DEVICE FOR RIVETING OF AIRCRAFT FUSELAGE Russian patent published in 2017 - IPC B21J15/14 B21J15/32 B23P19/06 B25B23/14 B64F5/00 

FIELD: physics, instrument engineering.

SUBSTANCE: head (25) of the device for riveting with HI-LITE-type rivets of the structure components and with the possibility of automatic installation of the pun supported heads (13) (11) previously inserted into the structure. The head (25) contains: a tool (31, 31 ') for installation of the head; means (41, 45, 55) for inserting the head into the tool (31, 31 ') for installation of the head thereof; means (35) actuating the tool; means of the linear movement during the screwing operation; means (57, 45) for the removal of the second part (17) of the head (13); control means for automatic installation of the heads (13) on the pins (11), and then for the removal of the second portion (17) using the tools (31, 31 ') and the heads(13) suitable for the pins (11). The robot has a head (25) as the operating entity. The process of the aircraft fuselage riveting for the two components is characterized by the use of the robot.

EFFECT: invention provides the simplification of the riveting process of the aircraft fuselage components.

15 cl, 7 dwg