Abstract
The Lynx multi-service helicopter, which is being jointly developed by Westland Helicopters Ltd. (W.H.L.) in the U.K., and Societe Nationale Industrielle Aérospatiale, (A.S.) in France, embodies, among many other advanced technology systems, a semirigid rotorhead and an electron beam welded transmission drive shaft in Ti-6A1-4V alloy.
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Stubbington, C.A. and Ballett, J.T., ‘Weld Optimisation and Fatigue Tests on Low Voltage Electron Beam Welded 2 in (51mm) Thick Ti-6A1–4V Alloy“, ibid Session V, Paper 5.
Stubbington, C.A. and Ballett, J.T., “Metallographic and Fatigue Tests on a High Voltage Electron Beam Welded Joint in 2 in (51mm) Thick Ti-6A1–4V Bar”, R.A. E. Technical Report 70204, November 1970.
Bowen, A.W.L. and Stubbington, C.A., “The Effect of Dc-ß Working on the Fatigue and Tensile Properties of Ti-6A1–4V Bars”, ibid Session X, Paper 16.
Stubbington, C.A. and Bowen, A.W.L., “The Effect of Section Size on the Fatigue Properties of Ti-6A1–4V Bars”, ibid Session VIIb, Paper 7.
Mejan, M., “Influence de la Structure sur la Tenue ‘a la Fatigue de l’Alliage de Titane T-A6V”, S.N.I.A.S. Report H/DE.ER 170–81.
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© 1973 Springer Science+Business Media New York
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Wedden, P.R., Liard, F. (1973). Design and Development Support for Critical Helicopter Applications in Ti-6A1-4V Alloy. In: Jaffee, R.I., Burte, H.M. (eds) Titanium Science and Technology. Springer, Boston, MA. https://doi.org/10.1007/978-1-4757-1346-6_7
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DOI: https://doi.org/10.1007/978-1-4757-1346-6_7
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