公开(公告)号：EP3028940B1

公开(公告)日：2018-06-06

申请号：EP15196204.0

申请日：2015-11-25

申请人： The Boeing Company

发明人： Reeves, Andrew C.

IPC分类号： B64C1/06 ,  B64C1/12

CPC分类号： B64C1/069 ,  B64C1/061 ,  B64C1/064 ,  B64C1/12 ,  Y10T29/49622

摘要： A splice assembly (100) may include 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 splice assembly (100) may further include 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 complementary. Surface contact between the first mating surface (108a) and the second mating surface (108b) defines a fastening location for connecting the first splice bracket (102a) and the second splice bracket (102b).