Solid propellant gas generator, extinguishing device, method for cooling a flowing mixture and method for extinguishing a fire

US9283414B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9283414-B2
Application numberUS-201314024091-A
CountryUS
Kind codeB2
Filing dateSep 11, 2013
Priority dateSep 12, 2012
Publication dateMar 15, 2016
Grant dateMar 15, 2016

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A solid propellant gas generator releases a flowing mixture from a solid propellant, separated from a surrounding area, into the surrounding area. The solid propellant gas generator includes a cooling system for cooling the flowing mixture. The cooling system has at least one feed device for feeding a gas from the surrounding area to the flowing mixture in order to mix the flowing mixture prior to entering into the surrounding area with the gas from the surrounding area.

First claim

Opening claim text (preview).

The invention claimed is: 1. A solid propellant gas generator, comprising: a housing containing a solid propellant, which is separated from a surrounding area, that is released as a flowing mixture into the surrounding area; and a cooling system configured to cool the flowing mixture, wherein the cooling system has at least one feed device configured to feed a gas from the surrounding area to the flowing mixture so that gas from the surrounding area mixes with the flowing mixture prior to entering into the surrounding area, wherein the cooling system comprises: an acceleration device configured to accelerate the flowing mixture, an introducing device configured to introduce the flowing mixture into the surrounding area, and a linear contact region of acceleration device and introducing device, wherein the feed device is arranged at the linear contact region. 2. The solid propellant gas generator, as claimed in claim 1 , wherein the feed device is arranged radially to the contact region, wherein a cross-section of the feed device tapers off from the surrounding area in a direction of the contact region. 3. The solid propellant gas generator, as claimed in claim 1 , wherein the acceleration device connects an interior of the solid propellant gas generator with the contact region, a cross-section of the acceleration device tapers off from the interior in a direction of the contact region or the introducing device connects the contact region with the surrounding area, a cross-section of the introducing device expands from the contact region in a direction of the surrounding area. 4. The solid propellant gas generator, as claimed in claim 1 , wherein a cross-section of the cooling system tapers off in a flow direction of the flowing mixture. 5. The solid propellant gas generator, as claimed in claim 1 , wherein the housing includes thermal insulation. 6. The solid propellant gas generator, as claimed in claim 1 , further comprising: an igniting device configured to ignite the solid propellant to generate the flowing mixture. 7. The solid propellant gas generator, as claimed in claim 1 , wherein the solid propellant generates a gas, an aerosol, or a gas-aerosol mixture as an extinguishing agent. 8. The solid propellant gas generator, as claimed in claim 7 , further comprising: a metal mesh filter unit arranged between the cooling system and the solid propellant. 9. A solid propellant gas generator, comprising a housing containing a solid propellant, which is separated from a surrounding area, that is released as a flowing mixture into the surrounding area; and a cooling system configured to cool the flowing mixture, wherein the cooling system has at least one feed device configured to feed a gas from the surrounding area to the flowing mixture so that gas from the surrounding area mixes with the flowing mixture prior to entering into the surrounding area, wherein the cooling system comprises a sealing mechanism configured to seal off the interior from the surrounding area, wherein the sealing mechanism is a water impermeable foil. 10. The solid propellant gas generator, as claimed in claim 9 , wherein the feed device is arranged at the cooling system downstream of the sealing mechanism in a flow direction of the flowing mixture. 11. The solid propellant gas generator, as claimed in claim 9 , further comprising: an ignition device configured to ignite the solid propellant to generate the flowing mixture. 12. The solid propellant gas generator, as claimed in claim 9 , wherein the solid propellant generates a gas, an aerosol, or a gas-aerosol mixture as an extinguishing agent. 13. The solid propellant gas generator, as claimed in claim 12 , further comprising: a metal mesh filter unit arranged between the cooling system and the solid propellant. 14. An extinguishing device for extinguishing a fire, the comprising: a solid propellant gas generator, which includes a housing containing a solid propellant, which is separated from a surrounding area, that is released as a flowing mixture into the surrounding area; and a cooling system configured to cool the flowing mixture, wherein the cooling system has at least one feed device configured to feed a gas from the surrounding area to the flowing mixture so that gas from the surrounding area mixes with the flowing mixture prior to entering into the surrounding area, wherein the cooling system comprises: an acceleration device configured to accelerate the flowing mixture, an introducing device configured to introduce the flowing mixture into the surrounding area, and a linear contact region of acceleration device and introducing device, wherein the feed device is arranged at the linear contact region.

Assignees

Inventors

Classifications

  • A62C13/22Primary

    with incendiary substances producing pressure gas · CPC title

  • Extinguishants produced by combustion · CPC title

  • Fire prevention, containment or extinguishing specially adapted for particular objects or places ({in oil wells E21B29/08, A62C35/00; in mines or tunnels E21F5/00} ; for nuclear reactors G21C9/04) · CPC title

  • Methods of extinguishing or preventing the spread of fire by cooling down or suffocating the flames · CPC title

  • with the chemicals in a single case, e.g. in a cartridge · CPC title

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What does patent US9283414B2 cover?
A solid propellant gas generator releases a flowing mixture from a solid propellant, separated from a surrounding area, into the surrounding area. The solid propellant gas generator includes a cooling system for cooling the flowing mixture. The cooling system has at least one feed device for feeding a gas from the surrounding area to the flowing mixture in order to mix the flowing mixture prior…
Who is the assignee on this patent?
Eads Deutschland Gmbh, Airbus Defence & Space Gmbh
What technology area does this patent fall under?
Primary CPC classification A62C13/22. Mapped technology areas include Human Necessities.
When was this patent published?
Publication date Tue Mar 15 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).