Rohr, Inc.

Noushin Bahramshahi

Michael Van Tooren

Daniel O Ursenbach

Lamia Salah

Jeffrey D Woods

Jonathan S Huang

Sarah Lohman

Andrew Adan

Dennis Lunenborg

Roberto Ramos

Peter Boer

David Manten

Nicole M Sannes

Shawn Tardy

A method for forming a fiber-reinforced thermoplastic part may comprise the steps of locating a lightning strike protection layer on a mold surface of a mold tool, locating a thermoplastic layer over the mold tool, heating the thermoplastic layer to a pliable forming temperature, conforming the thermoplastic layer to a mold surface of the mold tool, and depositing a plurality of fiber strips over the thermoplastic layer.

Assemblies and methods for forming fiber-reinforced thermoplastic structures with lightning strike protection

A method for forming a fiber reinforced thermoplastic part may comprise the steps of locating a thermoplastic material over a mold tool, heating the thermoplastic material to a pliable forming temperature, conforming the thermoplastic material to a mold surface of the mold tool, and depositing a plurality of fiber strips over the thermoplastic material.

Assemblies and methods for forming fiber reinforced thermoplastic structures

A joining method is provided during which a first thermoplastic component joint section and a second thermoplastic component joint section are arranged between first tooling and second tooling. The second thermoplastic component joint section is abutted against the first thermoplastic component joint section at a joint area. The first thermoplastic component joint section is joined to the second thermoplastic component joint section to provide a unitized thermoplastic structure. The joining includes: pressing the first thermoplastic component joint section against the second thermoplastic component joint section at the joint area between the first tooling and the second tooling using a pressure device; and heating the first thermoplastic component joint section and the second thermoplastic component joint section at the joint area using a first heater configured with the first tooling. The unitized thermoplastic structure is cooled at the joint area using a first cooler configured with the first tooling.

Joining thermoplastic components

A method of manufacturing a thermoplastic panel may comprise: laying up a panel preform within a consolidation assembly, the panel preform comprising a plurality of plies of material comprising thermoplastic resin and fiber; generating, via a hot bond unit, a vacuum environment within the consolidation assembly; and heating, via the hot bond unit and through a heated blanket within the consolidation assembly, the panel preform.

Systems and methods for thermoplastic panel manufacturing

A first thermoplastic component and a second thermoplastic component including a first joint portion and a second joint portion, respectively, are provided. A least a portion of a surface area of each of the first and second joint portions include a respective first and second mating surface. The first and second mating surfaces of the respective first and second joint portions are positioned in contact with one another. The first and second joint portions are fusion joined. Fusion joining the first and second joint portions forms a fused unitary portion of the first and second thermoplastic components.

Methods of joining and repairing composite components

A method of and system for removing a portion of a thermoplastic component is provided. The component includes a thermoplastic material having a melting temperature. The method includes: a) providing a glider that includes an electrically conductive material operable to produce thermal energy resulting from electrical resistance; b) heating a portion of the glider with electrical energy to a glider operating temperature that is equal or greater than the melting temperature; and c) removing the portion by engaging the component with the glider and translating one of the glider or the component relative to the other. The engagement of the glider and the component causes an amount of the thermoplastic material to melt, and the translation of the one of the glider or the component relative to the other removes the portion from the thermoplastic component.

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San Diego, CA, United States of America

Noushin Bahramshahi