Pressure vessel
10337670 ยท 2019-07-02
Assignee
Inventors
Cpc classification
F17C13/084
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/0153
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/0604
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/066
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/0123
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/036
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2221/012
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/031
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/0663
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/0109
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B29C49/16
PERFORMING OPERATIONS; TRANSPORTING
F17C2203/0673
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/056
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2209/221
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
F17C13/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2205/0305
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/0675
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C1/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/058
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2209/2127
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2270/0184
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B29C49/071
PERFORMING OPERATIONS; TRANSPORTING
F17C2270/0178
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2260/011
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2209/227
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B29C49/20
PERFORMING OPERATIONS; TRANSPORTING
F17C2221/033
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F17C1/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C13/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C13/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B29C49/00
PERFORMING OPERATIONS; TRANSPORTING
B29C49/20
PERFORMING OPERATIONS; TRANSPORTING
Abstract
The present invention relates to a pressure vessel, comprising a connecting element, an inner vessel and a support shell which surrounds the inner vessel, wherein the pressure vessel has the following features: the connecting element comprises a neck section in the form of a sleeve and a shoulder section; the connecting element is bonded via its outer face to an inner face of the inner vessel; the inner vessel is bonded to the support shell in such a way that the inner vessel is arranged in a sandwich-like manner at least in sections between the connecting element and the support shell; and the pressure vessel has at least one orifice delimited by the neck section of the connecting element, wherein the pressure vessel is characterized in that the outer face of the connecting element facing the inner vessel at least partly has a mean roughness of more than 50 m.
Claims
1. A pressure vessel, comprising: a connecting element; an inner vessel; a support shell which surrounds the inner vessel; wherein the connecting element comprises a neck section in a form of a sleeve and a shoulder section; wherein the connecting element is bonded via an outer face thereof to an inner face of the inner vessel; wherein the inner vessel is bonded to the support shell such that the inner vessel is arranged in a sandwich-like manner at least in sections between the connecting element and the support shell; wherein the pressure vessel has at least one orifice defined by the neck section of the connecting element; wherein at least a portion of the outer face of the connecting element facing the inner vessel has a mean roughness of 50 m or more; wherein at least a portion of the outer face of the connecting element has a coating of thermoplastic polymer; wherein the outer face of the neck section of the connecting element has at least one circumferential groove extending in a circumferential direction of the neck section; and wherein the coating of thermoplastic polymer fully covers an entirety of the outer face of the neck section of the connecting element and fills the at least one circumferential groove.
2. The pressure vessel as claimed in claim 1, wherein the outer face of the shoulder section of the connecting element has at least one radial groove having an extension component in the radial direction of the connecting element.
3. The pressure vessel as claimed in claim 2, wherein the coating of thermoplastic polymer fully covers an entirety of the outer face of the shoulder section of the connecting element and fills the at least one radial groove.
4. The pressure vessel as claimed in claim 1, wherein the mean roughness of 50 m or more is between 50 m and 1,000 m.
5. The pressure vessel as claimed in claim 1, wherein the mean roughness of 50 m or more is between 50 m and 500 m.
6. The pressure vessel as claimed in claim 1, wherein the connecting element is formed of metal.
7. The pressure vessel as claimed in claim 1, wherein the connecting element includes an internal thread in the neck section.
8. The pressure vessel as claimed in claim 1, wherein the inner vessel is blow-molded.
9. The pressure vessel as claimed in claim 1, wherein the inner vessel is formed of thermoplastic.
10. The pressure vessel as claimed in claim 1, wherein the inner vessel is mutilayered.
11. The pressure vessel as claimed in claim 1, wherein the support shell is formed of fiber-reinforced plastic.
12. The pressure vessel as claimed in claim 1, wherein at least a portion of the coating of thermoplastic polymer has a thickness that is thinner than the mean roughness of the outer face of the connecting element.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DETAILED DESCRIPTION
(8) In the description which now follows, identical reference numerals denote the same components or the same features, such that a description with regard to one component conducted in relation to one figure also applies to the other figures, and so repetitive description is avoided.
