EP4155600A1 - Fuel tank - Google Patents
Fuel tank Download PDFInfo
- Publication number
- EP4155600A1 EP4155600A1 EP20936089.0A EP20936089A EP4155600A1 EP 4155600 A1 EP4155600 A1 EP 4155600A1 EP 20936089 A EP20936089 A EP 20936089A EP 4155600 A1 EP4155600 A1 EP 4155600A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- internal
- holes
- strut
- fuel tank
- internal strut
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 239000002828 fuel tank Substances 0.000 title claims abstract description 19
- 230000008878 coupling Effects 0.000 claims abstract description 39
- 238000010168 coupling process Methods 0.000 claims abstract description 39
- 238000005859 coupling reaction Methods 0.000 claims abstract description 39
- 238000003466 welding Methods 0.000 claims abstract description 11
- 229920005989 resin Polymers 0.000 claims abstract description 5
- 239000011347 resin Substances 0.000 claims abstract description 5
- 238000010276 construction Methods 0.000 description 6
- 229920005992 thermoplastic resin Polymers 0.000 description 5
- 238000000034 method Methods 0.000 description 3
- 230000033001 locomotion Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000004698 Polyethylene Substances 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 239000012141 concentrate Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- -1 for example Substances 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 229920001903 high density polyethylene Polymers 0.000 description 1
- 239000004700 high-density polyethylene Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C1/00—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge
- F17C1/16—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of plastics materials
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/01—Shape
- F17C2201/0147—Shape complex
- F17C2201/0157—Polygonal
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/05—Size
- F17C2201/056—Small (<1 m3)
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/01—Reinforcing or suspension means
- F17C2203/011—Reinforcing means
- F17C2203/013—Reinforcing means in the vessel, e.g. columns
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0602—Wall structures; Special features thereof
- F17C2203/0612—Wall structures
- F17C2203/0614—Single wall
- F17C2203/0621—Single wall with three layers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0634—Materials for walls or layers thereof
- F17C2203/0658—Synthetics
- F17C2203/066—Plastics
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/068—Special properties of materials for vessel walls
- F17C2203/0682—Special properties of materials for vessel walls with liquid or gas layer
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2209/00—Vessel construction, in particular methods of manufacturing
- F17C2209/22—Assembling processes
- F17C2209/221—Welding
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/01—Improving mechanical properties or manufacturing
- F17C2260/011—Improving strength
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2270/00—Applications
- F17C2270/01—Applications for fluid transport or storage
- F17C2270/0165—Applications for fluid transport or storage on the road
- F17C2270/0168—Applications for fluid transport or storage on the road by vehicles
Definitions
- the present invention relates to a resinous fuel tank.
- a technique for supporting walls that face each other in a tank body with an internal strut is known.
- walls of the tank body can deform toward outside or inside the fuel tank due to internal pressure variation.
- the internal strut has no elasticity, stress tends to concentrate on welded parts between the tank body and the internal strut. In some cases, there is a risk that the welded parts crack or a risk that the internal strut buckles.
- Patent Document 1 describes a technique for providing an internal strut with a lobe that elastically deforms easily. According to this technique, when walls of a tank body deform toward outside or inside a fuel tank, the lobe flexes to absorb the amount of deformation of the tank body. This reduces concentration of stress on the welded parts.
- Patent Document 1 U.S. Patent No. 6338420B1
- a fuel tank made of a resin includes: a tank body that has walls facing each other therein; and an internal strut including both ends fixed to the facing walls respectively.
- the internal strut has a grid shape such that through holes are arranged as viewed from a side.
- an internal strut has a grid shape such that through holes are arranged as viewed from the side. Therefore, as compared to an internal strut partially including a portion that elastically deforms easily, the internal strut enhances in the rigidity.
- the grid structure has a portion around each of the through holes flexed in the axis direction.
- the through holes are hexagonal holes.
- the grid shape is a honeycomb shape and thus both high rigidity and excellent elasticity of the internal strut are achieved.
