ZONAL LAMINATION FOR COMPOSITE PARTS IN MOVING LINE

To provide systems and methods for fabricating composite parts.SOLUTION: The method includes subdividing a laminate into zones, laying up tows of fiber reinforced material for the laminate over a layup mandrel via multiple laminations such that each lamination head applies tows to a different zone,...

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Bibliographic Details
Main Authors JORDAN SETH ERICKSON, DARRELL D JONES, DANIEL R SMITH, RICHARD ALLEN MILLER II, MICHAEL KENNETH-QUE LOUIE
Format Patent
LanguageEnglish
Japanese
Published 31.05.2022
Subjects
AEROPLANES
AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR
SHAPING OR JOINING OF PLASTICS
TRANSPORTING
WORKING OF PLASTICS
WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
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Summary:To provide systems and methods for fabricating composite parts.SOLUTION: The method includes subdividing a laminate into zones, laying up tows of fiber reinforced material for the laminate over a layup mandrel via multiple laminations such that each lamination head applies tows to a different zone, and splicing the zones together to form the laminate during the laying up of the tows.SELECTED DRAWING: None 【課題】複合材部品を製造するためのシステム及び方法を提供する。【解決手段】方法は、積層板をゾーンに小分割すること、各積層ヘッドが異なるゾーンにトウを適用するように、積層板のための繊維強化材料のトウを、複数の積層を介してレイアップマンドレル上にレイアップすること、及びトウのレイアップの間に、積層板を形成するためにゾーンをまとめて接合することを含む。【選択図】なし
Bibliography:Application Number: JP20210183101