NZ263248A - Fluid pressure vessel boss-liner attachment with boss having exterior annular shoulder and interior annular groove for coupling to liner - Google Patents

Fluid pressure vessel boss-liner attachment with boss having exterior annular shoulder and interior annular groove for coupling to liner

Info

Publication number
NZ263248A
NZ263248A NZ26324894A NZ26324894A NZ263248A NZ 263248 A NZ263248 A NZ 263248A NZ 26324894 A NZ26324894 A NZ 26324894A NZ 26324894 A NZ26324894 A NZ 26324894A NZ 263248 A NZ263248 A NZ 263248A
Authority
NZ
New Zealand
Prior art keywords
boss
liner
shell
opening
pressure vessel
Prior art date
Application number
NZ26324894A
Inventor
Sadanandan N Sirosh
Original Assignee
Edo Canada Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Edo Canada Ltd filed Critical Edo Canada Ltd
Publication of NZ263248A publication Critical patent/NZ263248A/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C1/00Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge
    • F17C1/16Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of plastics materials
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C13/00Details of vessels or of the filling or discharging of vessels
    • F17C13/002Details of vessels or of the filling or discharging of vessels for vessels under pressure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/01Shape
    • F17C2201/0104Shape cylindrical
    • F17C2201/0109Shape cylindrical with exteriorly curved end-piece
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0602Wall structures; Special features thereof
    • F17C2203/0604Liners
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0602Wall structures; Special features thereof
    • F17C2203/0612Wall structures
    • F17C2203/0614Single wall
    • F17C2203/0619Single wall with two layers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634Materials for walls or layers thereof
    • F17C2203/0636Metals
    • F17C2203/0646Aluminium
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634Materials for walls or layers thereof
    • F17C2203/0636Metals
    • F17C2203/0648Alloys or compositions of metals
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634Materials for walls or layers thereof
    • F17C2203/0658Synthetics
    • F17C2203/0663Synthetics in form of fibers or filaments
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2205/00Vessel construction, in particular mounting arrangements, attachments or identifications means
    • F17C2205/03Fluid connections, filters, valves, closure means or other attachments
    • F17C2205/0302Fittings, valves, filters, or components in connection with the gas storage device
    • F17C2205/0305Bosses, e.g. boss collars
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2205/00Vessel construction, in particular mounting arrangements, attachments or identifications means
    • F17C2205/03Fluid connections, filters, valves, closure means or other attachments
    • F17C2205/0388Arrangement of valves, regulators, filters
    • F17C2205/0394Arrangement of valves, regulators, filters in direct contact with the pressure vessel
    • F17C2205/0397Arrangement of valves, regulators, filters in direct contact with the pressure vessel on both sides of the pressure vessel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2209/00Vessel construction, in particular methods of manufacturing
    • F17C2209/21Shaping processes
    • F17C2209/2154Winding
    • F17C2209/2163Winding with a mandrel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2221/00Handled fluid, in particular type of fluid
    • F17C2221/01Pure fluids
    • F17C2221/011Oxygen
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2221/00Handled fluid, in particular type of fluid
    • F17C2221/01Pure fluids
    • F17C2221/014Nitrogen
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2221/00Handled fluid, in particular type of fluid
    • F17C2221/03Mixtures
    • F17C2221/032Hydrocarbons
    • F17C2221/033Methane, e.g. natural gas, CNG, LNG, GNL, GNC, PLNG
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2221/00Handled fluid, in particular type of fluid
    • F17C2221/03Mixtures
    • F17C2221/032Hydrocarbons
    • F17C2221/035Propane butane, e.g. LPG, GPL
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2260/00Purposes of gas storage and gas handling
    • F17C2260/01Improving mechanical properties or manufacturing
    • F17C2260/012Reducing weight
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2260/00Purposes of gas storage and gas handling
    • F17C2260/05Improving chemical properties
    • F17C2260/053Reducing corrosion

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Pressure Vessels And Lids Thereof (AREA)

Abstract

A fluid pressure vessel (80) includes an exterior composite structural shell (84) formed with a cylindrical sidewall (84a) and first and second dome-shaped end sections with two axially aligned openings (88) in the end sections. An interior fluid impermeable liner (94) is disposed in the shell to fit against the inside surface thereof, and includes two openings (98), each aligned with and adjacent to a respective one of the openings in the shell. A pair of end bosses (104) are each disposed in respective adjacent openings of the shell and liner. The improvement of the invention involves forming the bosses so that each includes a cylindrical neck (112), an annular collar (116) extending radially outwardly from the neck, a central hollow or bore (108) extending axially through the neck, and an annular groove (120) formed in the bore to include downwardly and inwardly sloping shoulders (122) on one side of the groove.

