Riveting device for aircraft fuselages
A head (25) of a riveting device -for Hi-Lite type rivets- of at least two components of a structure for installing automatically collars (13) on pins (11) previously inserted in the structure is provided. The head (25) comprises: a collar installation tool (31, 31'); collar supply means (41, 4...
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Format: | Patent |
Sprache: | eng ; fre ; ger |
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Zusammenfassung: | A head (25) of a riveting device -for Hi-Lite type rivets- of at least two components of a structure for installing automatically collars (13) on pins (11) previously inserted in the structure is provided. The head (25) comprises: a collar installation tool (31, 31'); collar supply means (41, 45, 55) to said collar installation tool (31, 31'); tool actuating means (35); linear displacement means during the threading operation; withdrawal means (57, 45) of the second part (17) of the collars (13); control means arranged to automatically perform the installation of collars (13) on pins (11) and after this the withdrawal of the second part (17) of it, using tools (31, 31') and collars (13) appropriate for the pins (11). The invention also refers to a robot having as end-effector the head (25) and to a method of riveting two components of an aircraft fuselage. |
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