A splice assembly 100 includes a first splice bracket 102a including first longitudinal axis Xa, a first connecting member 104a, and a first mating member 106a extending from the first connecting member 104a along the first longitudinal axis Xa, the first mating member 106a including a first mating surface 108a disposed at a non-zero first angle relative to the first longitudinal axis Xa. The disclosed slice assembly 100 further includes a second splice bracket 102b including second longitudinal axis Xb, a second connecting member 104b, and a second mating member 106b extending from the second connecting member 104b along the second longitudinal axis Xb, the second mating member 106b including a second mating surface 108b disposed at a non-zero second angle relative to the second longitudinal axis Xb. The first mating surface 108a and the second mating surface 108b are in contact for connecting the first splice bracket 102a and the second splice bracket 102b together.
SPLICE ASSEMBLY FOR JOINING STRUCTURAL COMPONENTS
VERBINDUNGSEINHEIT FÜR DAS ZUSAMMENFÜGEN VON BAUTEILEN
ENSEMBLE D'ÉPISSURE POUR L'ASSEMBLAGE DE COMPOSANTS STRUCTURELS
2018-06-06
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |