05308228 is referenced by 47 patents and cites 10 patents.

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.

Title
Gas turbine blade comprising layers of composite material
Application Number
7/982945
Publication Number
5308228
Application Date
November 30, 1992
Publication Date
May 3, 1994
Inventor
Catherine L F Guet
Brunoy
FR
Christophe G R Grosbois
Bagneux
FR
Daniel G Girault
Melun
FR
Patrick Fouche
Viry-Chatillon
FR
Laurent J P David
Limours
FR
Bruno J G Dambrine
Chartrettes
FR
Joel M D Benoit
Cesson La Foret
FR
Agent
Oblon Spivak McClelland Maier & Neustadt
Assignee
Societe Nationale d Etude et de Construction de Moteurs d Aviation S N E C M A
FR
IPC
F04D 29/38
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