Compressed gas tank and method for producing same

US9683699B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9683699-B2
Application numberUS-201214352422-A
CountryUS
Kind codeB2
Filing dateSep 20, 2012
Priority dateOct 21, 2011
Publication dateJun 20, 2017
Grant dateJun 20, 2017

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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 compressed gas tank ( 1 ) made from carbon fibre materials, which has a filling and removal neck, and a method for the production thereof, with the following steps: providing a meltable core, which forms an interior of the compressed gas tank ( 1 ), wrapping the core with at least one carbon fibre bandage and impregnating the carbon fibres with a curable polymer matrix material, thereby providing a preform of the compressed gas tank ( 1 ), consolidating the polymer matrix material of the preform and obtaining the carbon fibre composite compressed gas tank ( 1 ), and liquefying the core material by melting, and removing the liquid core material from the filling and removal neck.

First claim

Opening claim text (preview).

The invention claimed is: 1. A gas tank ( 1 ) for compressed hydrogen, the tank made from carbon fibre materials, the tank having a filling and removal neck, the tank produced by a method comprising: providing a meltable core, which forms an inner shape of the compressed gas tank ( 1 ), wherein when providing the meltable core, providing a support structure made from struts or spokes ( 3 ) made from carbon fibre material in the core, wherein free ends of the struts or spokes ( 3 ) protrude beyond a surface of the core that is to be wrapped, wrapping the core including enwrapping the protruding free ends of the struts or spokes ( 3 ) with carbon fibres thereby generating at least one carbon fibre bandage, and impregnating the carbon fibres of the bandage with a curable polymer matrix material, thereby providing a preform of the compressed gas tank ( 1 ), then consolidating the polymer matrix material of the preform and obtaining the carbon fibre composite compressed gas tank ( 1 ), and during the consolidation, fixing the free ends in the carbon fibre composite bandage, liquefying the core material by melting, and removing the liquid core material from the filling and removal neck, and leaving the support structure ( 3 ) behind after the liquefaction and removal of the liquid core material in the compressed gas tank ( 1 ), wherein a wall ( 2 ) of the compressed gas tank ( 1 ) consists of a carbon fibre composite material layer and has an inner surface free from a liner layer, wherein the carbon fibre composite material layer is formed by the carbon fibre bandage made from wrapped carbon fibres and wherein the support structure made from struts or spokes ( 3 ) made from carbon fibre material is arranged inside the compressed gas tank ( 1 ), wherein the protruding strut or spoke ends are enwrapped into the carbon fibre bandage and are received in a polymer matrix of the carbon fibre composite material layer that forms the wall ( 2 ) of the compressed gas tank ( 1 ). 2. A gas tank ( 1 ) for compressed hydrogen, the tank made from carbon fibre materials, the tank having a filling and removal neck, the tank produced by a method comprising: providing a meltable core, which forms an inner shape of the compressed gas tank ( 1 ), wherein when providing the meltable core, providing a support structure made from struts or spokes ( 3 ) made from carbon fibre material in the core, wherein free ends of the struts or spokes ( 3 ) protrude beyond a surface of the core that is to be wrapped, wrapping the core including enwrapping the protruding free ends of the struts or spokes ( 3 ) with carbon fibres thereby generating at least one carbon fibre bandage, and impregnating the carbon fibres of the bandage with a curable polymer matrix material, thereby providing a preform of the compressed gas tank ( 1 ), then consolidating the polymer matrix material of the preform and obtaining the carbon fibre composite compressed gas tank ( 1 ), and during the consolidation, fixing the free ends in the carbon fibre composite bandage, liquefying the core material by melting, and removing the liquid core material from the filling and removal neck, and leaving the support structure ( 3 ) behind after the liquefaction and removal of the liquid core material in the compressed gas tank ( 1 ), wherein a wall ( 2 ) of the compressed gas tank ( 1 ) consists of a carbon fibre composite material layer and has an inner surface free from a liner layer, wherein the carbon fibre composite material layer is formed by the carbon fibre bandage made from wrapped carbon fibres and wherein the support structure made from struts or spokes ( 3 ) made from carbon fibre material is arranged inside the compressed gas tank ( 1 ), wherein the protruding strut or spoke ends are enwrapped into the carbon fibre bandage and are received in a polymer matrix of the carbon fibre composite material layer that forms the wall ( 2 ) of the compressed gas tank ( 1 ), wherein the compressed gas tank ( 1 ) is a tank ( 1 ) for compressed hydrogen. 3. A gas tank ( 1 ) for compressed hydrogen, the tank made from carbon fibre materials, the tank having a filling and removal neck, the tank produced by a method comprising: providing a meltable core, which forms an inner shape of the compressed gas tank ( 1 ), wherein when providing the meltable core, providing a support structure made from struts or spokes ( 3 ) made from carbon fibre material in the core, wherein free ends of the struts or spokes ( 3 ) protrude beyond a surface of the core that is to be wrapped, wrapping the core including enwrapping the protruding free ends of the struts or spokes ( 3 ) with carbon fibres thereby generating at least one carbon fibre bandage, and impregnating the carbon fibres of the bandage with a curable polymer matrix material, thereby providing a preform of the compressed gas tank ( 1 ), then consolidating the polymer matrix material of the preform and obtaining the carbon fibre composite compressed gas tank ( 1 ), and during the consolidation, fixing the free ends in the carbon fibre composite bandage, liquefying the core material by melting, and removing the liquid core material from the filling and removal neck, and leaving the support structure ( 3 ) behind after the liquefaction and removal of the liquid core material in the compressed gas tank ( 1 ), wherein a wall ( 2 ) of the compressed gas tank ( 1 ) consists of a carbon fibre composite material layer and has an inner surface free from a liner layer, wherein the carbon fibre composite material layer is formed by the carbon fibre bandage made from wrapped carbon fibres and wherein the support structure made from struts or spokes ( 3 ) made from carbon fibre material is arranged inside the compressed gas tank ( 1 ), wherein the protruding strut or spoke ends are enwrapped into the carbon fibre bandage and are received in a polymer matrix of the carbon fibre composite material layer that forms the wall ( 2 ) of the compressed gas tank ( 1 ), wherein the support structure ( 3 ) is a spoke support structure with spokes extending radially away from a central axis of the compressed gas tank ( 1 ). 4. The gas tank ( 1 ) according to claim 3 , wherein the compressed gas tank ( 1 ) has a round or oval cross-sectional shape.

Assignees

Inventors

Classifications

  • Hydrogen storage · CPC title

  • Component parts, details or accessories; Auxiliary operations {, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing} · CPC title

  • Integral reinforcements, e.g. ribs · CPC title

  • by adhesive means · CPC title

  • Polymers · CPC title

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Frequently asked questions

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What does patent US9683699B2 cover?
A compressed gas tank ( 1 ) made from carbon fibre materials, which has a filling and removal neck, and a method for the production thereof, with the following steps: providing a meltable core, which forms an interior of the compressed gas tank ( 1 ), wrapping the core with at least one carbon fibre bandage and impregnating the carbon fibres with a curable polymer matrix material, th…
Who is the assignee on this patent?
Daimler Ag
What technology area does this patent fall under?
Primary CPC classification B29C70/32. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Jun 20 2017 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).