External Fuel Container Jettison and Venting System

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Solution Overview

Problem

The transportation of flammable liquids to remote sites poses challenges due to potential damage, improper sizing and securing of containers, hazardous venting, and weight-balance issues in aircraft cargo bays, which can lead to safety hazards and operational risks.

Innovation Solution

The system integrates storage containers attached to the aircraft to maintain balance, with vented double-walled cavities and vapor barriers, a fuel jettison subsystem for emergency fuel removal, and a vent system to manage pressure changes, ensuring safe and efficient transportation of flammable liquids.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If fuel containers are transported inside aircraft cargo bays, then bulk flammable liquids can be delivered to remote sites, but the containers are subject to damage during loading and unloading as well as in flight, creating risk of explosion or fire

Engineering Contradiction:
Improvedelivery capability to remote sitesVSAvoidcontainer safety
Core Design Contradiction:
ProductivityVSReliability

Solution Approach 1:

The system divides the fuel transport function into separate components: an external container mounted on the aircraft exterior, a venting subsystem with separate vent lines, and a jettison subsystem with independent valve control. This segmentation isolates the fuel container from the cargo bay environment, protecting it from damage during loading/unloading while maintaining delivery capability to remote sites.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent introduces intermediary components including a venting subsystem with vent lines that channel vapors away from the aircraft, and a jettison subsystem with controlled valve mechanisms. These intermediaries mediate between the fuel container and the aircraft environment, preventing direct harmful interactions while enabling safe transport to remote locations.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Quantity of substance

If traditional fuel containers are used in aircraft cargo bays, then bulk flammable liquids can be transported, but improper stowing results in weight-and-balance configuration outside the safe operating envelope

Engineering Contradiction:
Improvefuel transport capacityVSAvoidweight-balance safety
Core Design Contradiction:
Quantity of substanceVSReliability

Solution Approach 1:

The external mounting system positions the fuel container at a location on the aircraft exterior that maintains proper weight and balance equilibrium. The container is secured with straps and chains arranged to distribute weight evenly, ensuring the aircraft operates within its safe center of gravity envelope regardless of fuel quantity.

Inventive Principle:
Principle #12Equipotentiality

3Stability of the object's composition

If fuel containers are vented into cargo bays, then pressure changes during flight can be accommodated, but aircraft cargo bays are not intrinsically safe environments, creating hazard when fuel containers vent or leak

Engineering Contradiction:
Improvepressure equalizationVSAvoidcargo bay contamination
Core Design Contradiction:
Stability of the object's compositionVSObject-affected harmful factors

Solution Approach 1:

The venting subsystem extracts the venting function from the cargo bay environment and relocates it to the external atmosphere. Vent lines channel vapors from the fuel container through conduits that terminate outside the aircraft, separating the pressure equalization process from the cargo bay space and eliminating contamination hazards.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The system creates an inert barrier between the flammable fuel vapors and the aircraft environment through external venting. By directing vapors away from the aircraft structure and cargo bay, the system effectively creates a safe separation zone, preventing vapors from creating hazardous conditions inside the aircraft.

Inventive Principle:
Principle #39Inert atmosphere (Inert environment)

4Object-affected harmful factors

If non-vented fuel containers are used, then cargo bay contamination is avoided, but containers are subjected to expanding and contracting forces during ascent and descent

Engineering Contradiction:
Improvecargo bay contaminationVSAvoidcontainer structural integrity
Core Design Contradiction:
Object-affected harmful factorsVSStrength

Solution Approach 1:

The venting function is extracted from the cargo bay and redirected externally through dedicated vent lines. This allows the fuel container to maintain pressure equilibrium with the external atmosphere rather than the cargo bay environment, accommodating pressure changes during flight without compromising structural integrity or creating contamination hazards.

Inventive Principle:
Principle #2Taking out (Extraction)

5Ease of operation

If fuel containers are improperly secured in the aircraft, then loading and unloading becomes simpler, but containers can be dislodged during aircraft operation creating safety hazards

Engineering Contradiction:
Improveloading simplicityVSAvoidcontainer security
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The container is pre-equipped with mounting features including attachment points for straps and chains, and a structure designed to distribute loads evenly. These preliminary structural preparations enable secure mounting that prevents dislodgement during flight while maintaining ease of loading and unloading operations.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS8668167B2System for airborne transport of flammable liquids
Publication Date: 2014.03.11 864341 ONTARIO LTD
  • US8668167B2 patent drawing
  • US8668167B2 patent drawing
  • US8668167B2 patent drawing

AI summary

A system for airborne transport of flammable liquids with an aircraft. A fuel tank and a reservoir, each for storing flammable liquids, are joined to the aircraft. A fuel jettison subsystem is coupled between an interior portion and an exterior of the reservoir to selectably expel fuel from the reservoir to an exterior portion of the aircraft. The fuel jettison subsystem includes a jettison valve opening formed in the reservoir. A lid selectably closes off the opening. A biasing member urges the lid away from the jettison valve opening. A solenoid retains the lid in the jettison valve opening when unactuated and releases the lid when actuated. A jettison linkage is coupled to the solenoid, the jettison linkage being operable to actuate the solenoid. The lid is urged away from the jettison valve opening by the biasing member when the solenoid is actuated by the jettison linkage.