elements while reducing overall system complexity compared to separate independent components.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The subsidiary displaceable member serves multiple functions: it closes the aperture during pressure refueling to prevent fuel leakage, and is displaceable to allow gravity refueling when needed. This multi-functional design eliminates the need for separate mechanisms for each refueling mode, thereby reducing device complexity while maintaining reliability.

Inventive Principle:
Principle #6Universality (Multi-functionality)

2Ease of operation

If the subsidiary displaceable member is pivotally displaceable with a return spring, then automatic closure is achieved after gravity refueling, but the device complexity increases

Engineering Contradiction:
Improveautomatic closureVSAvoidmechanism complexity
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The return spring automatically returns the subsidiary displaceable member to its closed position after gravity refueling without requiring manual intervention. The spring is compressed when the member is displaced for gravity refueling and automatically pushes it back to the sealing position, making the system self-servicing and eliminating the need for additional actuation mechanisms.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The subsidiary member exhibits periodic motion: it is displaced during gravity refueling and automatically returns to its closed position via the spring. This periodic action alternates between open and closed states based on refueling mode, simplifying operation while using a straightforward spring mechanism rather than complex control systems.

Inventive Principle:
Principle #19Periodic action

3Adaptability or versatility

If an aperture is provided in the dry-break member for gravity refueling, then gravity refueling capability is enabled, but fuel leakage risk increases during pressure refueling

Engineering Contradiction:
Improverefueling method flexibilityVSAvoidfuel leakage risk
Core Design Contradiction:
Adaptability or versatilityVSObject-affected harmful factors

Solution Approach 1:

The subsidiary displaceable member is pre-positioned to close the aperture before pressure refueling begins. This preliminary closure action prevents fuel leakage through the aperture during pressure refueling, while still allowing the aperture to be opened when gravity refueling is required. The member is normally closed and only opened when needed.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The subsidiary displaceable member is designed to be dynamically displaceable rather than fixed. It can pivot between closed and open positions depending on the refueling mode required. This dynamic capability allows the system to adapt to different refueling methods while maintaining fuel containment when the aperture is not in use.

Inventive Principle:
Principle #15Dynamics

Data Source

PatentUS11904681B2Refuelling coupling
Publication Date: 2024.02.20 REMFRY LEIGH MAXWELL
  • US11904681B2 patent drawing
  • US11904681B2 patent drawing
  • US11904681B2 patent drawing

AI summary

A refueling coupling has an annular fitting 101 having a bore 102, bayonet lugs 103 and slots 104 suiting it for connection to a pressure filling nozzle. A flange 122, drilled with screw holes for securement to a fuel tank (not shown), extends out from the fitting 101. Also not shown for the sake of clarity is a tube extending own from the flange. Rods extend down from the flange 122 to a spider 125, with springs bearing upwards onto the underside of a dry-break member 105, through which the rods extend. The rods, springs and spider are within the non-shown tube.On attaching and opening of a pressure filling nozzle to the coupling, the dry-break member 105 is displaced resiliently inwards fuel can flow past this member and into the tank.The dry-break member has a central aperture 111, normally closed by a plug 112, which is threaded externally 114 and carries an O-ring seal 115 above the thread. The central aperture has a plain bore orifice 116 and is threaded 117 below the plain bore. Thus, when the plug is screwed in, the dry-break member is fluid tight as normal.