Composite pressure vessel for gas storage and method for its production

Abstract

A pressure vessel includes a carbon fiber reinforced plastic with an integrated permeation barrier as its innermost layer. Alternating layers of permeation barrier and carbon fiber reinforced plastic may also be used. During manufacturing, the permeation barrier is sprayed on and integrated into the composite. The vessel, which is well-suited for high pressure gas storage is lighter weight than prior art vessels and has more usable volume than same-dimensioned prior art vessel. The permeation barrier encapsulates one or more ports or fittings of the vessel to reduce or eliminate the potential for gaps through which gas can escape. In one embodiment, a removable tooling process is employed in the manufacture of the vessel. In another embodiment, a permanent tooling process is employed and the tooling serves as a sorbent material for the vessel.

Claims

1. A liner-free pressure vessel comprising: a mandrel including a sorbent material; a composite shell formed about and surrounding the mandrel; the composite shell including: an innermost layer of impermeable film located immediately adjacent to the mandrel and surrounded by a layer of composite material; and a second layer of impermeable film surrounding the layer of composite material and being surrounded by a second layer of the composite material; a third layer of impermeable film surrounding the second layer of composite material and being surrounded by a third layer of the composite material; the impermeable film layers being integrated into the composite material layers during curing of the pressure vessel; wherein the composite shell and the mandrel comprise a monolithic structure, the mandrel being a permanent component of the pressure vessel; and wherein the pressure vessel does not include a plastic or metallic liner; and wherein when in an intended use of the pressure vessel the mandrel is adapted to adsorb natural gas.

2. A liner-free pressure vessel according to claim 1 wherein the impermeable film is a non-metallic material.

3. A liner-free pressure vessel according to claim 1 wherein the impermeable film includes metallic additives.

4. A liner-free pressure vessel according to claim 1 wherein the impermeable film is a polymer material.

5. A liner-free pressure vessel according to claim 1 wherein the composite material includes a carbon fiber roving and resin matrix.

6. A liner-free pressure vessel according to claim 1 further wherein a filament winding of said second layer of composite material is oriented at a different angle than a filament winding of said third layer of composite material.

7. A liner-free pressure vessel according to claim 1 wherein the pressure vessel is cylindrical shaped.

8. A liner-free pressure vessel according to claim 1 wherein the pressure vessel is non-cylindrical shaped.

9. A liner-free pressure vessel according to claim 1 wherein the pressure vessel is pressure-rated up to 10,000 psi.

10. A liner-free pressure vessel according to claim 1 wherein the pressure vessel has a useable storage volume in a range of 1 gallon to 10,000 gallons of its total volume.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is an enlarged cross-section view of a composite material made according to this invention and used to form the vessel shell. An impermeable film forms the most innermost layer to make a permeation barrier that eliminates the use of a liner. The composite shell of the vessel is formed using removable tooling (see FIGS. 3 and 4). The shell of the adsorbed natural gas (“ANG”) vessel is formed using a rigid porous structure as the mandrel, which forms a monolithic structure with the shell and serves as a sorbent (see FIGS. 6 and 7).

(2) FIG. 2 is a cross-section view of a preferred embodiment of pressure vessel or tank using the composite material of FIG. 1 and having been formed about removable tooling.

(3) FIG. 3 is a process flow diagram of a method of manufacturing the vessel of FIG. 2.

(4) Non-cylindrical shaped vessels can also be made using a non-cylindrical shaped mandrel.

(5) FIG. 4 is a schematic of the vessel of FIG. 2 as it is being manufactured using the process of FIG. 3.

(6) FIG. 5 is a cross-section view of a preferred embodiment of an ANG pressure vessel or tank made according to this invention and using the composite material of FIG. 1.

(7) FIG. 6 is a process flow diagram of a method of manufacturing the vessel of FIG. 5. Non-cylindrical shaped vessels can also be made using a non-cylindrical shaped mandrel made of the sorbent material.

(8) FIG. 7 is a schematic of the vessel of FIG. 5 as it is being manufactured using the process of FIG. 6.

(9) FIG. 8 is an isometric view of a preferred embodiment of the vessel main body made with removable tooling.

(10) FIG. 9 is an isometric view of a preferred embodiment of the vessel main body made with permanent tooling, the tooling serving as a sorbent for the vessel.

(11) FIG. 10 is an enlarged cross-section view of an alternate embodiment of a composite material made according to this invention and used to form the vessel shell. An impermeable film forms the most innermost layer to make a permeation barrier that eliminates the use of a liner. A second (next outermost) layer is comprised of a carbon fiber roving and resin or its equivalent. The next layer is formed by the impermeable film which, in turn, is covered by another layer of carbon fiber and roving.

ELEMENTS AND NUMBERING USED IN THE DRAWINGS

(12) 10 Composite material of vessel shell 11 First or innermost layer or layers 13 Impermeable film 15 Second or next outermost layer or layers 20 Liner-less, all-composite pressure vessel formed from removable tooling 21 Shell 23 Fitting or fittings 30 Disposable mandrel 31 Main body 33 End or ends 41 Assembled vessel structure (shell, fitting, and mandrel combination) 50 Liner-less, all-composite ANG pressure vessel 51 Shell 53 Fitting or fittings 60 Sorbent mandrel 61 Main body or core 63 End or ends 101 Molding step 103 Molding step 105 Mandrel assembly step 107 First layer application step 109 Second layer application step 111 Curing step 113 Post curing step 115 Mandrel removing step

DETAILED DESCRIPTION OF THE INVENTION

(13) A composite vessel made according to this invention is especially well-suited for use in high-pressure storage of gaseous matter such industrial and fuel gasses in compressed natural gas applications and compressed hydrogen fuel applications. A composite material made according to this invention also can be used in vessels to store other types of gasses, liquids and powders under pressure (or not under pressure) and can be used in one of its embodiments for adsorbed natural gas (“ANG”) applications.

