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US 5,308,228 AGranted
Gas turbine blade comprising layers of composite material
AssigneeSociete Nationale d'Etude et de Construction de Moteurs d-Aviation (SNECMA)
InventorsJoel M. D. Benoit, Bruno J. G. Dambrine, Laurent J. P. David, Patrick Fouche, Daniel G. Girault, Christophe G. R. Grosbois, Catherine L. F. Guet
Life of this patent
Estimating the term…
Abstract
A gas turbine blade includes a central core covered by a plurality of layers of composite material, and optionally also an outer sleeve of woven composite material. A network of transverse seams pass through the layers of composite material, and preferably also the core and the outer sleeve. This construction is particularly applicable to large diameter turbine blades.
Claims2
A gas turbine blade comprising:
- a central core and a fixing root forming an integral, monolithic single part of the blade, a plurality of layers of a first composite material covering said central core, and a network of transverse seams passing through at least said layers of composite material;
- and
- a sleeve made from a woven composite material, said sleeve having an open end and a closed end and which receives said central core and said layers of composite material covering said core, said network of transverse seams also passing through said sleeve wherein said central core is made from a second composite material and said transverse seams also pass through said core.
Dependencies are inferred from the claim text.