A fillet for a composite panel may be formed by pulling a prepreg slit tape from a spool and winding the slit tape into a fillet mold around the perimeter of a wheel. The tension, heat, and speed may all be adjusted during the winding process. A guide may guide the slit tape to specific locations in the fillet mold. The fillet may be removed from the wheel and coupled to the composite panel and cured.

A method of manufacturing a gas tank comprises: a step (a) of preparing a liner having a hollow cylindrical shape; a step (b) of forming a first layer by winding a first fiber bundle impregnated with resin around the liner; a step (c) of forming a second layer by winding a second fiber bundle impregnated with resin around the liner with the wound first fiber bundle in such a manner that portions of the second fiber bundle overlap each other in a direction parallel to a center axis of the liner; a step (d) of causing a section where the portions of the second fiber bundle overlap each other to get into the first layer; and a step (e) of curing the resin.

The method for forming from a round shaped cylinder to a square shaped cylinder which can be inserted in a square or rectangular shape metal container (shipping container and frac tanks) includes initiating turning of a heated mandrel, extruding heated polymer, wrapping while compressing a first layer of heated polymer, disposing a mesh layer over the cylinder encapsulating the cylinder on the turning mandrel while simultaneously laying a second layer of heated polymer over the turning mandrel and compressing the layer of heated polymer into the mesh layer and the mesh layer into the first layer of heated polymer simultaneously, and repeating the layering of the heated polymer and mesh layer until a desired wall is reached. The method forms a hybrid polymer square or oval tank or a hybrid polymer round, which achieves over 95 percent of the total volume of the metal container.

A tank for containing a pressurized fluid, including at least one cylindrical element made of a pultruded fibrous material impregnated with a thermoplastic matrix, a first cap placed at one end of at least one cylindrical element closing it, a second cap placed at the other end of at least one cylindrical element, fitted with an orifice intended to make possible the entry and the exit of the fluid, and at least one additional fibrous reinforcement, partially or completely surrounding the cylindrical element(s) and optionally the caps, the fibers contained in the additional fibrous reinforcement being positioned along a different axis from the longitudinal axis of the cylindrical element, the total content of fibers of the tank being of between 40% and 70% by volume, with respect to the volume of the matrix and of the fibers contained in the tank.

A method of forming a reinforced polymeric component includes securing a plurality of pins within a mold and wrapping reinforcing fibers around the pins to form a web of reinforcing fibers. The web of reinforcing fibers has a plurality of layers. The method of forming a reinforced polymeric component further includes adding a polymer to the mold and processing the polymer to form a molded polymeric component that contains the pins and the web of reinforcing fibers. A reinforced polymeric component includes a web of reinforcing fibers wrapped around a plurality of pins. The web of reinforcing fibers includes a plurality of layers. The reinforced polymeric component further includes a molded and processed polymer containing the web of reinforcing fibers and pins.

The present invention relates to a method and an assembly for manufacturing a leaf spring from a fiber-composite material. To this end, tape material from a fiber material, which has been pre-impregnated with a matrix resin, for manufacturing a semi-finished leaf spring is wound under tension onto a winding core, wherein at least two cavities for shaping are configured on the winding core. The tape material here is pressed on by way of a contact pressure means, such that adjacent layers of the fiber material are adhesively interconnected and air pockets are removed. The semi-finished leaf spring under impingement by pressure and heat and under curing of the matrix resin is finally processed to form a leaf spring.

A tension member with at least one loop made from fiber-reinforced plastic, which tension member has a plurality of fibers that run substantially parallel to each other, so that the loop is formed by the plurality of fibers, wherein a first group of fibers is turned over along the loop in a first turning direction, while a second group of fibers is turned over along the loop in a second turning direction, which is opposed to the first turning direction. Some of the turned-over fibers of both groups end in a different distance from the vertex of the loop than others of the turned-over fibers, so that a cross-section of the tension member that results from the respective number of fibers that run approximately parallel to each other outside the turning-over area of the fibers approximately continuously decreases until it reaches the cross-section size of the tension member.

Apparatus and systems provide for the construction of wing sections having multi-box wing spars. According to one aspect of the disclosure provided herein, an aircraft wing includes multi-box wing spars attached to an aircraft fuselage, an upper wing surface, a lower wing surface, and a number of wing segments. The multi-box wing spars, upper wing surface, and lower wing surface are composite layers having continuous fibers.

The fiber-reinforced plastic member includes a continuous variation layer which includes a synthetic resin constituting a base and a plurality of reinforcement fibers embedded in the synthetic resin, and a reinforcing layer which is attached to the continuous variation layer to constitute the fiber-reinforced plastic member for a vehicle and is composed of a synthetic resin constituting the base and a plurality of reinforcement fibers.

In particular, the plurality of reinforcement fibers in the continuous variation layer are arranged so as to be inclined with respect to a longitudinal direction of the fiber-reinforced plastic member for a vehicle and angles of the reinforcement fibers with respect to the longitudinal direction of the fiber-reinforced plastic member progressively varying along the longitudinal direction and the plurality of reinforcement fibers in the reinforcing layer are embedded in the synthetic resin and intersecting each other in a reticular pattern.

The invention outlines a method for producing large-sized square tubes from composite materials, incorporating a finishing process. This method addresses the need for high-quality square tube products made from composite materials, which must meet stringent requirements for lightweight design, high mechanical strength, and pressure resistance both internally and externally. The process consists of the following steps: step 1: prepare necessary equipment and materials; step 2: wind the inner layers; step 3: wrap the foam core layer over the inner layers; step 4: vacuum press the foam core layer onto the inner layers; step 5: wind the outer layers; step 6: vacuum press and heat to solidify the entire product; step 7: demould and finish the product.