- the internal strut has circular welding faces welded to the walls on both ends of the internal strut respectively having a substantially cylindrical shape.
- the internal strut when the internal strut is formed in a substantially cylindrical shape having circular welding face parts on both ends thereof, respectively, the load applied to the welded parts or the internal strut is transmitted uniformly around the axis. This construction reduces excessive stress concentration on the internal strut.
- the internal strut is two or more internal struts and the fuel tank further includes a coupling part coupling neighboring internal struts to each other.
- the coupling part that couples the internal struts to each other is provided, and if an excessive force is applied to one of the internal struts, the coupling part transmits the excessive force to the other internal strut through the coupling part.
- the coupling part is located away from both ends of the internal struts.
- the coupling part is provided at a region highly elastic due to the grid shape, and thus stress concentration on the coupling part is reduced.
- the coupling part has coupling through holes extending therethrough in the same direction as the through holes extend, and the coupling through holes are arranged side by side in axial directions of the internal struts.
- the elasticity of the coupling part itself is ensured and the coupling part is expanded and contracted according to expanding and contracting motions of the internal struts. This construction further reduces the stress concentration on the coupling part.
- the elasticity and the rigidity of the internal strut is ensured in a balanced manner.
- a fuel tank 1 includes an internal strut 3 that has both ends respectively fixed to walls 2A and 2B facing each other inside a resinous tank body 2.
- the tank body 2 has a layer structure which includes, for example, a multilayer sectional structure including a barrier layer made of a material highly impermeable to a fuel interposed between an inside thermoplastic resin layer forming the inner surface of the tank and an outside thermoplastic resin layer forming the outer surface of the tank.
- the inside thermoplastic resin layer and the outside thermoplastic resin layer are made of materials, for example, PE (high-density polyethylene) having high thermofusibility and high moldability.
- PE high-density polyethylene
- the internal strut 3 has a grid shape in which through holes 4 are arranged adjacent to each other as viewed from the side (in a direction P orthogonal to the direction of an axis O of the internal strut 3).
- the through holes 4 are also arranged adjacent to each other in the vertical section of the internal strut 3 (section orthogonal to the directions of axis O and axis P).
- the internal strut 3 in the grid shape increases the rigidity of the internal strut 3 as compared to the conventional structure including an elastic portion provided in some part.
- the internal strut 3 ensures both the elasticity and the rigidity in a balanced manner and reduces the stress concentration on welded parts between the tank body 2 and the internal strut 3. Further, flexing of the internal strut 3 also reduces the risk of the buckling of the internal strut 3.
- the internal strut 3 includes a strut central part 6 having the through holes 4 provided thereon, and welding face parts 8 formed on both the ends of the strut central part 6 with strut end parts 7 interposed therebetween, respectively, and has a substantially cylindrical shape as a whole.
- the internal strut 3 is made of a resin and the strut central part 6, the strut end parts 7, and the welding face parts 8 are molded integrally.
- the through holes 4 are hexagonal holes 9. That is, the strut central part 6 of the internal strut 3 has a honeycomb structure.
- the hexagonal holes 9 are arranged in three lines extending in the direction of the axis O.
- the hexagonal holes 9 are arranged in a grid such that lines connecting the centers of the adjacent three hexagonal holes 9 define a triangular grid.
- lines connecting the centers of the adjacent three hexagonal holes 9 define a regular triangular grid.
- the grid wall 5 near the circumferential surface of the strut central part 6 is formed as accordion-like planes 10.
- the strut central part 6 has a substantially cylindrical shape as a whole.
- the welding face parts 8 are formed as a circular plate.
- the welding face parts 8 have arc ribs 12 formed thereon concentrically on the axis O.
- the arc ribs 12 each located on the same circumferential line are formed with cuts. Provision of these arc ribs 12 enables resin of the tank body 2 to come around the arc ribs 12 during thermal welding and therefore improves the weldability between the tank body 2 and the internal strut 3.
