Method of preparing the connection between two fuselage...

B - Operations – Transporting – 23 – B

Patent

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Details

B23B 35/00 (2006.01) B21J 15/14 (2006.01) B23P 19/04 (2006.01) B64F 5/00 (2006.01)

Patent

CA 2707110

The present invention relates to a method of preparating the connection of two fuselage sections (2,3). A less complicated and time consuming method was found by using High-Speed- Drilling (HSD) for a group of final bore holes through the outer skin of at least one fuselage section and/or the coupling means using one drilling template preferably without any pilot drilling.

La présente invention se rapporte à un procédé de préparation du raccordement de deux sections de fuselage (2, 3). Un procédé moins compliqué et plus rapide a été trouvé grâce à l'utilisation du perçage à grande vitesse (HSD) pour un groupe de trous d'alésage finals à travers le revêtement extérieur d'au moins une section de fuselage et/ou des moyens de couplage utilisant un gabarit de perçage de préférence sans aucun perçage pilote.

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