DocumentCode :
2674231
Title :
Electrical contacts on nickel plated aluminium: the state of the art
Author :
Lefebvre, J. ; Galand, J. ; Marsolais, R.M.
Author_Institution :
Centre de Recherches de Voreppe, France
fYear :
1990
fDate :
20-24 Aug 1990
Firstpage :
454
Lastpage :
460
Abstract :
A direct nickel plating procedure for aluminum is described. It is shown that the main disadvantage of aluminum as far as electrical applications are concerned, namely its unstable contact properties, can be cured by direct nickel plating. This economical solution meets all standards, including the highly demanding standards of the airplane industries. Untreated aluminum surfaces and coated aluminium are considered. Instead of the several steps imposed by the standard procedures, the procedure requires only two basic steps: surface activation and electroplating. The electrolytes are selected so as to warrant pure nickel layers free of residual internal stresses. The method (developed for wires) through liquid contacts allows high current densities, thereby a rapid plating (typically 1 μm/s) and a high yield. The nickel layer obtained with this procedure is globular, with nodules about 0.5 μm in diameter, which favors better electrical contacts. The improved properties brought by recent developments of this technology are discussed, and the severe certification tests performed for use on airplanes are reported. In particular, the test conditions were: 500 heat cycles, tang current densities in the vicinity of 150 A/cm2, (up to 250 A/cm2), connector lug temperature up to 165°C, and cable temperature near 210°C
Keywords :
aerospace industry; aluminium; electrical contacts; electroplated coatings; environmental testing; nickel; 165 C; 210 C; Al substrate; Ni plating; Ni-Al; aircraft industries; airplane industries; cable temperature; connector lug temperature; economical solution; electrical contacts; electrolytes; electroplating; globular Ni layer; heat cycles; high yield; pure Ni layers; rapid plating; severe certification tests performed; state of the art; stressfree layers; surface activation; tang current densities; temperature cycling; test conditions; two step electroplating process; Airplanes; Aluminum; Contacts; Current density; Industrial economics; Internal stresses; Nickel; Temperature; Testing; Wires;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electrical Contacts, 1990. Proceedings of the Thirty-Sixth IEEE Holm Conference on ... and the Fifteenth International Conference on Electrical Contacts
Conference_Location :
Montreal, Que.
Type :
conf
DOI :
10.1109/HOLM.1990.113043
Filename :
113043
Link To Document :
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