- the through holes 4 are the hexagonal holes 9 and accordingly the internal strut 3 has a honeycomb structure. Therefore, both high rigidity and excellent elasticity of the internal strut 3 are provided.
- the internal strut 3 in a substantially cylindrical shape, having the circular welding face parts 8 on the both ends, respectively, enables the load applied to the welded parts or the internal strut 3 to be transmitted uniformly around the axis O. This construction reduces excessive stress concentration on the internal strut 3.
- two internal struts 3 are coupled with a coupling part 13 as illustrated in FIGS. 4 and 5 .
- the coupling part 13 is provided at a midpoint of the internal struts 3 away from the both ends of the internal struts 3, specifically, on the strut central parts 6.
- the coupling part 13 is formed of rectangular plate-like parts as viewed in the direction of the axis O, which couples the planes 10 of the respective internal struts 3 to each other.
- the plate-like parts are placed to be spaced in the direction of the axis O.
- the coupling part 13 has hexagonal coupling through holes 14 extending therethrough in the same direction as the hexagonal holes 9 extend, that is, in the direction P and being arranged side by side in the directions of the axes O of the internal struts 3.
- the coupling part 13 coupling the internal struts 3 to each other makes the excessive force transmitted to the other internal strut 3 through the coupling part 13.
- the coupling part 13 With the coupling part 13 provided at a midpoint of the internal struts 3 away from the both ends of the internal struts 3, the coupling part 13 is placed at a region being highly elastic due to the grid shape and stress concentration on the coupling part 13 is reduced.
- the coupling part 13 includes the coupling through holes 14 extending therethrough in the same direction as the hexagonal holes 9 and being arranged side by side in the directions of the axes O of the internal struts 3, the elasticity of the coupling part 13 itself is ensured and the coupling part 13 is expanded and contracted according to expanding and contracting motions of the internal struts 3. This construction further reduces the stress concentration around the coupling part 13.
- the through holes 4 are not limited to the hexagonal holes 9 and may be circular holes 15 illustrated in FIG. 6 , triangular holes 16 illustrated in FIG. 7 , or the like as long as these holes are arranged in a grid.
- the circular holes 15 are arranged in a grid such that lines connecting the centers of the adjacent three circular holes 15 define a regular triangular grid.
- the triangular holes 16 are arranged in a grid such that lines connecting the centers of the adjacent six triangular holes 16 define a hexagonal grid.
- the triangular holes 16 each are a regular triangle, the lines connecting the centers of the adjacent six triangular holes 16 define regular hexagonal grid.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Abstract
Description
- The present invention relates to a resinous fuel tank.
- As a resinous fuel tank, a technique for supporting walls that face each other in a tank body with an internal strut is known. In a fuel tank, walls of the tank body can deform toward outside or inside the fuel tank due to internal pressure variation. At this time, if the internal strut has no elasticity, stress tends to concentrate on welded parts between the tank body and the internal strut. In some cases, there is a risk that the welded parts crack or a risk that the internal strut buckles.
- To solve this problem,
Patent Document 1 describes a technique for providing an internal strut with a lobe that elastically deforms easily. According to this technique, when walls of a tank body deform toward outside or inside a fuel tank, the lobe flexes to absorb the amount of deformation of the tank body. This reduces concentration of stress on the welded parts. - Patent Document 1:
U.S. Patent No. 6338420B1 - Meanwhile, in a case where a portion that elastically deforms easily is provided in some part, there is a problem that the strut tends to lack rigidity. Therefore, an internal strut that has high-level elasticity and rigidity at the same time in a balanced manner is demanded.
- According to a first aspect of the present invention, a fuel tank made of a resin includes: a tank body that has walls facing each other therein; and an internal strut including both ends fixed to the facing walls respectively. The internal strut has a grid shape such that through holes are arranged as viewed from a side.
