Patent ID: 9499250
Filing Date: 2016-11-22
CPC Classification: B64C,Y02T,Y10T

Claim Text:
1. An aircraft structure arrangement forming a part of a secondary structure of an aircraft and which comprises: a first longitudinal profile, a first frame profile, and a mounting bracket, wherein the mounting bracket is directly attached to both the first longitudinal profile and the first frame profile, and wherein the mounting bracket further is connectable to a component of a primary structure of the aircraft so as to fasten the first longitudinal profile and the first frame profile to the primary structure of the aircraft, wherein the mounting bracket comprises a plurality of attachment portions, each attachment portion serving to attach the mounting bracket to a respective longitudinal profile or frame profile, wherein the number of attachment portions formed on the mounting bracket is adapted to the number of longitudinal and frame profiles attached to the mounting bracket, further comprising at least one of a second frame profile, wherein the mounting bracket is directly attached to the second frame profile, and a second longitudinal profile, wherein the mounting bracket is directly attached to the second longitudinal profile.