Description

New Zealand No. 263248 International No. PCT/IB94/00074 Priority DatB(s): .7./.H J.S 3 Complete Specificstion Fifed: Ciass: (6) " ' ^n.ciBjoo Publication Dafe: '2.4 1997 P-O. Journal No: IM-IB -'1 NEW ZEALAND PATENTS ACT 1953 COMPLETE SPECIFICATION Title of Invention: Fluid pressure vessel boss-liner attachment system with liner/exterior mechanism direct coupling Name, address and nationality of appiicant(s) as in international application form: EDO CANADA LTD, of 1940 Centre Avenue N.E., Calgary, Alberta T2E OA7, Canada . Ar f. J=y 26324 « - x A FLUID PRESSURE VESSEL BOSS-LINER ATTACHMENT SYSTEM WITH LINER /EXTERIOR MECHANISM DIRECT COUPLING This invention relates to a pressure vessel according to the preamble of claim 1, and in particular to a new and improved system and structure for attaching bosses used in such vessels to the liners.
Composite (fiber reinforced resin matrix) containers or vessels have come into common use for 20 storage of a variety of fluids under pressure, including storage of oxygen, natural gas, nitrogen, rocket fuel, propane, etc. Such composite construction provides numerous advantages such as lightness in weight and resistance to corrosion, fatigue and catastrophic 25 failure. This combination of lightness in weight and resistance to failure is possible due to the high specific strengths of the reinforcing fibers or filaments (carbon, glass, aramid, etc.) which, in the construction of pressure vessels, are typically oriented 30 in the direction of the principal forces.
Since the resin matrix of the composite pressure vessel (shell) is subject to cracking and crazing during service and use, the vessels are oftentimes furnished with fluid impermeable liners. While metal liners are hr:\ "" ,v > iOuJ OFF'tCS most common, elastomeric rubber and thermoplastic liners have also been utilized. Advantageously, the liners are designed not only to prevent leaks from the vessel, but also to serve as mandrels during the vessel fabrication-5 -i.e., profile definition for the composite shell.
Maximum structural efficiency is attained when the lightweight composite shell is used to carry the majority of the load, with little contribution from the liner;- and so if metal liners are used, the liner must 10 be relatively thin in order to reduce the weight. However, thin metal liners have low fatigue life and because of this problem of sacrificing a low weight for durability, and vice versa, users have increasingly looked to use non-metallic liners which are lighter in 15 weight and yet fluid impervious.
One problem with the use of non-metallic liners is that of securely attaching the liners to the vessel bosses which are typically metallic. The end-bosses support fluid passage into and out of the vessel and 20 also may function in the fabrication of the composite shell by providing for fiber turnaround at the ends or poles of the vessel and for mandrel support if filament, winding is used to construct the shell. When metal liners are used, such bosses are generally constructed 25 integrally with the liners, but with the increased use of non-metallic liners, other methods of attaching the bosses to the liners have been needed.
Some prior approaches to attaching non-metallic liner :;, to bosses have included adhesive-bonding of the 30 boss to the liner (if the liner is sufficiently rigid), and simple reliance on the internal pressure in the vessel to provide a boss-liner seal (if the liner is a flexible, collapsible membrane) . FIGS. 2 and 3 of the drawings illustrate these two approaches for attaching 35 non-metallic liners to bosses, and will be discussed momentarily.
The above two approaches, however, fpreseit'problems'- ' including breakdown under fatigue cycling or exposure to certain environments of the metal (boss) to non-metallic (liner) bonding, disintegration of the bond because of 5 significantly different coefficients of thermal expansion of most metals versus non-metals, and shifting of the liner in the shell (if only internal pressure is relied upon) giving rise to leak paths through the boss-liner joint.
In addition to the need for properly attaching the 10 liner to the bosses, it is also important to provide a shear layer at the composite shell/metallic boss interface to reduce the tendency for large shear stresses to develop at that interface. In the past, rubberized compounds have been utilized for such layers but these are prone to 15 disintegrate over time.
Tn attempts to overcome such problems, liners have "made so as to extend up to the hollow defined by the boss and have been made with two lips, one extending between the composite shell and the metallic boss, and the other extending to the hollow at the axial center of the boss. Examples of such attempts are shown in French Patent No. 2 280 856. This patent shows a liner one lip of which terminates in a groove formed at the inward end of the hollow.
