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Charier
Gaelle Charier, Zurich CH
| Patent application number | Description | Published |
|---|---|---|
| 20090169539 | PDGF FUSION PROTEINS INCORPORATED INTO FIBRIN FOAMS - Compositions for wound healing, use of the compositions, and kits and methods of using thereof are described herein. In a preferred aspect, the compositions are suitable for use in a method for forming a fibrin matrix or foam that can be applied or injected at the site of need. In another preferred aspect, the compositions are also suitable for use in methods for forming enhanced controlled delivery fibrin matrices that can be administered as gels or foams. | 07-02-2009 |
Gilles Alain Charier, La Grande Paroisse FR
| Patent application number | Description | Published |
|---|---|---|
| 20100104438 | DEVICE FOR CONTROLLING THE PITCH OF FAN BLADES OF A TURBOPROP - The invention relates to a device for controlling the pitch of fan blades of a turboprop. The device includes at least at least one set of adjustable pitch fan blades secured to rotate with a rotary ring centered on a longitudinal axis and mechanically connected to a turbine rotor. Each blade of the set is coupled for pitch-adjustment purposes with a synchronization ring centered on the longitudinal axis, the synchronization ring being suitable for pivoting about the longitudinal axis relative to the rotary ring under drive from actuators carried by the rotary ring and each having a respective axis extending in a direction that is substantially tangential to the synchronization ring. | 04-29-2010 |
Gilles Alain Marie Charier, La Grande Paroisse FR
| Patent application number | Description | Published |
|---|---|---|
| 20090304498 | MULTISTAGE TURBOMACHINE COMPRESSOR - A multistage compressor for a turbomachine, in particular an airplane turboprop or turbojet, the compressor comprising a double-walled casing having an inner wall made up of shrouds surrounding respective annular rows of moving blades and annular rows of straightening stator vanes, said shrouds being connected to the outer wall of the casing by independent suspension means enabling the radial clearances between the outer ends of the moving blades and the shrouds of the inner wall of the casing to be adjusted independently from one compression stage to another. | 12-10-2009 |