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Gallois
Christophe Gallois, Chateauneuf Sur Loire FR
Philippe Gallois, Corbeil Essonnes FR
| Patent application number | Description | Published |
|---|---|---|
| 20090308506 | METHODS FOR HEAT TREATING AND MANUFACTURING A THERMOMECHANICAL PART MADE OF A TITANIUM ALLOY, AND THERMOMECHANICAL PART RESULTING FROM THESE METHODS - A method of heat treating a thermomechanical part made of a TA6Zr4DE titanium alloy. A solution-annealing is performed at a temperature lying in the range beta transus −20° C. and beta transus −15° C. for a duration lying in the range four hours to eight hours. The method is applicable to fabricating high pressure compressor disks. | 12-17-2009 |
Valérie Gallois, Paris FR
| Patent application number | Description | Published |
|---|---|---|
| 20100204184 | Phosphonates useful as modulators of T-gamma-9-delta-2 activity - The invention concerns novel phosphonate derivatives, preparation method, use thereof as ligands modulating T γ9δ2 lymphocyte activity and pharmaceutical compositions comprising them. | 08-12-2010 |
Valérie Gallois, Paris FR
| Patent application number | Description | Published |
|---|---|---|
| 20100204184 | Phosphonates useful as modulators of T-gamma-9-delta-2 activity - The invention concerns novel phosphonate derivatives, preparation method, use thereof as ligands modulating T γ9δ2 lymphocyte activity and pharmaceutical compositions comprising them. | 08-12-2010 |
Yann Gallois, Frasnoy FR
| Patent application number | Description | Published |
|---|---|---|
| 20110174482 | COMPONENT FOR DRILLING AND OPERATING HYDROCARBON WELLS - A component used for drilling and operating hydrocarbon wells which is substantially tubular in form, and including a first end configured to be connected to a second end of another component also used for drilling and operating hydrocarbon wells. The first end includes a terminal portion including a first abutment surface configured to cooperate by interference with a corresponding abutment surface on the second end, and including a sealing surface configured to cooperate by interference with a corresponding sealing surface on the second end, the terminal portion being preceded by a threaded zone configured to be made up into a corresponding threaded zone of the second end. A compressible volume is provided in the thickness of the first terminal portion and partially beneath the sealing surface, to reduce radial stiffness of the terminal portion by at least 20%, while conserving at least 60% of axial stiffness. | 07-21-2011 |