- According to the first aspect of the present invention, an internal strut has a grid shape such that through holes are arranged as viewed from the side. Therefore, as compared to an internal strut partially including a portion that elastically deforms easily, the internal strut enhances in the rigidity. When walls of a tank body are deformed outward or inward due to internal pressure variation of the tank body and a tensile or compressive force is applied to the internal strut in the axis direction, the grid structure has a portion around each of the through holes flexed in the axis direction. This construction of the internal strut of the present invention ensures the elasticity and the rigidity in a balanced manner and reduces stress concentration on welded parts between the tank body and the internal strut.
- According to a second aspect, the through holes are hexagonal holes.
- According to the second aspect, the grid shape is a honeycomb shape and thus both high rigidity and excellent elasticity of the internal strut are achieved.
- According to a third aspect, the internal strut has circular welding faces welded to the walls on both ends of the internal strut respectively having a substantially cylindrical shape.
- According to the third aspect, when the internal strut is formed in a substantially cylindrical shape having circular welding face parts on both ends thereof, respectively, the load applied to the welded parts or the internal strut is transmitted uniformly around the axis. This construction reduces excessive stress concentration on the internal strut.
- According to a fourth aspect, the internal strut is two or more internal struts and the fuel tank further includes a coupling part coupling neighboring internal struts to each other.
- According to the fourth aspect, the coupling part that couples the internal struts to each other is provided, and if an excessive force is applied to one of the internal struts, the coupling part transmits the excessive force to the other internal strut through the coupling part.
- According to a fifth aspect, the coupling part is located away from both ends of the internal struts.
- According to the fifth aspect, the coupling part is provided at a region highly elastic due to the grid shape, and thus stress concentration on the coupling part is reduced.
- According to a sixth aspect, the coupling part has coupling through holes extending therethrough in the same direction as the through holes extend, and the coupling through holes are arranged side by side in axial directions of the internal struts.
- According to the sixth aspect, the elasticity of the coupling part itself is ensured and the coupling part is expanded and contracted according to expanding and contracting motions of the internal struts. This construction further reduces the stress concentration on the coupling part.
- According to the present invention, when the stress concentration on the welded parts between the tank body and the internal strut is reduced during deformation of the tank body, the elasticity and the rigidity of the internal strut is ensured in a balanced manner.
-
-
FIG. 1 is a side sectional view of a fuel tank according to the present invention; -
FIG. 2 is a side view of an internal strut according to a first embodiment; -
FIG. 3 is an external perspective view of the internal strut according to the first embodiment; -
FIG. 4 is a side view of internal struts according to a second embodiment; -
FIG. 5 is an external perspective view of the internal struts according to the second embodiment; -
FIG. 6 is a side view of an internal strut having circular holes as through holes; and -
FIG. 7 is a side view of an internal strut having triangular holes as through holes. - As illustrated in
FIG. 1 , afuel tank 1 includes aninternal strut 3 that has both ends respectively fixed towalls resinous tank body 2. Thetank body 2 has a layer structure which includes, for example, a multilayer sectional structure including a barrier layer made of a material highly impermeable to a fuel interposed between an inside thermoplastic resin layer forming the inner surface of the tank and an outside thermoplastic resin layer forming the outer surface of the tank. The inside thermoplastic resin layer and the outside thermoplastic resin layer are made of materials, for example, PE (high-density polyethylene) having high thermofusibility and high moldability. The both ends of theinternal strut 3 are thermally welded to the inside thermoplastic resin layer of thewalls - With reference also to
