Provided is a structure manufacturing device (100) including a constant-current power supply (10) that is configured to apply a current having a predetermined current value to a gap that is present between a composite material (31) and a bolt (32), each having conductivity, and has a higher electrical resistance than the composite material (31) and the bolt (32) in order to decrease the electrical resistance of the gap.
STRUCTURE MANUFACTURING DEVICE AND STRUCTURE MANUFACTURING METHOD
2018-03-22
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / F16B DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES , Vorrichtungen zum Befestigen oder Sichern von Konstruktionselementen oder Maschinenteilen, z.B. Nägel, Bolzen, Schrauben, Sprengringe, Klemmen, Klammern oder Keile |
STRUCTURE MANUFACTURING DEVICE, STRUCTURE MANUFACTURING METHOD, AND STRUCTURE
Europäisches Patentamt | 2016
|STRUCTURE MANUFACTURING DEVICE AND STRUCTURE MANUFACTURING METHOD
Europäisches Patentamt | 2020
|