High pressure tank having reinforced boss part
10823332 ยท 2020-11-03
Assignee
Inventors
Cpc classification
F17C2203/0604
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2260/042
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/011
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/0123
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/036
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C1/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2270/0171
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2221/012
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2205/0305
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C13/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2270/0168
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2260/012
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/067
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2270/0184
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/0663
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/0109
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2270/0178
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E60/50
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
F17C2260/011
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2270/0102
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
F17C2270/0176
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/0646
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F17C1/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A high pressure tank having a reinforced boss part includes: a liner; a dome formed at each end of the liner; and a boss formed at one end of the dome. The boss includes: a head including a flow path through which fuel flows into and out of the high pressure tank; and a shoulder extending in a radial direction from the head and surrounding the head. The shoulder has one or more hollow portions formed therein.
Claims
1. A high pressure tank having a reinforced boss, the high pressure tank comprising: a liner; a dome disposed at each end of the liner; and a boss disposed at one end of the dome, wherein the boss comprises: a head having a flow path through which fuel flows into and out of the high pressure tank; and a shoulder extending in a radial direction from the head and surrounding the head, wherein the shoulder has one or more hollow portions defined therein, wherein the one or more hollow portions are an empty space, and wherein the one or more hollow portions does not contact the liner.
2. The high pressure tank of claim 1, wherein each of the one or more hollow portions has a ring shape in the shoulder while having a concentric circular shape from the head of the boss, and wherein a width of each of the one or more hollow portions increases toward the head.
3. The high pressure tank of claim 1, wherein each of the one or more hollow portions has a plate shape in the shoulder and arranged in a radial direction from a center of the head.
4. The high pressure tank of claim 1, wherein the one or more hollow portions are arranged at a constant interval.
5. The high pressure tank of claim 1, wherein a composite material is wound around the shoulder of the boss.
6. The high pressure tank of claim 1, wherein the head comprises: a plurality of liners having different diameters; and a tapered inclined surface connecting the plurality of liners from each other, wherein a composite material is wound around the head to a level at which the tapered inclined surface meets a liner that has the largest diameter among the plurality of liners.
7. A high pressure tank having a reinforced boss, the high pressure tank comprising: a liner; a dome disposed at either end of the liner; and a boss disposed at one end of the dome, wherein the boss comprises: a head comprising a flow path through which fuel is introduced into and out of the high pressure tank; and a shoulder extending in a radial direction from the head and surrounding the head, wherein the shoulder has one or more semi-hollow portions defined at an outer circumferential surface of the shoulder, wherein the one or more semi-hollow portions are an empty space, and wherein the one or more semi-hollow portions does not contact the liner.
8. The high pressure tank of claim 7, wherein the one or more semi-hollow portions are defined at the outer circumferential surface of the shoulder while being arranged in a radial direction from a center of the head.
9. The high pressure tank of claim 7, wherein the one or more semi-hollow portions are arranged in a waffle pattern at the outer circumferential surface of the shoulder.
10. The high pressure tank of claim 7, wherein the one or more semi-hollow portions are arranged at a constant interval.
11. The high pressure tank of claim 7, wherein a composite material is wound around the shoulder of the boss.
12. The high pressure tank of claim 7, wherein the head comprises: a plurality of liners having different diameters; and a tapered inclined surface connecting the plurality of liners, wherein a composite material is wound around the head to a level at which the tapered inclined surface meets a liner having the largest diameter among the plurality of liners.
13. A high pressure tank having a reinforced boss, the high pressure tank comprising: a liner; a dome disposed at each end of the liner; and a boss disposed at one end of the dome, the boss comprises: a head comprising a flow path through which fuel is introduced into and out of the high pressure tank; and a shoulder extending in a radial direction from the head, and surrounding the head, and wherein the shoulder has one or more hollow portions defined therein and one or more semi-hollow portions defined at an outer circumferential surface of the shoulder, wherein the one or more hollow portions and the one or more semi-hollow portions are an empty space, and wherein the one or more hollow portions and the one or more semi-hollow portions do not contact the liner.
14. The high pressure tank of claim 13, wherein each of the one or more semi-hollow portions defined at the circumferential surface of the shoulder is located at an upper portion of a wall between two adjacent one or more hollow portions among the one or more hollow portions defined in the shoulder.
15. The high pressure tank of claim 13, wherein the one or more hollow portions and the one or more semi-hollow portions are arranged at a constant interval.
