COMPOSITE ASSEMBLY FOR UNHARDENED FUSELAGE COMPONENTS

To provide systems and methods for fabricating a preform for a fuselage section of an aircraft.SOLUTION: The method includes advancing a series of arcuate mandrel sections 112 in a process direction through an assembly line 100, mounting a stringer preform 107 onto the arcuate mandrel sections via s...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	PAUL T PRITCHARD, DARRELL D JONES, RAVIENDRA SIDATH SURIYAARACHCHI, DANIEL R SMITH, JEREMY EVAN JUSTICE, JASON A MEDENCIY, STEPHEN KEITH KIRCHMEIER, PAUL CHACE WILCOXSON, ROBERT WILLIAM WHITING, MICHAEL BEERMAN, KURTIS SHULDBERG WILLDEN
Format:	Patent
Sprache:	eng ; jpn
Schlagworte:	AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR 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
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	To provide systems and methods for fabricating a preform for a fuselage section of an aircraft.SOLUTION: The method includes advancing a series of arcuate mandrel sections 112 in a process direction through an assembly line 100, mounting a stringer preform 107 onto the arcuate mandrel sections via stringer placement stations 113, uniting the series of arcuate mandrel sections into a combined mandrel 118; and laying up the fiber reinforced material onto the combined mandrel and stringer preform.SELECTED DRAWING: Figure 1A 【課題】航空機の胴体セクションのプリフォーム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】本方法は、一連の弧状マンドレルセクション１１２を、組立ライン１００を通してプロセス方向に前進させることと、ストリンガ載置ステーション１１３を介して、ストリンガプリフォーム１０７を弧状マンドレルセクション上に載置することと、一連の弧状マンドレルセクションを結合されたマンドレル１１８へと一体化することと、繊維強化材料を結合されたマンドレル及びストリンガプリフォーム上にレイアップすることを含む。【選択図】図１Ａ