Fiber structure, pressure container, and method of producing fiber structure
11092287 ยท 2021-08-17
Assignee
Inventors
Cpc classification
F17C2203/0668
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/0604
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/066
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/0665
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/0123
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B65H54/16
PERFORMING OPERATIONS; TRANSPORTING
F17C1/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/036
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2221/012
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2270/0168
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2209/2154
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16J12/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/0663
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/0109
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/0673
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/056
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2221/014
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E60/32
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F17C2221/033
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/0104
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
A fiber structure that includes a liner, and a fiber reinforcement base material formed of a fabric. The fiber reinforcement base material externally covers a body portion and a dome-shaped portion of the liner, and includes first yarns and second yarns. The first yarns are arranged such that a direction in which a yarn main axis of each of the first yarns in the body portion and the dome-shaped portion proceeds is a circumferential direction of the liner. The second yarns are arranged such that a direction in which a yarn main axis of each of the second yarns in the body portion proceeds is an axial direction of the body portion and that a direction in which a yarn main axis of a portion of each of the second yarns arranged in the dome-shaped portion proceeds is an axial direction of the dome-shaped portion.
Claims
1. A fiber structure, comprising: a liner including: a body portion having a cylindrical shape; a dome-shaped portion being continuous with at least one end of the body portion in an axial direction thereof; and a mouthpiece having a shape protruding from the dome-shaped portion in the axial direction of the body portion; and a fiber reinforcement base material formed of a fabric, the fiber reinforcement base material externally and entirely covering the body portion and the dome-shaped portion of the liner, wherein the fiber reinforcement base material includes: first yarns arranged in such a way that a direction in which a yarn main axis of each of the first yarns in the body portion and the dome-shaped portion proceeds is a circumferential direction of the liner; and second yarns forming the fabric with the first yarns, the second yarns being arranged in such a way that a direction in which a yarn main axis of each of the second yarns in the body portion proceeds is the axial direction of the body portion and that a direction in which a yarn main axis of a portion of each of the second yarns arranged in the dome-shaped portion proceeds is an axial direction of the dome-shaped portion.
2. The fiber structure according to claim 1, wherein the fabric is a multi-layered fabric comprising: a first yarn layer in which the first yarns are arranged; a second yarn layer in which the second yarns are arranged; and a binder yarn binding the first yarn layer and the second yarn layer.
3. A pressure container, comprising: a fiber structure impregnated with a matrix resin, the fiber structure including: a fiber reinforcement base material formed of a fabric, the fiber reinforcement base material externally covering a liner, wherein the fiber structure is the fiber structure according to claim 1 impregnated with a matrix resin.
4. A method of producing a fiber structure, the fiber structure comprising: a liner including: a body portion having a cylindrical shape; a dome-shaped portion being continuous with at least one end of the body portion in an axial direction thereof; and a mouthpiece having a shape protruding from the dome-shaped portion in the axial direction of the body portion; and a fiber reinforcement base material formed of a fabric, the fiber reinforcement base material externally covering the body portion and the dome-shaped portion of the liner; warp yarns arranged in such a way that a direction in which a yarn main axis of each of the warp yarns in the body portion and the dome-shaped portion proceeds is a circumferential direction of the liner; and weft yarns forming the fabric with the warp yarns, wherein the method of producing the fiber structure comprising: arranging the warp yarns along the axial direction of the body portion and the dome-shaped portion of the liner; inserting each of the weft yarns into a shed formed between the warp yarns adjacent to each other in the axial direction of the liner; pressing the inserted weft yarn toward the liner by beating with a reed to weave the fabric out of the warp yarns and the weft yarns; and winding the woven fabric around the liner by rotating the liner around a center axis of the liner.
5. The fiber structure according to claim 1, wherein the second yarns are arranged in such a way that an end of each of the second yarns in the body portion is continuous with each of the second yarns arranged in the dome-shaped portion in the axial direction of the liner.
