B29C66/91411

FASTENERLESS STRUCTURAL ASSEMBLY

A structural assembly (900) and method of fabricating the same, the method comprising: providing a first member (204) comprising a bond surface (800) and a plurality of protrusions (802) extending from the bond surface (800), a length of each of the protrusions (802) from the bond surface (800) being less than or equal to 2 mm; providing a second member (202) comprising a fibre-reinforced composite material, the fibre-reinforced composite material comprising a plurality of elongate fibres (902) embedded in a polymer matrix (904); while the polymer matrix (904) is in its plastic state, forcing the second member (202) against the bond surface (800) and the protrusions (802) so as to cause the second member (202) to form onto the bond surface (800) and the protrusions (802); and thereafter causing the polymer matrix (904) to harden, thereby fixing the first member (204) to the bond surface of the second member (202).

METHODS AND APPARATUS FOR FABRICATING PANELS

A composite sandwich panel includes a first composite part and a second composite part. A plurality of stiffeners extend between the first and second composite parts. A fiberglass composite perimeter edge closeout is positioned along one or more edges of the first and second composite parts. The fiberglass composite perimeter edge closeout controls a magnetic flux to bond the first and second composite parts to the plurality of stiffeners.

METHODS FOR INCREASING A RETENTION FORCE BETWEEN A POLYMERIC SCAFFOLD AND A DELIVERY BALLOON

A medical device includes a scaffold crimped to a catheter having an expansion balloon. The scaffold is crimped to the balloon by a process that includes inflating the delivery balloon during a diameter reduction to improve scaffold retention and maintaining an inflated balloon during the diameter reduction and prior and subsequent dwell periods.

METHOD AND APPARATUS FOR EMBEDDING AN IMPLANT IN A BALLOON SURFACE BY INDUCTIVE HEATING OF THE IMPLANT
20200069926 · 2020-03-05 ·

A method fixes an implant on a balloon. The balloon, together with an implant, which is crimped onto a balloon surface of the balloon such that the implant by an inner side contacts a contact region of the balloon surface, is provided in the interior of a mold. The balloon interior is acted on by a pressure and the implant is inductively heated so that the contact region over the implant is heated and plastically deformed. The inner side of the implant is embedded in the balloon surface. Additionally, an assembly is produced by the method and an apparatus are provided for carrying out the method.

Storage bag

A method of making a storage bag comprising the following steps performed in any order: (a) forming a composite tube having an inner surface comprising a higher melting polymer, an outer surface comprising a lower melting polymer, two ends, and a diameter; (b) flattening the tube in a direction perpendicular to the diameter; (c) forming a joint at one of the ends at a temperature between respective melting points of the higher melting polymer and the lower melting polymer; (d) providing a composite sheet having a first side comprising a higher melting polymer and a second side comprising a lower melting polymer; and (e) disposing the composite sheet over the joint such that the first side comprising a lower melting polymer engages the joint and forming a lap seam over the joint at a temperature between respective melting points of the higher melting polymer and the lower melting polymer, and a storage bag made by such method.

METHODS OF CO-BONDING A FIRST THERMOSET COMPOSITE AND A SECOND THERMOSET COMPOSITE TO DEFINE A CURED COMPOSITE PART

Methods of co-bonding a first thermoset composite (TSC) and a second TSC to define a cured composite part are disclosed herein. The methods include partially curing the first TSC to a target state of cure (SOC) to define a first partially cured TSC. The partially curing is based, at least in part, on a maximum temperature of the first TSC during the partially curing and on an elapsed time that an actual temperature of the first TSC is greater than a threshold temperature. The methods further include combining the first partially cured TSC with the second TSC to define a partially cured TSC assembly and heating the partially cured TSC assembly to bond the first partially cured TSC to the second TSC, cure the partially cured TSC assembly, and produce a cured composite part.

PROCESS FOR MANUFACTURING THERMOPLASTIC POLYMER COMPOSITE PARTS, AND OBJECT OBTAINED BY SAID PROCESS

The invention relates to a process (100) for manufacturing an object (1) made of thermoplastic polymer composite from at least two parts (10) made of thermoplastic polymer composite, said thermoplastic polymer composite comprising a fibrous reinforcement and a thermoplastic polymer matrix, said process comprising the steps of:

arranging (120) the two parts (10) made of thermoplastic polymer composite adjacently or overlapping at an assembly interface zone (11), and

heating (130) to melt the thermoplastic polymer matrix at said assembly interface zone (11), so as to form an object (1) made of thermoplastic polymer composite comprising a welded interface (12).

METAL CLAD LAMINATE AND PRODUCTION METHOD THEREOF

Provided are a metal clad laminate and a method for producing the same. The metal clad laminate at least includes a thermoplastic liquid crystal polymer film and a metal sheet bonded to each other, wherein the thermoplastic liquid crystal polymer film has a surface with a glossiness (20) of 55 or higher in accordance with JIS Z 8741 on the opposite side of the bonding surface to the metal sheet. The method for producing a metal clad laminate at least includes: providing a thermoplastic liquid crystal polymer film 2 and a metal sheet 6; and introducing the thermoplastic liquid crystal polymer film 2 and the metal sheet 6 between a pair of heating rolls so as to laminate them.

CO-CONSOLIDATION OF THERMOPLASTIC PARTS
20200031060 · 2020-01-30 ·

Systems and methods are provided for consolidating thermoplastic parts. One embodiment is a method of automatically forming a thermoplastic composite structure. The method includes heating a thermoplastic preform to a forming temperature, forming the thermoplastic preform into a thermoplastic part having a desired shape, aligning multiple thermoplastic parts together, and consolidating the multiple thermoplastic parts together while controlling crystallization to form a complex thermoplastic part.

Article having a seal and process for forming the same

An article having an embossed seal includes at least two webs, and an embossed seal joining a portion of the at least two webs, the seal including co-registered concentric discrete extended elements formed in the at least two webs, the discrete extended elements having open proximal ends.