(9) As apparent from
(10) It is apparent from
(11) As apparent from
(12)
(13) The connecting element 10 may be manufactured from a metal. In the present working example, the connecting element 10 is manufactured from aluminum. The inner vessel 30 may be formed from a thermoplastic material. The thermoplastic material may have a multilayer structure, in which case, for example, an EVOH layer arranged in the middle may be bonded to two outer layers consisting of HDPE by means of two adhesion promoters, for example in the form of LDPE layers. The support shell 40, which can also be referred to as outer shell 40, is formed from a fiber-reinforced plastic. More particularly, the support shell 40 may be formed from CRP (carbon-reinforced plastic), in which case the plastic is preferably a thermoplastic polymer.
(14) Because of the varying compressive stress on the pressure vessel 1, the bond between the connecting element 10 and the inner vessel 30, which can also be referred to as inner shell 30 or lining 30 or liner 30, has to be particularly stable. Firstly axial forces which are caused by the pressure differential between the external pressure and the internal pressure of the pressure vessel 1 and secondly radial forces are transmitted to the connecting element, which can cause the connecting element 10 to become detached from the pressure vessel 1 by rotation.
(15) To increase the bond strength between the connecting element 10 and the inner vessel 30, the outer face 16 of the connecting element 10 facing the inner vessel 30 at least partly has a mean roughness of more than 50 m. The mean roughness is preferably between 50 m and 1000 m. The rougher the outer face 16, the greater the effective bonding area of the connecting element 10. Thus, the connecting element 10 having a roughened outer face 16 can enter into a more intimate and cohesive bond with the inner face 31 of the inner vessel 30. When the still thermoplasticized inner vessel 30 or a still thermoplasticized parison is pressed onto the outer face 16 of the connecting element 10, the thermoplasticized material adapts to the rough surface 16 of the connecting element 10, such that a stable cohesive bond is established between the connecting element 10 and the inner vessel 30.
(16) The outer face 16 of the connecting element 10 can be effected, for example, by blasting of an abrasive blasting agent onto the outer face 16. For example, the outer face 16 can be sandblasted. In addition, it is possible that the outer face 16 is also blasted with ceramic particles or with steel particles or else, for example, with steel shot. In the case of corresponding blasting with an abrasive blasting agent, it is possible to produce a very rough outer face 16 having a high mean roughness of more than 50 m. Correspondingly high mean roughnesses are possible only with difficulty, if at all, by an etching method for example. Moreover, in the case of roughening of the outer face by an etching method, it is necessary to use correspondingly hazardous chemical substances.
(17) In addition, it is possible to achieve roughening of the outer face 16 of the connecting element 10 by applying a material layer to the outer face 16 of the connecting element 10. The material can be applied, for example, by selective laser melting. For example, it is possible to blast an aluminum powder onto the outer face 16 of the connecting element 10, while a high-powered laser beam is used to irradiate the contact region of the aluminum powder with the outer face 16, such that the aluminum particles melt at least at the surface, such that they are able to enter into a cohesive bond with the outer face 16.
(18) As apparent from
(19) It is of course also possible for the outer face 16 shown in
(20) It is apparent from
(21) It is apparent from
(22)
(23) The application of the coating 20 on the outer face 16 can be achieved, for example, by meandering movement of the plasma jet on the outer face 16. In addition, it is also possible that the coating is formed by annular coating tracks. In this respect, there are no restrictions with regard to the movement characteristics of the plasma jet 120 relative to the outer face 16.
(24) The connecting element 10 coated in this way can be introduced into a multipart blow mold which is in an opened receiving position, and the blow mold in a closed position forms a mold cavity. Subsequently, a tubular parison can be extruded into the blow mold in the receiving position in such a way that the connecting element 10 is surrounded by the tubular parison. Subsequently, the blow mold can be closed, such that the parison is pressed onto an outer face 16 of the connecting element 10 by means of the blow mold. The parison is still in the thermoplasticized state, and so it is able to adapt to the contour of the connecting element. By applying a pressure differential, the parison is molded in the mold cavity of the closed blow mold. After the blow mold has been opened, the inner vessel 30 can be extracted from the blow mold and then provided with the support shell.
LIST OF REFERENCE NUMERALS
(25) 1 pressure vessel 2 orifice (of the pressure vessel) 10 connecting element, connecting flange, insert, attachment piece 11 neck section 12 circumferential groove 13 shoulder section 14 radial grooves 15 inner thread 16 outer face (of the connecting element) 20 coating 30 inner vessel, lining, inner shell, liner, inliner 31 inner face (of the inner vessel) 40 support shell, outer shell (comprising fiber-reinforced plastic) 50 impact guard, cap 100 coating apparatus 110 coating head 120 plasma jet 130 turntable