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| Number | Title | Issue Date |
| 4416434 | Blade section for rotating wings of an aircraft The present invention relates to a blade section for rotating wings of an aircraft comprising, between the leading edge and the trailing edge, a convex lower surface and an upper surface which is convex over the greater part of its length, but concave nea... | 11/22/1983 |
| 4392781 | High performance blade for helicopter rotor The present invention relates to a high performance blade for helicopter rotor presenting an aerodynamic surface produced by profiles of which the aerodynamic twist increases from the end profile towards the root profile and is then reversed and becomes z... | 07/12/1983 |