It is the object of the present invention to provide a vessel as mentioned at the beginning of the description which is improved over the prior art.
This object is achieved by the features as set forth in the characterizing part of the independent claims 1 and 5.
The present invention provides a system which is specially suitable for attaching non-metallic liners to metal or similarly rigid bosses, in which system the likelihood of fluid leaks between a pressure vessel liner and bosses is reduced. Furthermore, the present invention provides a system in which exterior couplings assist in maintaining attachment of the liners of the bosses and in which the internal fluid pressure in the vessel is utilized to enhance the attachment of the liner to the bosses. 3a A specific illustrative embodiment of a pressure vessel for holding fluids includes an outer shell made of a substantially rigid, mechanically strong material such as composite fiber-reinforced resin, and having at least one oblate end section with an opening therein. Also included is a boss having a neck portion for fitting in the opening of the outer 5 shell and a flange portion extending outwardly from one end of the neck portion. An inner, generally fluid impervious liner is disposed within the outer shell against the inside surface thereof and includes at least one end section with an opening aligned with the opening 10 of the outer shell. The inr.er liner is formed with a dual-layer lip circumscribing the opening in the liner and having an upper lip segment and a lower lip segment, with an annular recess therebetween for receiving and holding the flange portion of the boss. In effect, the 15 flange portion of the boss is encapsulated in the recess between the upper and lower lip segments of the liner which securely holds it in place.
In accordance with one aspect of the invention, the boss includes a generally cylindrical hollow extending 20 through the neck portion to define a first opening at said one end of the neck portion from which the flanged portion extends, and a second opening at the other end of the neck portion. A first section of the cylindrical hollow adjacent the first opening has a diameter which 25 is smaller than the diameter of a second section of the cylindrical hollow adjacent the second opening. An inwardly sloping shoulder is formed in the cylindrical hollow at the transition between the second section and the first section. The lower lip segment is formed to 30 extend radially inwardly under the flanged portion of the boss and then upwardly through the first opening and along the wall of the hollow of the boss to overlie the shoulder. An attachment, such as a valve, is received into the hollow through the second opening to contact 35 the lower lip segment and pin it against the shoulder. In this manner, the liner is directly coupled to the attachment to provide a more leak-free joint.
In accordance with another aspect of the invention, the underside of the flanged portion of the boss is formed to be radially convex with broadly rounded edges between the underside and the interior of the hollow.
The lower lip segment hugs the convex underside of the flanged portion and the rounded edges leading to the Interior of the hollow, and is held in place by the internal pressure of the fluid in the vessel.
BRIEF DESCRIPTION OF THE DRAWINGS 10 The above and other objects, features and advantages of the invention will become apparent from a consideration of the following detailed description presented in connection with the accompanying drawings in which: FIG. 1 is a side, elevational view of a composite vessel of the type for which the present invention is especially suitable; FIG. 2 is a side, cross-sectional, fragmented view of a composite vessel with an elastomeric liner attached 20 to a boss utilizing only internal pressure of the fluid in the vessel, in accordance with a conventional prior art approach; FIG. 3 is a side, cross-sectional, fragmented view of a composite vessel having a rigid non-metallic liner 25 bonded to a boss in a conventional fashion; FIG. 4 is a side, cross-sectional fragmented view of a fluid pressure vessel made in accordance with the principles of the present invention; and FIG. 5 shows a top, plan view, of a pressure vessel 30 boss made in accordance with the principles of the present invention.
DETAILED DESCRIPTION Referring to the drawings, there is shown in FIG. 1 a typical composite (fiber-reinforced resin) pressure 35 vessel 4, in which the present invention may be utilized. The vessel 4 includes a hollow generally cylindrical central section, and integral oblate end 6 sections 12 and 16. The end sections 12 and 16 include axially-aligned openings 20 and 24 in which are disposed access bosses 28 and 32 respectively. As discussed earlier, the bosses 28 and 32 are typically constructed 5 of metal or metal alloy and are provided for receiving attachments such as valves to allow for the supply of fluid into and removal of fluid from the vessel 4. The bosses 28 and 32 are also typically used, during fabrication of the vessel, for fiber turnaround and 10 mandrel support.
