| 摘要 |
<p>#CMT# #/CMT# The frame element (10) has a pair of longitudinal parallel struts (12,14) that extend parallel to the ribs of the aircraft structure (36), when the frame element is mounted to the aircraft structure. A storage bin (26) is fastened at desired position along the longitudinal ribs of the frame element. #CMT# : #/CMT# An independent claim is included for method for installing storage bin in aircraft. #CMT#USE : #/CMT# Frame element for use in installation of storage bin in aircraft. #CMT#ADVANTAGE : #/CMT# The number of fastening points to be provided on the aircraft structure for storage bin can be reduced, and the flexibility during installation of the storage bin can be improved, by using the frame element. #CMT#DESCRIPTION OF DRAWINGS : #/CMT# The drawing shows a three-dimensional view of the frame element. 10 : Frame element 12,14 : Struts 18 : Connection strut 26 : Storage bin 36 : Aircraft structure.</p> |
