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Culot
Benedicte Culot, Jemeppe-Sur-Sambre BE
| Patent application number | Description | Published |
|---|---|---|
| 20080206125 | Catalyst System for a Multi-Walled Carbon Nanotube Production Process - The present invention relates to a catalyst system for the selective conversion of hydrocarbons into multi-walled carbon nanotubes and hydrogen comprising a compound of the formula: (Ni,Co)Fe | 08-28-2008 |
| 20080213160 | Method of Synthesising a Support Catalyst for the Production of Carbon Nanotubes - The present invention relates to a method for synthesising a catalyst with a view to the production of multi-wall nanotubes comprising the following stages: | 09-04-2008 |
Louis J. Culot, Boston, MA US
| Patent application number | Description | Published |
|---|---|---|
| 20080306966 | Deriving Product Information - A method and a system determine that product information acquired from an electronic catalog includes a product identifier and chemical structure information that is associated with the product identifier. A substance identifier and a quality identifier for a chemical product are derived from product information for a chemical product, and a product identifier for the chemical product is derived from the substance identifier and the quality identifier. | 12-11-2008 |
Yves Culot, Liege BE
| Patent application number | Description | Published |
|---|---|---|
| 20110002787 | Blade Retention at a Compressor Rectifier Stage for Impact Resistance - A rectifier stage of an axial turbine engine compressor is placed directly downstream of the input blower of a turbo-reactor or turboshaft engine compressor. The blade roots of the rectifier stage are housed inside the inner shroud by insertion into respective slots. The blade roots include at least one opening protruding from the slot of the shroud, so as to receive a spiral ring having at least two loops so as to prevent the blade roots from escaping from the respective slots of the inner shroud, and so as to form a connection between the blade roots. A method for retaining blades of a rectifier stage of an axial turbine engine compressor on an inner shroud, in particular a rectifier stage placed directly downstream of the input blower of a turbo-reactor or turboshaft engine compressor, includes positioning a spiral ring having at least two loops inside the openings of the blade roots by threading one end of the ring successively into the openings until all of the spirals of the ring are housed inside the openings. | 01-06-2011 |