Continuous fuselage connection

Details Continuous fuselage connection Continuous fuselage connection

B - Operations, Transporting

64

C

B64C 1/26 (2006.01)

Patent

CA 2618858

The present invention relates to a connection system (1) for attaching a tail unit (2) to an attachment surface (3) of an aircraft. In this arrangement the attachment system (1) comprises a mounting (6) with a first bearing surface (17) that is designed to rest against the tail unit (2), and a second bearing surface (18) that is designed to rest against the attachment surface (3). Thereby, the first bearing surface (17) and the second bearing surface (18), of which there is at least one, comprise a common line of contact (16). In this arrangement the planes of the first bearing surface (17) and of the second bearing surface (18) are at an angle that differs from 0~ and 180~.

Système de raccord (1) servant à fixer un empennage de queue (2) à une surface de fixation (3) d~un aéronef. Le système de raccord (1) comprend un châssis (6) présentant une première surface portante (17) conçue pour reposer sur l~empennage de queue (2), et une deuxième surface portante (18) conçue pour reposer sur la surface de fixation (3). La première surface portante (17) et la deuxième surface portante (18), chacune au moins au nombre de un, comprennent une ligne de contact commune (16). Les plans de la première surface portante (17) et de la deuxième surface portante (18) forment un angle différent de 0° et de 180°.

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