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Fuel cell devices for fire prevention on-board aircraft

A fuel cell system and aircraft technology, applied in the field of aviation aircraft, can solve problems such as excessive voltage, overheating of components, arc discharge, etc.

Pending Publication Date: 2018-02-13
SAFRAN AEROTECHNICS SAS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

There is a risk that electrical components or other compartment areas may be subjected to excessive voltage, excessive current, or other conditions that could result in arcing, overheating of components, and / or other possible causes of fire

Method used

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  • Fuel cell devices for fire prevention on-board aircraft
  • Fuel cell devices for fire prevention on-board aircraft
  • Fuel cell devices for fire prevention on-board aircraft

Examples

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Embodiment Construction

[0022] The subject matter of the present invention is described herein with particularity to satisfy legal requirements, but this description is not necessarily intended to limit the scope of the claims. The claimed subject matter may be embodied in other ways, may comprise different elements or steps, and may be used in combination with other present or future technologies. This description should not be interpreted as implying any particular order or arrangement between various steps or elements, unless the order of individual steps or arrangement of elements is explicitly described.

[0023] Disclosed herein are systems and processes for providing an inerting system that supplies an inert gas or an inert medium to electrical compartments housing electrical components. The systems and processes may also supply inert gas or media to other compartments on an aircraft or other passenger transport vehicle. The inerting system may be powered by the fuel cell system and / or incorp...

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Abstract

Described are inerting systems that may be used on board an aircraft or other passenger transportation vehicle to reduce a risk of fire due to electronic components or to other elements in a compartment and to assist in preventing or extinguishing any fire or hazardous condition that may occur. The systems include a source of inert gas such as oxygen depleted air generated from a fuel cell on board the aircraft. The oxygen depleted air or other inert gas is conveyed through ducts to compartments that house the electronics, thus changing the conditions in the compartment to be less conducive tofire.

Description

[0001] Cross References to Related Applications [0002] This application is related to and claims priority from US Provisional Application Serial No. 62 / 106,493, entitled "FUEL CELL-ODA USAGE," filed January 22, 2015, which is hereby incorporated by reference in its entirety. technical field [0003] Embodiments of the invention relate generally to the field of aerospace vehicles using fuel cell system by-products to prevent or extinguish fires. In some cases, the system is particularly useful for delivering oxygen-depleted air to compartments housing electrical components and / or any other compartments where there is a risk of fire. Background technique [0004] Many components onboard an aircraft require electrical power for their activation. Many of these components are separate from the electrical components actually required to run the aircraft (ie, navigation systems, fuel gauges, flight controls, and hydraulic systems). For example, aircraft also have catering equi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): A62C3/08A62C5/00A62C99/00
CPCA62C3/08A62C5/006A62C99/0018A62C3/16B64D11/04B64D37/32B64D41/00B64D2041/005B64D2221/00
Inventor S·克拉森F·马塞特A·胡格文H·兹拉艾L·布隆C·西里C·方辛G·加格J·兰达R·席福尔斯特
Owner SAFRAN AEROTECHNICS SAS
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