PROBLEM TO BE SOLVED: To provide a structure manufacturing device and a structure manufacturing method for manufacturing a structure, in which the occurrence of a spark due to a thunderbolt is suppressed without increasing the weight of a structure and the labor of a quality management.SOLUTION: A structure manufacturing device 100 comprises a constant current source 10 existing between a composite material 31 and a bolt 32 individually having electric conductivities, for lowering the electric resistance value of a clearance by applying an electric current of a predetermined value to a clearance of a higher electric resistances than those of the composite material 31 and the bolt 32 thereby to lower the electric resistance of the clearance.SELECTED DRAWING: Figure 1
【課題】構造体の重量増加や品質管理の労力を増大させることなく落雷による火花(スパーク)の発生を抑制した構造体を製造する構造体製造装置および構造体製造方法を提供する。【解決手段】それぞれ導電性を有する複合材料31およびボルト32の間に存在するとともに複合材料31およびボルト32よりも電気抵抗値の高い間隙に所定電流値の電流を印加して間隙の電気抵抗値を低下させる定電流源10を備える構造体製造装置100を提供する。【選択図】図1
STRUCTURE MANUFACTURING DEVICE, STRUCTURE MANUFACTURING METHOD, AND STRUCTURE
構造体製造装置、構造体製造方法、および構造体
2016-11-10
Patent
Electronic Resource
Japanese
IPC: | 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 / 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 / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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