16. The high pressure tank of claim 13, wherein a composite material is wound around the shoulder of the boss.
17. The high pressure tank of claim 13, wherein the head comprises: a plurality of liners having different diameters; and a tapered inclined surface connecting the plurality of liners, wherein a composite material is wound around the head to a level at which the tapered inclined surface meets a liner having the largest diameter among the plurality of liners having different diameters.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The above and other features of the present disclosure will now be described in detail with reference to certain exemplary embodiments thereof illustrated in the accompanying drawings which are given hereinbelow by way of illustration only, and thus are not limitative of the present disclosure, and wherein:
(2)
(3)
(4)
(5)
(6)
(7)
(8) It should be understood that the appended drawings are not necessarily to scale, presenting a somewhat simplified representation of various features illustrative of the basic principles of the disclosure. The specific design features of the present disclosure as disclosed herein, including, for example, specific dimensions, orientations, locations, and shapes will be determined in part by the particular intended application and use environment.
(9) In the figures, reference numbers refer to the same or equivalent parts of the present disclosure throughout the several figures of the drawing.
DETAILED DESCRIPTION
(10) Hereinafter reference will now be made in detail to various embodiments of the present disclosure, examples of which are illustrated in the accompanying drawings and described below. While the disclosure will be described in conjunction with exemplary embodiments, it will be understood that present description is not intended to limit the disclosure to those exemplary embodiments. On the contrary, the disclosure is intended to cover not only the exemplary embodiments, but also various alternatives, modifications, equivalents and other embodiments, which may be included within the spirit and scope of the disclosure as defined by the appended claims.
(11) The terms er, unit and module described in the specification may indicate a unit for processing one or more functions or operations, and the unit can be implemented by hardware, software, or a combination of hardware and software.
(12) A fuel cell system mounted in a vehicle generally includes a fuel cell stack for generating electrical energy, a fuel supply device for supplying a fuel (hydrogen) to the fuel cell stack, an air supply device for supplying oxygen of the air to the fuel cell stack, the oxygen serving as an oxidizer required for an electrochemical reaction, and a cooling system for removing reaction heat of the fuel cell stack to the outside of the system and controlling an operation temperature of the fuel cell stack.
(13) A fuel supply system of the fuel cell system may include a high pressure tank containing fuel therein and serving as a fuel storage tank. The high pressure tank may contain hydrogen as a fuel. For example, hydrogen gas compressed at a high pressure of about 700 bar may be stored in the high pressure tank.
(14) Thus, the fuel or hydrogen gas contained in the high pressure tank may be continuously maintained in a high-pressure state, while pressurizing the high pressure tank. In particular, when a leak or fracture occurs at one spot of the high pressure tank, the internal high pressure may be concentrated on the spot, thereby damaging the high pressure tank or causing an explosion. Thus, the durability and stability of the high pressure tank is an important factor for a fuel cell system and a vehicle in which the fuel cell system can be mounted.
(15) The high-pressure tank includes a liner made of plastics and a boss part, which is formed at one end of the liner and includes a nozzle for injecting or discharging fuel. According to the recent trend, a type-4 high pressure tank has been frequently used. The type-4 high pressure tank may be formed by winding a carbon fiber composite material on the outside of a structure in which the liner and the boss part are coupled to each other.
(16) Such a type-4 high pressure tank may include a liner which constitutes the main body of the high pressure tank and a hemispherical dome which is formed at either end of the liner and constitutes the high pressure tank with the liner. The hemispherical dome may have a portion relatively weak to high-pressure hydrogen. In order to reinforce such a weak portion, a large amount of carbon fiber composite material needs to be wound on the outside of the dome. A winding thickness may have an influence on the durability of the dome or specifically the weak portion of the dome and the whole weight of the high pressure tank, and determine the whole efficiency of the fuel cell system.
(17) Therefore, the present disclosure provides a high pressure tank including a boss structure which has an empty space formed in a boss at one end of a dome or a groove formed outside the boss, thereby not only lowering the weight of the boss while increasing the strength and durability thereof, but also reducing the amount of wound carbon fiber composite material. Hereafter, a high pressure tank having a reinforced boss according to an exemplary embodiment of the present disclosure will be described in detail with reference to the accompanying drawings. In an exemplary embodiment, the high pressure tank is divided into liner and dome. Specifically, liner may indicate a cylindrical part of the high pressure tank, and dome may indicate a hemispherical part which is formed at either end of the liner and constitutes the high pressure tank with the liner. Further, hollow portion may indicate empty space which can be formed in the boss or specifically a shoulder, and semi-hollow portion may indicate groove which can be formed along the outer circumferential surface of the boss, or specifically the outer circumferential surface of the shoulder of the boss. In this specification, the terms of a singular form may include plural forms unless referred to the contrary.
(18)
(19)
=M/Z,
(20) where : stress, M: moment, and Z: section factor
(21) Considering the above stress equation, it is obvious to those skilled in the art that the stress is decreased as the section modulus is increased. Thus, when the section modulus is increased, the stress is decreased while the resistance to bending is increased. As a result, although the same external pressure is applied, the strength and durability of the corresponding member to the external pressure can be improved. Therefore, in the present exemplary embodiment, an empty space may be formed in the boss or a groove may be formed at the outer circumferential surface of the boss in order to increase the section modulus of the boss. Hereafter, the empty space will be referred to as hollow portion, and the groove will be referred to as semi-hollow portion.