Description
BRIEF DESCRIPTION OF DRAWINGS
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DESCRIPTION OF EMBODIMENTS
(11) A fiber structure, a pressure container, and a method of producing the fiber structure will now be described with reference to an embodiment that embodies the fiber structure used in a high-pressure tank, the high-pressure tank, and a method of producing the fiber structure, shown in
(12) As shown in
(13) The liner 12 is made of resin, and has an elongated hollow shape. A direction in which a center axis L of the liner 12 extends is referred to as an axial direction. The liner 12 includes a cylindrical body portion 13. A center axis of the body portion 13 coincides with the center axis L of the liner 12. The liner 12 includes a dome-shaped portion 14 at each of both ends of the body portion 13 in an axial direction Y. An axial direction of each of the dome-shaped portions 14 coincides with the axial direction of the liner 12. The liner 12 includes a mouthpiece 15 that outwardly protrudes from each of the dome-shaped portions 14 in the axial direction Y. The mouthpieces 15 are made of metal (e.g. stainless steel). Each of the mouthpieces 15 includes a hole portion 16 that communicates with a space in the liner 12. A valve 17 is fitted into the hole portion 16 of one of the mouthpieces 15 at one end of the liner 12 in the axial direction Y, and a screw 18 is screwed into the hole portion 16 of the other of the mouthpieces 15 at the other end of the liner 12 in the axial direction Y.
(14) The fiber reinforcement base material 19 uses a carbon fiber as a reinforcement fiber according to the present embodiment. The reinforcement fiber is not limited to the carbon fiber, but other reinforcement fibers that are generally said to have high elasticity and high strength may be used, such as glass fibers, silicon-carbide base ceramic fibers, aramid fibers, and ultra-high molecular weight polyethylene fibers.
(15) As shown in
(16) The plurality of weft yarns 23 are arranged parallel to one another, along the circumferential direction Z of the liner 12. A portion of each of the weft yarns 23 that proceeds ahead in the axial direction of the liner 12 along the outer peripheral surface of the body portion 13 is a body-portion weft yarn 23a. A portion of each of the weft yarns 23 that proceeds in the axial direction of the liner 12 along each of the outer peripheral surfaces of each of the dome-shaped portions 14 is a dome-portion weft yarn 23b. Each end of the body-portion weft yarn 23a is continuous with each of the dome-portion weft yarns 23b in the axial direction of the liner 12. As to the weft yarns 23, a direction X2 in which a yarn main axis of each of the dome-portion weft yarns 23b proceeds is the axial direction of the liner 12, curving along the each of the curved surfaces of each of the dome-shaped portions 14. Also as to the weft yarns 23, the direction X2 in which a yarn main axis of each of the body-portion weft yarns 23a proceeds is the axial direction of the body portion 13 of the liner 12.
(17) Each of the warp yarns 22 and each of the weft yarns 23 are arranged orthogonal to each other. By making the direction X1 in which the yarn main axis of the warp yarns 22 proceeds coincide with the circumferential direction Z of the liner 12, the liner 12 is reinforced in the radial direction. By making the direction X2 in which the yarn main axis of the weft yarns 23 proceeds coincide with the axial direction of the liner 12, the liner 12 is reinforced in the axial direction.
(18) As shown in
(19) A method of producing a high-pressure tank 10 will now be described.
(20) In producing the high-pressure tank 10, the woven fabric 24 is wound around the liner 12 while the warp yarns 22 and the weft yarns 23 are woven with the plain weave.
(21) As shown in
(22) In weaving the fiber reinforcement base material 19 with the plain-weave loom described above, the ends of a plurality of warp yarns 22a and a plurality of warp yarns 22b that are drawn out of the warp beams 32 and 33 respectively are fixed to the outer peripheral surface of the liner 12 using a fixing member 36 made of, for example, an adhesive tape, as shown in
(23) By alternately shifting to raise and lower the heddle frames 31a and 31b without rotating the liner 12, the heddle frame 31a, the one of the heddle frames, and the heddle frame 31b, the other of the heddle frames, are shifted in the directions opposite to each other. Then, each of the weft yarns 23 is inserted into a warp shed 37 formed between the warp yarns 22a and 22b every time the warp yarns 22a and 22b adjacent to each other are alternately raised and lowered. The weft yarns 23 have a flat shape after inserted.