Although the bosses 28 and 32 are shown positioned in the end sections 12 and 16, sometimes called polar sections, the bosses may be placed at other locations, and more than two bosses may be provided. Also, fully 15 spherical vessels could be provided as could other conventional container shapes, with bosses provided where desired.
FIGS. 2 and 3 show prior art approaches to attaching a non-metallic liner, used in vessels of the 20 type shown in FIG. 1, to the end bosses. In particular, FIG. 2 shows a side, cross-sectional, fragmented view of a composite vessel shell 4 0 in which is disposed an elastomeric rubber liner 44. The liner 44 is positioned against the inside surface of the shell 40 and extends 25 to an opening 48 in the shell. A boss 52 is disposed in the opening 48 and includes a lower flange portion 56 which is positioned against the liner 44 surrounding the opening 48. With this prior art configuration, the internal pressure in the vessel against the boss 52 is 30 used to help seal the liner 44 against the boss. However, in the event of an internal vacuum in the vessel, the seal is likely to break down, drawing contaminants into the vessel and causing leak paths to develop between the boss 52 and liner 44. Internal 35 vacuums oftentimes occur even for vessels intended for pressure use, such as when a vessel is partially filled with fluid which then cools down to produce the vacuum.
FIG. 3 illustrates, in side, cross-sectional, fragmented view, a shell 60 of a pressure vessel, in which is disposed a rigid non-metallic liner 64. A boss 68 is disposed in an opening 72 of the shell 60 and is 5 adhesively bonded to a top wall 64a of the liner to provide the desired seal between the liner and the boss. However, as previously mentioned, non-metallic materials (such as plastic)-to-metal adhesive bonding is difficult to maintain, when used in boss-liner attachment, and it 10 generally deteriorates over time and service, leading to leakage at the boss-liner interface.
FIG. 4 shows a side, cross-sectional, fragmented view of a fluid pressure vessel 80 made in accordance with the present invention. The pressure vessel 80 15 includes an exterior shell 84 having a hollow cylindrical center section 84a and two (only one of which is shown) oblate, generally ellipsoidal end sections 84b which are formed integral with the center section. Axially aligned openings 88 (only one of which 20 is shown) are formed in the . end sections 84b as indicated in FIG. 4. The shell 84 is formed of a composite fiber-reinforced resin in the conventional manner.
Disposed inside the shell 84 is a fluid impermeable 25 liner 94 made, for example, of a thermoplastic material such as polyethylene, nylon polyamide, or polyethylene terephthalate (PET). The liner 94 is disposed against the inside surface of the shell 84 and thus has the same general form as the shell including a pair of openings 30 98 (only one of which is shown) which are aligned with respective openings 88 of the shell.
Disposed in the adjacent openings 88 and 98 of the shell and liner respectively is an end boss 104, . typically made of a metal or metal alloy such as 35 aluminum or carbon chromium-molybdenum alloy steel. The boss 104 is formed with an axial cylindrical hollow or bore 108, an upper portion 108a of which is for 8 receiving an attachment 110, such as a -votive, for j supplying fluid into and removing fluid from the vessel 80. The bore 108 also is formed with a lower portion 108b, which has a smaller diameter than the upper 5 portion 108a. The boss 104 is also formed with a generally cylindrical neck portion 112 and which fits within the opening 88 of the shell 84, and a collar or flange portion 116 extending radially outwardly from the lower end of the neck portion. The lower surface of the 10 flange 116 is formed to be generally convex and includes broadly rounded edges 116a between the lower surface of the flange and the interior sidewall 118 of the lower portion 108b of hollow 108. The radius of curvature of the edges 116a is about equal to the thickness of the 15 flange portion 116 at the location of the edges. Similarly a transition 116b between the top of the flange portion 116 and the neck portion 112 is smooth and rounded. The reason for this is to aid in reducing stress concentrations in the boss and in the liner which 20 will follow the boss contours, as will be described hereafter.
