Method for manufacturing glass-fibre reinforced plastic container

• US 5,547,533 A
• Filed: 12/08/1994
• Issued: 08/20/1996
• Est. Priority Date: 05/24/1991
• Status: Expired due to Term

• Current Assignee: Composite Scandinavia AB (Hexagon Composites ASA)
• Original Assignee: Composite Scandinavia AB (Hexagon Composites ASA)
• Inventors: Berglund, Kurt
• Primary Examiner(s): AFTERGUT, JEFFRY H
• Application Number:
  US08/352,282
• Time in Patent Office: 621 Days
• Field of Search: 156/169, 156/172, 156/173, 156/175, 156/166, 156/425, 156/242, 156/245, 156/304.5, 156/158, 264/136, 264/137, 264/257, 264/258, 264/328.12
• US Class Current: 156/175
• CPC Class Codes: B29C 65/00 Joining or sealing of preformed parts , e.g. welding of plastics materials; Apparatus therefor general aspects of processes or apparatus for joining preformed parts B29C66/00; using porous material formed by internal pressure generated therein for joining preformed parts B29C44/1228, B29C44/326
• CPC Class Codes: B29C 65/483 Reactive adhesives, e.g. chemically curing adhesives
• CPC Class Codes: B29C 65/4845 Radiation curing adhesives, e.g. UV light curing adhesives
• CPC Class Codes: B29C 65/5014 being fibre-reinforced B29C65/5028 takes precedence
• CPC Class Codes: B29C 65/5021 being multi-layered
• CPC Class Codes: B29C 65/5042 covering both elements to be joined
• CPC Class Codes: B29C 66/1122 Single lap to lap joints, i.e. overlap joints B29C66/45, B29C66/472, B29C66/52272 take precedence
• CPC Class Codes: B29C 66/1162 Single bevel to bevel joints, e.g. mitre joints
• CPC Class Codes: B29C 66/1224 comprising at least a butt joint-segment
• CPC Class Codes: B29C 66/1226 comprising at least one bevelled joint-segment
• CPC Class Codes: B29C 66/14 the joint having the same thickness as the thickness of the parts to be joined B29C66/1142 takes precedence
• CPC Class Codes: B29C 66/54 Joining several hollow-preforms, e.g. half-shells, to form hollow articles, e.g. for making balls, containers; Joining several hollow-preforms, e.g. half-cylinders, to form tubular articles
• CPC Class Codes: B29C 66/7212 characterised by the composition of the fibres
• CPC Class Codes: B29C 66/723 being multi-layered B29C66/7292, B29C66/72941 take precedence
• CPC Class Codes: B29C 66/8322 Joining or pressing tools reciprocating along one axis
• CPC Class Codes: B29C 70/207 arranged in parallel planes of fibres crossing at substantial angles
• CPC Class Codes: B29K 2105/06 containing reinforcements, fillers or inserts
• CPC Class Codes: B29K 2309/08 Glass
• CPC Class Codes: B29L 2031/7156 Pressure vessels
• CPC Class Codes: F16J 12/00 Pressure vessels in general covers therefor F16J13/00; for particular applications, see the relevant subclasses, e.g. B01J, F17C, G21C
• CPC Class Codes: F17C 1/06 : built-up from wound-on bands or filamentary material, e.g. wires
• CPC Class Codes: F17C 1/16 : constructed of plastics materials shaping of plastics B29C
• CPC Class Codes: F17C 2201/0109 : with exteriorly curved end-piece
• CPC Class Codes: F17C 2201/0123 : with variable thickness or diameter
• CPC Class Codes: F17C 2201/032 : with substantially vertical main axis
• CPC Class Codes: F17C 2201/056 : Small (<1 m3)
• CPC Class Codes: F17C 2203/011 : Reinforcing means
• CPC Class Codes: F17C 2203/013 : in the vessel, e.g. columns
• CPC Class Codes: F17C 2203/0333 : Polyurethane
• CPC Class Codes: F17C 2203/0345 : Fibres
• CPC Class Codes: F17C 2203/0621 : with three layers
• CPC Class Codes: F17C 2203/0663 : in form of fibers or filaments
• CPC Class Codes: F17C 2203/0665 : radially wound
• CPC Class Codes: F17C 2203/0668 : axially wound
• CPC Class Codes: F17C 2203/0673 : Polymers
• CPC Class Codes: F17C 2209/2109 : Moulding
• CPC Class Codes: F17C 2209/2118 : by injection
• CPC Class Codes: F17C 2209/2154 : Winding
• CPC Class Codes: F17C 2209/221 : Welding
• CPC Class Codes: F17C 2209/225 : Spraying
• CPC Class Codes: F17C 2209/227 : by adhesive means
• CPC Class Codes: F17C 2209/232 : of walls
• CPC Class Codes: F17C 2221/018 : Acetylene
• CPC Class Codes: F17C 2221/031 : Air
• CPC Class Codes: F17C 2221/035 : Propane butane, e.g. LPG, GPL
• CPC Class Codes: F17C 2223/0123 : gaseous, e.g. CNG, GNC
• CPC Class Codes: F17C 2223/0153 : Liquefied gas, e.g. LPG, GPL
• CPC Class Codes: F17C 2223/033 : Small pressure, e.g. for liquefied gas
• CPC Class Codes: F17C 2223/035 : High pressure (>10 bar)
• CPC Class Codes: F17C 2260/011 : Improving strength
• CPC Class Codes: F17C 2260/013 : Reducing manufacturing time or effort
• CPC Class Codes: F17C 2260/042 : Reducing risk of explosion
• CPC Class Codes: F17C 2270/05 : for industrial use

Abstract

Glass-fibre reinforced plastic tank, for example for liquid petroleum gas under high pressure, compressed air for air brakes or for storage of acetylene. The tank is composed of two halves (10, 12), the open ends of which are conically bevelled to form a male end (20) and a female end (22), which are joined to each other by an adhesive. The reinforcement in the outer and inner layers of the halves contains essentially longitudinal glass-fibre strands and the intermediate layer contains essentially transverse glass-fibre strands. In the half with the male end (20), the longitudinal glass-fibre strands in the inner layer (35) are densely located adjacent to each other, while the longitudinal glass-fibre strands in the outer layer lie in separate groups (30) of densely arranged glass-fibre strands with the predetermined spacing between the groups to form channel-shaped spaces (31). In the half with the female end (22), the order is reverse. In order to store acetylene, a pre-fabricated absorbent body of porous material is enclosed in the tank when the tank halves are glued together.

