METHOD FOR MANUFACTURING A MULTI-SPAR BOX WITH A CONTINUOUS SKIN UPPER SHELL OF A TAIL CONE SECTION FOR A REAR END OF AN AIRCRAFT AND A COMPOSITE ASSEMBLY

Examples herein relate to a method for manufacturing a composite assembly with a continuous skin for a rear end of an aircraft by obtaining an upper part (405) of the rear end by composite tooling. The upper part comprises a multi-spar vertical tail plane. The spars (410) of the vertical tail plane...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	CANAS RIOS, Maria, Almudena, GARCIA NIETO, Carlos, INIESTA LOZANO, Fernando, MARTINO-GONZALEZ, Esteban, VAZQUEZ CASTRO, Jesus Javier, SANCHEZ PEREZ, Melania, MENARD, Edouard, ARANA HIDALGO, Alberto
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES 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 HELICOPTERS PERFORMING OPERATIONS PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCESIN A PLASTIC STATE 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:	Examples herein relate to a method for manufacturing a composite assembly with a continuous skin for a rear end of an aircraft by obtaining an upper part (405) of the rear end by composite tooling. The upper part comprises a multi-spar vertical tail plane. The spars (410) of the vertical tail plane comprise widening roots that form an upper shell of the rear end and an upper skin (425). Furthermore, a lower part (415) comprises a lower shell of the rear end including semi-complete frames (420) and stringers and a lower skin (430). The upper and lower parts are assembled with a joining procedure. The upper and lower skins are joined to obtain the composite assembly with the continuous skin.