Formed in the hollow 108 of the boss 104 is a circumferential groove 120 which, as will be explained later, is for receiving a portion of the liner 94 for 25 aid in holding the liner securely in place. The lower or bottom side of the groove 120 is formed with a downwardly and inwardly sloping shoulder 122, against which the attachment 110 presses an annular bead 128a (to be discussed momentarily) when the attachment is 30 inserted into the bore 108.
That portion of the liner 94 surrounding the opening 98 in the liner is formed into a dual-lip arrangement to include an upper lip segment 124 which circumscribes the neck portion 112 of the boss 104 when 35' the boss is in place, and overlies the upper surface of *" the flange -portion 116 of the boss. The dual-lip configuration of the liner 94 also includes a lower lip ;segment 128 which extends from the underside of the upper lip segment 124 radially inwardly under the lower surface of the flange portion 116 of the boss, and then upwardly, beyond the termination of the upper lip segment 124, into 5 the hollow 108 along the walls 118 of the hollow. The termination of the lower lip segment 128 is formed into an annular bead 128a which fits within the circumferential groove 120 of the boss 104 and serves to hold the lower lip segment 128 in place in the hollow 108. The upper lip 10 segment 124 and the lower lip segment 128 define an annular recess 132 between the two segments for receiving and, in effect, encapsulating and holding the flange portion 116 of the boss 104, as shown in FIG. 4. For the sake of clarity, upper and upwardly is used to designate an axially outward 15 position and direction, while underside, downwardly, lower and bottom are used to designate an axially inward directions and positions. ;With the dual-lip configuration of the liner 94 and the design of the boss 104 with a flange portion 116 that 20 is received and encapsulated within the recess 132 between the lip segments 124 and 128, there is no need for adhesively bonding the boss to the liner. The design of the boss 104 also accommodates use of internal fluid pressure in the vessel for enhancing adherer e of the liner 25 94 to . the boss. In particular, the internal pressure forces the lower lip segment 128 against the bottom surface of the flange portion 116, against the broadly rounded edges 116a, and against the walls 118 of the hollow 108. Because the edges 116a are broadly rounded, the pressure on 30 the lower lip segment 128 and against the boss 104 is substantially uniform to securely hold the liner in place. Such pressure also forces the bead 128a of the lower lip segment 128 into the circumferential groove 120. This groove 120, the locking of the bead 128a of the lower lip 35 segment 128 therein, and placement of an attachment 110 in the bore 108 so that it contacts and presses the lower lip r ;PAT3J*.T Qr< J 9a 263 segment against the shoulder 122, serves to prevent slippage of the liner 94 during pressurization and depressurization. Also, positioning the lower lip 26 3 2 4 8 segment 128 in the hollow 108 at the location of the circumferential groove 120 provides a direct link between the liner 94 and the upper or inlet portion 108a of the hollow 108 and thus the attachment 110 to thereby 5 minimize the likelihood of leak paths developing. Advantageously, the attachment includes exterior threads 111 which are compatible with and may be screwed into corresponding threads 109 formed in the inlet portion 108a of the bore 108.
The upper lip segment 124 of the liner 94 is disposed between the boss 104 and the shell 84 and, in particular, between the flange portion 116 of the boss and the shell to act as a shear layer.
To enhance torque transfer between the boss 104 and 15 the liner 94, cogs or notches 136 are formed at spaced-apart locations in the perimeter of the flange portion 116, as best seen in FIG. 5. These notches 136 are positioned to contact the walls of the annular recess 132 between the upper lip segment 124 and lower lip 20 segment 128 to assist, in the torque or torsional shear transfer between the boss and liner. The upper surface and lower surface of the flange portion 116 of the boss 104 may also be roughened or otherwise treated to prevent the sliding thereover of the upper lip segment 25 124 and lower lip segment 128 respectively to further enhance the torque transfer.
It is to be understood that the above-described arrangements are only illustrative of the application of the principles of the present invention. Numerous 30 modifications and alternative arrangements may be devised by those skilled in the art without departing from the scope of-the invention and the appended claims are intended to cover such modifications and arrangements. p I 2Gt)EClfW6 Re: International application No. PCT/EB 94/00074 FLUID PRESSURE VESSEL BOSS-LINER ATTACHMENT... Applicant: EDO CANADA LTD.
Our Ref.: PCT 493-422/ha 3. July 1995