(14) The pressure vessel includes a carbon fiber reinforced plastic with an integrated permeation barrier as its innermost layer. Alternating layers of permeation barrier and carbon fiber reinforced plastic may also be used for the vessel's shell. During manufacturing, the permeation barrier is sprayed on and integrated into (entrained in or drawn into) the composite. The vessel, which is well suited for high pressure gas storage is lighter weight than prior art vessels and has more usable volume than same-dimensioned prior art vessel. The permeation barrier encapsulates one or more ports or fittings of the vessel to reduce or eliminate the potential for gaps through which gas can escape. In one embodiment, a removable tooling process is employed in the manufacture of the vessel. In another embodiment, a permanent tooling process is employed and the tooling serves as a sorbent material for the vessel.

First Preferred Embodiment—Non-ANG Pressure Vessel (Removable Tooling)

(15) Referring to FIGS. 1, 4, 8 and 9, the composite material 10 of the vessels 20, 50 includes a first (innermost layer or layers) 11 comprised of an impermeable film 13 such as, but not limited to, a thin polymer material film. There can be more than one layer 11 of impermeable film 13 and, in a preferred embodiment, up to three layers 11 of film 13. The vessels 20, 50 also include a second (next outermost) layer or layers 15 comprised of carbon fiber roving and resin. Nano-additives may be added to the resin matrix used in one or more of the layers 15 (see e.g., Seshasai Gandikota, Selective toughening of carbon/epoxy composites using graphene oxide. Master's Thesis, Oklahoma State University (December 2011), hereby incorporated by reference).

(16) Alternatively, composite material 10 can include alternating layers of the impermeable film layer 13 and carbon fiber roving and resin layer 15 (see FIG. 10). The impermeable film 13 forms the most innermost layer 11 to make a permeation barrier that eliminates the use of a liner. A second (next outermost) layer 15 is comprised of a carbon fiber roving and resin or its equivalent. The next layer is formed by the impermeable film which, in turn, is covered by another layer of carbon fiber and roving. Preferably, there are three pairs of film and composite material layers 13, 15.

(17) Referring to FIGS. 2 and 3, the process of making the vessel 20 out of material 10 includes the steps 101, 103 of molding disposable ceramic mandrel components—core 31 and ends 33—and drying the components 31, 33. The mandrel components 31, 33 also could be formed by machining rather than molding and may be any shape preferable such as but not limited to a flatter, non-cylindrical shaped mandrel 30. The dried mandrel components 31, 33 are then assembled together in an assembly step 105 to form the mandrel 30. The mandrel components 31, 33 may be any shape preferable such as but not limited to a flatter, non-cylindrical shaped mandrel 30.

(18) A first application step 107 applies one or more layers 11 of impermeable film 13 to the fittings 23 and mandrel 30 to create a seamless barrier. Preferably, the film 13 is applied manually or by spraying. A second application step 109 makes use of a filament winder (not shown) and applies one or more layers 15 of carbon fiber roving and resin at preprogrammed angles to fully encapsulate, and bond to, the layer or layers 11 of impermeable film 13. Preferably, each layer 15 is applied at a different preprogrammed angle than its adjacent layer 15 or 11 (see e.g. FIG. 1). For example, one layer 15 can be at a first angle, another layer 15 at a second different angle from the first, and still another layer 15 at a third different angle from the first and second angles.

(19) The assembled structure 41 consisting of the shell 21, fittings 23, and mandrel 30 is removed from the filament winder and cured, preferably at room temperature for about 4 hours, during a curing step 111. A post-curing step 113 then takes place in an oven at a desired temperature and duration.

(20) A mandrel removing step 115 is accomplished by removing the post-cured material 37 from the oven and flushing the mandrel 30 with warm water, thereby removing the mandrel.

Second Preferred Embodiment—ANG Pressure Vessel (Permanent Tooling)

(21) Referring to FIGS. 5 and 6, the process of making an ANG pressure vessel 50 out of material 10 includes the steps 101, 103 of molding or forming a rigid porous structure—such as an activated carbon or its equivalent—into mandrel core and ends 61, 63 and drying the components 61, 63. The mandrel components 31, 33 also could be formed by machining rather than molding and may be any shape preferable such as but not limited to a flatter, non-cylindrical shaped mandrel 60. The dried mandrel components 61, 63 are then assembled together in an assembly step 105 to form the mandrel 60.

(22) A first application step 107 applies an impermeable film 11 to the fittings 53 and mandrel 60 to create a seamless barrier. Preferably, the film 13 is applied manually. A second application step 109 makes use of a filament winder (not shown) and applies carbon fiber roving and resin layer 15 at preprogrammed angles to fully encapsulate, and bond to, the layer or layers 11 of impermeable film 13. Each layer 15 is preferably at a different preprogrammed angle than its adjacent layer 15 or 11 (see e.g. FIG. 1). Similar to the first embodiment, one layer 15 can be at a first angle, another layer 15 at a second different angle from the first, and still another layer 15 at a third different angle from the first and second angles.

(23) The assembled structure 71 consisting of shell 51, fittings 51, and sorbent mandrel 60 is removed from the filament winder and cured, preferably at room temperature for about 4 hours, during a curing step 111. A post-curing step 113 then takes place in an oven at a desired temperature and duration.

(24) The mandrel 60 remains a part of the vessel 50.

(25) Preferred embodiments of the pressure vessel have been described so as to enable of person of ordinary skill in the art to make and use the invention, which is defined by the claims listed below. The claims cover designs that substitute one or more of the elements listed with equivalent elements.