FIGS. 2 and3 , theinternal strut 3 has a grid shape in which through holes 4 are arranged adjacent to each other as viewed from the side (in a direction P orthogonal to the direction of an axis O of the internal strut 3). The through holes 4 are also arranged adjacent to each other in the vertical section of the internal strut 3 (section orthogonal to the directions of axis O and axis P). Theinternal strut 3 in the grid shape increases the rigidity of theinternal strut 3 as compared to the conventional structure including an elastic portion provided in some part. For example, if an internal pressure variation in thetank body 2 causes a tensile or compressive stress to be applied to theinternal strut 3 from thewalls grid wall 5 around each of the through holes 4 flexes in the direction of the axis O. This elastically deforms theinternal strut 3 in the direction of the axis O without occurrence of excessive stress concentration on it. That is, theinternal strut 3 according to the present invention ensures both the elasticity and the rigidity in a balanced manner and reduces the stress concentration on welded parts between thetank body 2 and theinternal strut 3. Further, flexing of theinternal strut 3 also reduces the risk of the buckling of theinternal strut 3. - Preferred embodiments of the
internal strut 3 are described below. - In
FIGS. 1 to 3 , theinternal strut 3 includes a strutcentral part 6 having the through holes 4 provided thereon, andwelding face parts 8 formed on both the ends of the strutcentral part 6 withstrut end parts 7 interposed therebetween, respectively, and has a substantially cylindrical shape as a whole. Theinternal strut 3 is made of a resin and the strutcentral part 6, thestrut end parts 7, and thewelding face parts 8 are molded integrally. - The through holes 4 are hexagonal holes 9. That is, the strut
central part 6 of theinternal strut 3 has a honeycomb structure. The hexagonal holes 9 are arranged in three lines extending in the direction of the axis O. The hexagonal holes 9 are arranged in a grid such that lines connecting the centers of the adjacent three hexagonal holes 9 define a triangular grid. When the hexagonal holes 9 each are a regular hexagon, lines connecting the centers of the adjacent three hexagonal holes 9 define a regular triangular grid. Thegrid wall 5 near the circumferential surface of the strutcentral part 6 is formed as accordion-like planes 10. Meanwhile, a part of each of the hexagonal holes 9 around an opening end is formed like an arc in a circumferential direction around the axis O as can be seen fromFIG. 3 . Accordingly, the strutcentral part 6 has a substantially cylindrical shape as a whole. - The welding face
parts 8 are formed as a circular plate. The welding faceparts 8 havearc ribs 12 formed thereon concentrically on the axis O. Thearc ribs 12 each located on the same circumferential line are formed with cuts. Provision of thesearc ribs 12 enables resin of thetank body 2 to come around thearc ribs 12 during thermal welding and therefore improves the weldability between thetank body 2 and theinternal strut 3. - According to the present embodiment, the through holes 4 are the hexagonal holes 9 and accordingly the
internal strut 3 has a honeycomb structure. Therefore, both high rigidity and excellent elasticity of theinternal strut 3 are provided. Theinternal strut 3 in a substantially cylindrical shape, having the circularwelding face parts 8 on the both ends, respectively, enables the load applied to the welded parts or theinternal strut 3 to be transmitted uniformly around the axis O. This construction reduces excessive stress concentration on theinternal strut 3. - In a second embodiment, two
