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