A method for manufacturing a vessel configured for housing a fluid within, the method comprising: providing two Fiber Reinforced Polymer (FRP) structures shaped with complementary coupling interfaces configured to match with each other, such that an interior volume is defined when the FRP structures are coupled to each other; coupling the FRP structures to each other such that the interior volume is defined; and fastening the FRP structures after they have been coupled to each other.

A method for manufacturing a vessel configured for housing a fluid within, the method including: providing at least two at least partially cured fiber reinforced polymer (FRP) structures with complementary shapes configured for matching with each other such that an interior volume is defined when the at least partially cured FRP structures are coupled to each other; coupling the at least partially cured FRP structures to each other such that the interior volume is defined; winding at least one layer of FRP material onto at least a portion of the at least partially cured FRP structures once coupled to each other; and applying a curing cycle to cure the resulting assembly.

A high-pressure tank, a manufacturing method for a high-pressure tank, and a manufacturing device for a high-pressure tank capable of simplifying a shape of a metal fitting and performing high-speed FW molding without causing an idle rotation of the metal fitting or a deformation of a liner, for example, when performing the high-speed FW molding are provided. A high-pressure tank includes a liner, a reinforcing fiber layer, and a metal fitting. The reinforcing fiber layer is formed on an outer peripheral surface of the liner. The metal fitting is attached to the liner. The liner includes a liner main body and a protrusion part is provided in a part (cylindrical part) of the liner main body. The protrusion part is formed to protrude in a direction moving radially inward from the cylindrical part and to be fittable to a rotating shaft.

This manufacturing method is a manufacturing method of a high-pressure tank that is formed by joining dome-shaped side end members to both ends of a cylindrical tube member and that has a first reinforcing layer made of fiber-reinforced resin. The manufacturing method has a joining step of joining the side end members to both ends of the tube member such that an outer wall surface of the tube member and an inner wall surface of each side end member face each other. In the joining step, a margin for overlap between each side end member and the tube member in an axial direction of the tube member is within a range of 5% or more to 35% or less relative to the inside diameter of the tube member.

A gas tank comprises: a liner including a cylindrical body part, and a dome part, provided at each opposite ends of the body part; and a reinforcing layer covering an outer periphery of the liner. The reinforcing layer includes: at least one first fiber layer including a first reinforced section provided on an outer periphery of the body part, the first reinforced section being formed by winding fibers in such a manner that the fibers are interlaced with each other; and at least one second fiber layer including a second reinforced section provided on the outer periphery of the body part, the second reinforced section being formed by winding fibers at an angle determined in advance relative to a center axis of the liner.

A gas tank includes: a liner including a tubular body portion having a central axis and a dome portion being located at each of two ends of the body portion; and a reinforcing layer covering the outer periphery of the liner. The reinforcing layer includes at least one a first fiber layer. The first fiber layer includes, on an outer periphery of the body portion, a first reinforcing portion and a second reinforcing portion. The first reinforcing portion is a portion in which fibers are wound in a staggered weave pattern, and the second reinforcing portion is a portion in which the fibers are wound at a predetermined angle with respect to the central axis.

A high-pressure tank includes a cylindrical portion including a fiber-reinforced resin and a dome portion including a fiber-reinforced resin. The cylindrical portion includes an axial fiber layer including a fiber oriented in a center axis direction of the high-pressure tank, and a circumferential fiber layer including a fiber oriented in a circumferential direction of the high-pressure tank. An end portion of the axial fiber layer and an end portion of the dome portion are joined to each other.

The invention relates to a method of manufacturing a pressure vessel and to a corresponding pressure vessel. The invention proposes a manufacturing method for a pressure vessel where first a pressure vessel blank having at least one liner type 4 and a cylindrical pipe operatively connected to it is manufactured and subsequently, for instance, a fibre composite material is wrapped onto the pressure vessel blank.

The invention relates a pressure vessel (100) configured for storing a fluid under pressure, said pressure vessel comprising: a thermoplastic liner (40) having a cylindrical section (41), a first rounded end section (42) and a second rounded end section (42); a reinforcement structure (50) made of a composite material, said reinforcement structure surrounding at least the cylindrical section of the thermoplastic liner; and a local reinforcement layer (20).

The invention relates to a fiber-reinforced pressure vessel (1) and to a method (100) of manufacturing the same, having an inner vessel (2) made of a thermoplastic material for receiving a filling medium, with an outer face and a fiber composite layer (3) arranged around the outer face for providing pressure resistance of the pressure vessel and at least one valve connection (4) connected to the inner vessel and the fiber composite layer; a thermoplastic band (5) being applied additionally at least on a portion of the outer face of the inner vessel, the thermoplastic band having a thermal expansion coefficient which is small enough to keep any gap (6) which may be created by thermal shrinkage between the fiber composite layer and the inner vessel by its thermal expansion coefficient smaller than would be the case without the presence of the thermoplastic band.