internal struts 3 are coupled with acoupling part 13 as illustrated inFIGS. 4 and5 . Each of theinternal struts 3 has the same construction as that in the first embodiment, and descriptions thereof are omitted. Thecoupling part 13 is provided at a midpoint of theinternal struts 3 away from the both ends of theinternal struts 3, specifically, on the strutcentral parts 6. Thecoupling part 13 is formed of rectangular plate-like parts as viewed in the direction of the axis O, which couples theplanes 10 of the respectiveinternal struts 3 to each other. The plate-like parts are placed to be spaced in the direction of the axis O. Accordingly, thecoupling part 13 has hexagonal coupling throughholes 14 extending therethrough in the same direction as the hexagonal holes 9 extend, that is, in the direction P and being arranged side by side in the directions of the axes O of theinternal struts 3. - If an excessive force is applied on one of the
internal struts 3, thecoupling part 13 coupling theinternal struts 3 to each other makes the excessive force transmitted to the otherinternal strut 3 through thecoupling part 13. With thecoupling part 13 provided at a midpoint of theinternal struts 3 away from the both ends of theinternal struts 3, thecoupling part 13 is placed at a region being highly elastic due to the grid shape and stress concentration on thecoupling part 13 is reduced. Further, because thecoupling part 13 includes the coupling throughholes 14 extending therethrough in the same direction as the hexagonal holes 9 and being arranged side by side in the directions of the axes O of theinternal struts 3, the elasticity of thecoupling part 13 itself is ensured and thecoupling part 13 is expanded and contracted according to expanding and contracting motions of theinternal struts 3. This construction further reduces the stress concentration around thecoupling part 13. - Preferred embodiments of the present invention have been described above. The through holes 4 are not limited to the hexagonal holes 9 and may be circular holes 15 illustrated in
FIG. 6 , triangular holes 16 illustrated inFIG. 7 , or the like as long as these holes are arranged in a grid. Namely, in the present embodiment illustrated inFIG. 6 , the circular holes 15 are arranged in a grid such that lines connecting the centers of the adjacent three circular holes 15 define a regular triangular grid. In the present embodiment illustrated inFIG. 7 , the triangular holes 16 are arranged in a grid such that lines connecting the centers of the adjacent six triangular holes 16 define a hexagonal grid. When the triangular holes 16 each are a regular triangle, the lines connecting the centers of the adjacent six triangular holes 16 define regular hexagonal grid. - In the second embodiment, it is permissible to provide three or more
internal struts 3. -
- 1
- fuel tank
- 2
- tank body
- 3
- internal strut
- 4
- through hole
- 5
- grid wall
- 6
- strut central part
- 7
- strut end part
- 8
- welding face part
- 9
- hexagonal hole
- 13
- coupling part
- 14
- coupling through hole
Claims (6)
- A fuel tank made of a resin comprising:a tank body having walls facing each other therein;an internal strut including both ends fixed to the facing walls respectively;wherein the internal strut has a grid shape such that through holes are arranged as viewed from a side.
- The fuel tank according to Claim 1,
wherein the through holes are hexagonal holes. - The fuel tank according to Claim 1,
wherein the internal strut has circular welding faces welded to the walls on the both ends of the internal strut respectively, having a substantially cylindrical shape. - The fuel tank according to Claim 1,wherein the internal strut is two or more internal struts,the fuel tank further comprising a coupling part coupling neighboring internal struts to each other.
- The fuel tank according to Claim 4,
wherein coupling part is located away from both ends of the internal struts. - The fuel tank according to Claim 5,wherein the coupling part has coupling through holes extending therethrough in the same direction as the through holes extend, andwherein the coupling through holes are arranged side by side in axial directions of the internal struts.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/JP2020/020166 WO2021234921A1 (en) | 2020-05-21 | 2020-05-21 | Fuel tank |
Publications (2)
Publication Number | Publication Date |
---|---|
EP4155600A1 true EP4155600A1 (en) | 2023-03-29 |
EP4155600A4 EP4155600A4 (en) | 2024-02-28 |