(24) Each of the weft yarns 23 is inserted and beaten with the reed 34. Then, the heddle frames 31a and 31b are shifted in the directions opposite to each other so that the shedding state is changed. Subsequently, the next weft insertion is performed. These series of actions described above are repeated so that part of the fabric 24 is woven with the plain weave out of the warp yarns 22 and the weft yarns 23 and the part of the fabric 24 is integrated with the liner 12 into a single piece.
(25) As shown in
(26) Subsequently, as shown in
(27) In the fiber structure 21 configured as described above, the fiber-reinforced composite layer 11 is formed of the fiber reinforcement base material 19 with the matrix resin Ma impregnated thereinto and hardened, and then, the high-pressure tank 10 is produced with the liner 12 externally covered with the fiber-reinforced composite layer 11. For impregnating and hardening the matrix resin Ma, the resin transfer molding (RTM) method, for example, is used.
(28) The operation of a high-pressure tank 10 will now be described.
(29) The high-pressure tank 10 is used, for example, as a hydrogen-supply source for fuel cells of a fuel cell vehicle. The high-pressure tank 10 is used in a state where a pipe (not shown) is connected to the valve 17. Hydrogen gas is filled into the high-pressure tank 10 through the pipe for filling the hydrogen gas. In the high-pressure tank 10, the hydrogen gas that may have a pressure as high as several tens of MPa, for example, is filled.
(30) When the hydrogen gas is filled into the high-pressure tank 10, the pressure in the high-pressure tank 10 increases so that the liner 12 is pressed from the inside. Great forces are exerted on the liner 12 in the axial direction Y and the radial direction, by which an internal pressure stress is generated. According to the present embodiment, the liner 12 is reinforced in the axial direction by the weft yarns 23 and is reinforced in the radial direction by the warp yarns 22, which suppresses deformation in the high-pressure tank 10.
(31) The above-described embodiment has the following advantages.
(32) (1) In the fiber structure 21 that forms the high-pressure tank 10, the direction X2 in which the yarn main axis of the weft yarns 23 proceeds coincides with the axial direction Y of the body portion 13 and the dome-shaped portions 14. The weft yarns 23 thereby reinforce the liner 12 in the axial direction.
(33) (2) The direction X2 in which the yarn main axis of the weft yarns 23 proceeds curves along the curved surfaces of the dome-shaped portions 14 of the liner 12 toward the axial direction Y in the dome-shaped portion 14. In this state, the weft yarns 23 are not angled relative to the axial direction Y. Even the dome-shaped portion 14 is thereby reinforced in the axial direction Y.
(34) (3) The weft yarn 23 that is just inserted is beaten with the reed 34 to be sent to the weft yarn 23 that has been previously inserted, which allows the weft yarns 23 to be arranged closely one another along the circumferential direction Z of the liner 12. In the dome-shaped portions 14 that have smaller diameters than the body portion 13 has, the weft yarns 23 are beaten and pressed by the reed 34, which allows the weft yarns 23 to be arranged parallel to one another even in the dome-shaped portions 14 and which also prevents from generating wrinkles. The density of the weft yarns 23 is thereby the same in the body portion 13 and the dome-shaped portions 14, and wrinkles are prevented from being generated in the fiber structure 21 even on the curved surfaces of the dome-shaped portions 14.
(35) (4) An example of a conventional method of producing the fiber structure 21 that includes the fiber reinforcement base material 19 externally covering the liner 12 may be filament winding. In this method, productivity is low because yarns are wound around the liner 12 individually one by one. On the other hand, the productivity in producing the fiber structure 21 according to the present embodiment is enhanced as compared to the filament winding, because the fabric 24 is wound around the liner 12 while the fabric 24 is woven out of the warp yarns 22 and the weft yarns 23.