Claims (8)

1. A pressure vessel for holding fluids including an outer shell (84) made of a substantially rigid, mechanically strong material, and having at least one oblate end (84b) section with an opening (88) therein, boss means (104) having a neck portion (112) for fitting in the opening in the outer shell and a flange portion (116) extending radially outwardly from one end of the neck portion, the boss means having a generally cylindrical hollow (108) substantially aligned with the opening in the outer shell, and an inner, generally fluid impervious non-metallic liner (94) disposed within the outer shell against the inside surface thereof, and having at least one end section with an opening aligned with the opening of the outer shell, said inner liner being formed with a dual-layer lip circumscribing the opening in the liner and having an upper lip segment (124) and a lower lip segment (128), with an annular recess (132) therebetween for receiving and holding therein the flange portion of the boss means, the upper lip segment being held between the inside surface of the outer shell and the upper surface of the flange portion of the boss means and the lower lip segment extending radially inwardly under the lower surface of the flange portion of the boss means and then axially outwardly into the hollow (108) of the boss means, wherein the boss means includes a circumferential groove (120) in the hollow o^--the boss means, and wherein the lower lip 26 3 24 8 12 segment terminates in an annular bead (128a) for fitting in the circumferential groove, characterized in that the circumferential groove (120) is formed in the boss means (104) spaced axially outwardly from the flange poriton so that the lower lip (128) extends along the interior wall of said cylindrical hollow (108) .
2. A pressure vessel as in Claim 1 wherein said outer shell (84) is made of a composite fiber-reinforced resin material, wherein said inner (94) is made of a non-metallic material, and wherein said boss means (104) is made of metal or metal alloy.
3. A pressure vessel as in Claim 1 wherein the lower surface and the upper (axially outward) surface of the flange portion (116) of the boss means (104) have a rough, non-skid texture to inhibit sliding thereover of the lower lip segment (128) and upper lip segment (124) respectively.
4. A pressure vessel as in Claim 1 wherein said hollow includes a first portion having a first diameter for receiving the lower lip segment (12 8), and an inlet portion having a diameter greater than the first diameter for receiving an attachment mechanism, and wherein the said groove (120) is formed in the hollow with a sloping shoulder between the first portion and the inlet portion such that when the bead (128a) is fitted into the groove, an attachment mechanism (110) received in the inlet portion contacts the lower lip segment at the bead to pin the lower lip segment against the sloping shoulder of the groove. 13
A pressure vessel having an exterior composite structural shell (84) formed with a cylindrical sidewall and first and second dome-shaped end sections (84b) with two axially aligned openings (88) in the end sections, and interior fluid impermeable non-metallic liner (94) shaped to fit against the inside surface of the shell and having two openings (98) , each aligned with and adjacent to a respective one of the openings in the shell, and a pair of end bosses (104) each disposed in respective adjacent openings of the shell and the liner, wherein the bosses are each formed with a cylindrical neck (116b), a hollow neck portion (108), and an annular collar (116) extending radially outwardly from the neck, the perimeters of the openings in the liner are each formed with a first radially inwardly projecting section (124) for overlying the axially outward portion of the collar of a respective boss to define a first opening which circumscribes the neck of the respective boss, and a second section (123) projecting from an underside (axially inward portion) of the first section radially inwardly, for underlying the bottom (axially inward portion) of the collar of a respective boss, and then axially outwardly into a respective hollow neck portion to terminate in a second opening, said first and second sections defining an annular recess therebetween for receiving and encapsulating a respective collar therein such that the first section is held between the boss and the shell when the boss is installed in the shell, the hollow neck portion of at least one of the bosses is formed with an annular groove (120), the axially inward side of which includes a axially inwardly and radially inwardly sloping shoulder (122) on which a respective second section and second opening rests, characterized in tln^t 14 26 3 24 8 the collar has a radially convex bottom surface, and the axially inv/ardly and radially inwardly sloping shoulder is spaced axially outwardsly from the annular collar so that the second section projects axially outwardly from 5 the first opening along a sidewal'l of the respective neck portion.
6. A pressure vessel as in Claim 5 wherein said at least one boss (104) includes a bore (108) centrally 10 formed in the neck (116b) thereof to communicate with the respective hollow neck portion, one end of the bore being adapted for receiving thereinto an attachment (110) which extends to the annular groove (120) to contact said second section (128) of the opening 15 perimeter in which said at least one boss is disposed, and secure said second section against the sloping shoulder (124). 20 undersides (axially inner portions) of the collars (116) are formed with roughened surfaces to inhibit slipping thereover of the second sections of the liner opening (98) perimeters. least one of the second sections (12P) includes a bead (128a) which extends into the groove vl20) of said at least one boss for engagement with the attachment (110) received in the one end (108a) of the bore (108). 9. A pressure vessel as in Claim 8 wherein said one end (108a) of- the bore (108) has a first diameter, and wherein the other end (108b) of the bore has a second diameter, said groove (120) being formed between 3 5 the one end and the other end of the bore to define said shoulder (122) against which said at least one second
7. A pressure vessel as in Claim 6 wherein the 25
8. A pressure vessel as in Claim 6 wherein at 30 / 5 section (128) is forced by the attachment (110) when the attachment is received into the one end of the bore. amended sheet
NZ26324894A 1993-04-07 1994-04-05 Fluid pressure vessel boss-liner attachment with boss having exterior annular shoulder and interior annular groove for coupling to liner NZ263248A (en)