Family
ID=78707856
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP20936089.0A Pending EP4155600A4 (en) | 2020-05-21 | 2020-05-21 | Fuel tank |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP4155600A4 (en) |
JP (1) | JP7274051B2 (en) |
CN (1) | CN115667780B (en) |
WO (1) | WO2021234921A1 (en) |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6338420B1 (en) | 1999-06-08 | 2002-01-15 | Delphi Technologies, Inc. | Motor vehicle fuel tank and method |
US20020066737A1 (en) * | 2000-12-05 | 2002-06-06 | Stack Gary Francis | Fuel tank |
JP4393155B2 (en) * | 2003-10-30 | 2010-01-06 | 株式会社豊田自動織機 | Pressure vessel |
JP4575107B2 (en) * | 2004-10-13 | 2010-11-04 | 株式会社豊田自動織機 | Pressure vessel |
DE102013003247A1 (en) * | 2013-02-27 | 2014-09-11 | Kautex Textron Gmbh & Co. Kg | Fuel tank |
JP5807661B2 (en) * | 2013-06-14 | 2015-11-10 | トヨタ自動車株式会社 | Fuel tank |
JP6519465B2 (en) * | 2015-12-25 | 2019-05-29 | トヨタ自動車株式会社 | Fuel tank |
CN205736926U (en) * | 2016-04-28 | 2016-11-30 | 株式会社久保田 | Fuel tank |
JP6700145B2 (en) | 2016-09-08 | 2020-05-27 | トヨタ自動車株式会社 | Fuel tank |
JP6835511B2 (en) * | 2016-09-09 | 2021-02-24 | トヨタ自動車株式会社 | Resin fuel tank |
CN110198858B (en) * | 2017-01-20 | 2022-06-17 | 日本制铁株式会社 | Fuel tank |
JP2018127123A (en) | 2017-02-09 | 2018-08-16 | 株式会社Fts | Support post component for vehicle fuel tank |
JP2019014292A (en) | 2017-07-04 | 2019-01-31 | 株式会社Fts | Internal column attachment structure |
WO2019207362A2 (en) * | 2018-04-24 | 2019-10-31 | 亚普汽车部件股份有限公司 | Support for connecting upper and lower surfaces inside fuel tank |
CN208544112U (en) * | 2018-04-24 | 2019-02-26 | 亚普汽车部件股份有限公司 | Connect the supporter of fuel tank internal upper and lower surface |
-
2020
- 2020-05-21 WO PCT/JP2020/020166 patent/WO2021234921A1/en unknown
- 2020-05-21 EP EP20936089.0A patent/EP4155600A4/en active Pending
- 2020-05-21 CN CN202080100905.XA patent/CN115667780B/en active Active
- 2020-05-21 JP JP2022524814A patent/JP7274051B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
EP4155600A4 (en) | 2024-02-28 |
JPWO2021234921A1 (en) | 2021-11-25 |
CN115667780A (en) | 2023-01-31 |
JP7274051B2 (en) | 2023-05-15 |
CN115667780B (en) | 2023-05-26 |
WO2021234921A1 (en) | 2021-11-25 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US9731866B2 (en) | Fuel tank with supporting element | |
KR20130084665A (en) | Structure for tank dome flange section | |
US11052754B2 (en) | Fuel tank | |
WO2014112236A1 (en) | Fuel tank structure | |
EP4155600A1 (en) | Fuel tank | |
JP4801891B2 (en) | Fuel tank | |
JP2017106304A (en) | Segments | |
KR20000075397A (en) | Pipe coupling that has enhanced the earthquake-proof and sealing property | |
JP2017220344A (en) | Battery pack | |
JP2015227701A (en) | Pipe connecting structure and connecting member | |
EP2942498B1 (en) | Connecting piping and steam turbine system | |
JP2012012798A (en) | Reinforcing member for through-hole of steel beam and through-hole reinforcing structure thereof | |
JP2022063590A (en) | Double pipe spacer | |
WO2019117220A1 (en) | Composite pipe | |
WO2015037272A1 (en) | Dust cover | |
JP6513894B1 (en) | gasket | |
JP4592437B2 (en) | Anti-vibration clamp manufacturing method | |
JP6090176B2 (en) | Fuel tank | |
JP7467040B2 (en) | Panel structure and method for manufacturing the panel structure | |
JP7502224B2 (en) | Shock absorbing materials | |
JP7522437B2 (en) | Coupling device and method of coupling | |
JP4993743B2 (en) | Pressure vessel connection structure | |
JP7219171B2 (en) | Stopper member | |
KR102129688B1 (en) | Frame construction for industrial vehicle | |
KR102211620B1 (en) | Socket ring structure for duct |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: UNKNOWN Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE |
|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE |
|
17P | Request for examination filed |
Effective date: 20221219 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
DAV | Request for validation of the european patent (deleted) | ||
DAX | Request for extension of the european patent (deleted) | ||
A4 | Supplementary search report drawn up and despatched |
Effective date: 20240129 |
|
RIC1 | Information provided on ipc code assigned before grant |
Ipc: F17C 1/16 20060101AFI20240123BHEP |