(36) Another example of a conventional method of producing the fiber structure 21 that includes the fiber reinforcement base material 19 on the outer peripheral surface of the liner 12 may be braiding, in which a fabric is woven into a tubular shape to fit to the shape of the liner 12 by braiding, cut open into a flat shape, and then wound around the liner 12, In contrast to this conventional method, the fiber reinforcement base material 19 according to the present embodiment is wound around the liner 12 while the fiber reinforcement base material 19 is woven out of the warp yarns 22 and the weft yarns 23, which does not require an individual process to weave the fabric, a process to cut open the fabric, and a process to paste the fabric to the liner. Productivity is thereby enhanced as compared to the braiding. The liner 12 according to the present embodiment is reinforced in the axial direction because the direction X2 in which the yarn main axis of the weft yarns 23 proceeds is the axial direction of the liner 12.
(37) The following modifications may be made to the embodiment described above. As shown in
(38) In a fiber structure 46 including the fiber reinforcement base material 40 described above, a matrix resin (not shown) is impregnated along the binder yarn 45 into the fiber reinforcement base material 40 through the stacking direction of the fiber reinforcement base material 40. The fiber structure 46 is thereby reinforced also in the stacking direction. The number of the warp layers and the weft layers may be appropriately changed.
(39) In the embodiment described above, the fiber reinforcement base material 19 includes the stacked layers of the fabric 24 that is woven with the plain weave. The scope of the present invention is not limited to the embodiment described above. For example, the fiber reinforcement base material 19 may include the stacked layers of a fabric that is woven with a satin weave or a twill weave out of a plurality of the warp yarns 22 corresponding to the first yarns and a plurality of the weft yarns 23 corresponding to the second yarns.
(40) In the embodiment described above, the warp yarn 22 is referred to as the first yarn, and the weft yarn 23 is referred to as the second yarn. However, the weft yarn 23 may be referred to as the first yarn and the warp yarn 22 may be referred to as the second yarn.
(41) The liner 12 may have a shape in which one end of the body portion 13 in the axial direction Y is continuous with the dome-shaped portion 14 and the other end of the body portion 13 in the axial direction Y is continuous with a flat bottom surface. In this case, the mouthpiece 15 is provided only to the one end of the line 12 in the axial direction Y where the dome-shaped portion 14 is disposed.
(42) The liner 12 may be entirely made of aluminum or aluminum alloy. The mouthpiece 15 may be made of metal other than stainless steel.
(43) The body portion 13 and the dome-shaped portions 14 of the liner 12 may be welded into a single piece, instead of being separated.
(44) The high-pressure tank 10 in the embodiment described above is used as a hydrogen-supply source for fuel cells to be mounted on a fuel cell vehicle. The scope of the present invention is not limited to the embodiment. For example, the high-pressure tank 10 may be used as a hydrogen-supply source to power a hydrogen engine or may be used for a heat pump. Alternatively, the high-pressure tank 10 may be used as a hydrogen-supply source for fuel cells for household use.
(45) The high-pressure tank 10 in the embodiment described above is used to store hydrogen as the pressure container. The scope of the present invention is not limited to the embodiment. For example, the pressure container may be used to store other types of gases such as nitrogen and compressed natural gas.
REFERENCE SIGNS LIST
(46) L center axis Y axial direction Z circumferential direction Ma matrix resin X1, X2 direction of yarn main axis 10 high-pressure tank as pressure container 12 liner 13 body portion 14 dome-shaped portion 15 mouthpiece 19, 40 fiber reinforcement base material 21, 46 fiber structure 22 warp yarn as first yarn 23 weft yarn as second yarn 24 fabric 41, 42 warp layer as first yarn layer 43 weft layer as second yarn layer 45 binder yarn