Claims

1. Method of making a reinforcing body of fibre strands for insertion in a casting mould for casting of a fibre-reinforced cylinder with one end closed to be included in a plastic tank, said reinforcing body being built up with its open end facing downwards on a preshaping form, by several layers of both longitudinal and transverse reinforcing fiber strands being wound on the form, whereupon the reinforcing strands of the reinforcing body are sprayed with a meltable resin powder, which after heat treatment bonds the reinforcing strands to each other so that a pre-fabricated reinforcing body is formed, characterized by the following steps:

the reinforcing body (D) for casting a cylinder (10), the open end of which is made as a male end (20), is built up by first winding at least one layer (35) of longitudinal reinforcing strands closely adjacent to each other on the pre-shaping form (50) to define a longitudinal reinforcement;

winding at least one layer (33) of transverse reinforcing strands closely adjacent to each other on the longitudinal reinforcement to define a transverse reinforcement for said male end (20), and winding an additional layer (29) of longitudinal reinforcing strands on the transverse reinforcement, said additional layer of longitudinal reinforcing strands being collected in groups (30) of densely lying reinforcing strands with a pre-determined spacing (F) between the groups to provide channel-shaped spaces (31) between said groups (30),

the reinforcing body (C) for casting of a cylinder (12), the open end of which is to be formed as a female end (22), is built up by first winding a layer (36) of longitudinal reinforcing strands on the pre-shaping form (50), said longitudinal reinforcing strands being collected into groups (37) of densely lying reinforcing strands with a pre-determined spacing (F) between the groups to provide channel-shaped spaces (38) between said groups (37);

winding at least one layer (34) of transverse reinforcing strands closely adjacent to each other on the groups (37) of densely lying longitudinal reinforcing strands to define a transverse reinforcement for said female end (22); and

winding at least one additional layer (32) of longitudinal reinforcing strands closely adjacent to each other on the last mentioned transverse reinforcement.

2. Method of making a reinforcing body according to claim 1 wherein the form (50) includes a lower portion and an upper end (54), characterized in that a roving of the longitudinal reinforcing strands to be included in the first layer (35, 36) of each of said male and female ends is fixed in hooking means (56, 57) near said lower portion of the form (50), and is then drawn upwards parallel to one longitudinal side (52) of the form to its upper end (54), whereafter the reinforcing strands are drawn diametrically across said upper end and then downwards parallel to an opposite longitudinal side of the form (50) and on said opposite side near said lower portion of the form are fixed in opposing means (56, 57), whereupon a new roving of reinforcing strands are wound in the opposite direction closely adjacent to the already wound roving, said process being repeated until the predetermined density of windings is achieved and a predetermined number of courses of windings is achieved.

3. In the method of making cylindrical reinforcing bodies of fibre strands for insertion in a casting mould for casting of fibre-reinforced cylinders, with one end of each cylinder being open and one end closed, said cylinders to be included in a plastic tank;

and each of said reinforcing bodies being built up with its open end facing downwards on a pre-shaping form, by several layers of both longitudinal and transverse reinforcing fiber strands wound on the form, the improvement comprising the following steps;

a) building up a first reinforcing body (D) for casting a first cylinder (10), the open end of which is made as a male end (20), by

i) first winding at least one layer (35) of densely lying longitudinal reinforcing strands closely adjacent to each other on the pre-shaping form (50) to define a longitudinal reinforcement,

ii) winding at least one layer (33) of densely lying transverse reinforcing strands closely adjacent to each other on the longitudinal reinforcement to define a transverse reinforcement for said male end (2), and

iii) winding an additional layer (29) of longitudinal reinforcing strands on the transverse reinforcement in groups (30) of densely lying reinforcing strands with a pre-determined spacing (F) between the groups to provide channel-shaped spaces (31) between said groups (30); and

b) building up a second reinforcing body (C) for casting of a second cylinder (12), the open end of which is to be formed as a female end (22), by

i) first winding a layer (36) of longitudinal reinforcing strands on the pre-shaping form (50) in groups (37) of densely lying reinforcing strands with a pre-determined spacing (F) between the groups to provide channel-shaped spaces (38) between said groups (37),

ii) winding at least one layer (34) of densely lying transverse reinforcing strands closely adjacent to each other over the groups (37) of densely lying longitudinal reinforcing strands and over said channel-shaped spaces (38) to define a transverse reinforcement for said female end (22), and

iii) winding at least one additional layer (32) of densely lying longitudinal reinforcing strands closely adjacent to each other on the last mentioned transverse reinforcement.

4. The improvement in the method of making a reinforcing bodies according to claim 3 comprising:

a) spraying the reinforcing strands of each reinforcing body with a meltable resin powder; and

b) treating the reinforcing strands to bond the strands to each other so that a pre-fabricated reinforcing body is formed.

5. The improvement in the method of making a reinforcing bodies according to claim 3 comprising:

a) cutting off glass fibre reinforcing strands from the open end of each reinforcing body into complimentary conically bevelled surfaces.