(22)
(23) The boss 200 may be divided into a head 200a and a shoulder 200b. The head 200a of the boss 200 may include a flow path or passage formed therein, which connects the inside and outside of the high-pressure tank, and a nozzle (not shown) may be attached to or detached from an end of the flow path or passage. The head 200a of the boss 200 may include a spiral groove for screw tightening. Further, the head 200a may have a shape in which liners having different diameters are arranged above and below, and the liners having different diameters may be connected to each other by a tapered liner. According to an exemplary embodiment of the present disclosure, one liner that is farther from the high pressure tank may have a larger diameter than another liner closer to the high pressure tank.
(24) The shoulder 200b of the boss 200 may be radially extended from the head 200a at the bottom of the head 200a. Referring to the cross-sectional structure of
(25) According to an exemplary embodiment of the present disclosure, a carbon fiber composite material may be wound on both an outer circumferential surface of the boss 200 and a liner which are coupled to each other. The carbon fiber composite material may be repeatedly wound around the dome 100 until the carbon fiber composite material is stacked to the height at which the tapered liner of the head 200a meets the liner having the larger diameter between the liners having different diameters.
(26) Referring back to
(27) According to another exemplary embodiment of the present disclosure, the hollow portions 210a may have a ring shape in the shoulder 200b as illustrated in
(28) That is, the ring-shaped hollow portion 210a may be formed in an empty liner shape which has a predetermined width in a direction perpendicular to the ring-shaped circular cross-section. Further, when a plurality of hollow portions 210a is formed, liners formed by the hollow portions 210a may have different widths. Furthermore, even in one liner, hollow portions 210a may be formed in cylindrical shapes having different diameters along the direction perpendicular to the ring-shaped circular cross-section.
(29) Referring to
(30) Referring to
(31) When a plurality of semi-hollow portions 210b are formed at the outer circumferential surface of the shoulder 200b regardless of the direction in which the semi-hollow portions 210b are formed, the semi-hollow portions 210b may have depths at which the bottom surfaces of the semi-hollow portions 201b are formed at a constant level. According to still another exemplary embodiment of the present disclosure, the plurality of semi-hollow portions 210b may have a constant depth such that bottom surfaces of the semi-hollow portions 210b are formed at different levels.
(32) Turning back to
(33) In the exemplary embodiments of the present disclosure, the hollow portions 210a and/or the semi-hollow portions 210b may be arranged in parallel to each other at predetermined intervals. Moreover, the hollow portions 210a and/or the semi-hollow portions 210b may be arranged at irregular intervals. That is, although a distance between the hollow portions 210a or the semi-hollow portions 210b is not constant, the hollow portions 210a or the semi-hollow portions 210b may be arranged in such a manner that the distance is repeated according to a predetermined pattern.
(34) The locations where the hollow portions 210a and the semi-hollow portions 210b are formed, the angle, and the direction where the hollow portions 210a and the semi-hollow portions 210b are arranged may be related to the direction where a composite material is wound around the outside of the shoulder 200b of the boss 200. The present disclosure is directed to improving the durability and strength to an external force, while reducing the weight of the boss 200. In this connection, when the composite material is wound around the structure in which the boss 200 and the liner are coupled to each other after the boss 200 and the liner are coupled to each other, the boss 200 inevitably receives force caused by the wound composite material. In this case, the direction of the force received by the boss 200 is inevitably related to the direction in which the composite material is wound. Therefore, in the present embodiment, the design related to the locations and orientation angle of the hollow portions 210a and the semi-hollow portions 210b may consider the winding angle and direction as variables.
(35) That is, the hollow portions formed in the shoulder arranged around the boss or specifically the head of the boss and/or the semi-hollow portions formed at the outer circumferential surface of the shoulder can increase the section modulus of the cross-section of the boss shoulder, thereby reducing stress. Therefore, according to the present disclosure, the hollow portions are formed in the shoulder and the semi-hollow portions are formed at the outer circumferential surface of the shoulder.
(36) The present disclosure has been described in detail with reference to exemplary embodiments thereof. However, it will be appreciated by those skilled in the art that changes may be made in these embodiments without departing from the principles and spirit of the disclosure, the scope of which is defined in the appended claims and their equivalents.
(37) Detailed descriptions related to publicly-known functions or configurations will be ruled out in order not to unnecessarily obscure subject matters of the present disclosure. The terms used herein are defined in consideration of their functions in the exemplary embodiments of the present disclosure, and may differ depending on the custom or intention of a user or operator. Therefore, the definitions should be based on the overall contents of this specification. Thus, the present disclosure is not limited to the exemplary embodiments disclosed in the detailed descriptions, but attached claims may include other exemplary embodiments.