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AU (1) AU675835B2 (en)
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DE102006054208B4 (en) 2006-01-10 2016-04-07 Erhard & Söhne GmbH Container for operating materials of motor vehicles
DE102006006902B4 (en) * 2006-02-09 2008-02-21 Gräfenthaler Kunststofftechnik GmbH Plastic pressure vessel and process for its manufacture
DE102006057422B3 (en) * 2006-12-04 2008-06-26 Mcs International Gmbh Composite-pressure vessel e.g. for storing gaseous mediums, has liner made of plastic and which is reinforced with fiber composite material with neck
JP4392804B2 (en) 2007-04-06 2010-01-06 豊田合成株式会社 Pressure vessel
NO20073034A (en) * 2007-06-14 2008-09-22 Compressed Energy Tech As End boss and a composite pressure tank
EP2539626A4 (en) * 2010-02-26 2015-09-02 Luxfer Canada Ltd Anti-extrusion sealing system for the outlet of a plastic-lined compressed gas cylinder
DE102011056976A1 (en) * 2011-12-23 2013-06-27 Rehau Ag + Co Apparatus for storing and dispensing liquid and / or gaseous media under pressure, as well as fuel energy conversion apparatus and method for producing a device for storing and dispensing liquid and / or gaseous media under pressure
BR112016007931B1 (en) * 2013-10-08 2022-05-10 Performance Pulsation Control, Inc PULSE CONTROL DEVICE
WO2016167034A1 (en) * 2015-04-15 2016-10-20 八千代工業株式会社 Pressure vessel

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US5253778A (en) * 1992-01-28 1993-10-19 Edo Canada Ltd. Fluid pressure vessel boss-liner attachment system

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JPH08511323A (en) 1996-11-26
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AU6385894A (en) 1994-10-24
EP0693167A1 (en) 1996-01-24
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WO1994023240A1 (en) 1994-10-13
NO953986L (en) 1995-12-05

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