Abstract: A method for preparing carbon nanotubes, nanofibres or nanofilaments by decomposition of at least one carbon precursor in the presence of a catalyst, in which method continuously:—a first gas stream comprising a precursor of a catalyst is brought into contact with a porous substrate (43);—a second gas stream comprising at least one carbon precursor is brought into contact with said porous substrate (43);—said porous substrate (43) is heated to a temperature leading to the deposition of catalyst particles and to the catalytic growth of carbon nanotubes.

Abstract: A method for preparing a cable formed of carbon nanotubes, comprising decomposing at least one carbon precursor compound and at least one precursor compound of a catalyst on a porous substrate (43), in which method continuously: —a first gas stream comprising a precursor of a catalyst is brought into contact with a porous substrate (43); —a second gas stream comprising at least one carbon precursor is brought into contact with said porous substrate (43); —said porous substrate (43) is heated to a temperature leading to the deposition of catalyst particles and the catalytic growth of a carbon nanotube bundle, and preferably between 500° C. and 1000° C.

Abstract: A method for preparing a cable formed of carbon nanotubes, comprising decomposing at least one carbon precursor compound and at least one precursor compound of a catalyst on a porous substrate (43), in which method continuously:—a first gas stream comprising a precursor of a catalyst is brought into contact with a porous substrate (43);—a second gas stream comprising at least one carbon precursor is brought into contact with said porous substrate (43);—said porous substrate (43) is heated to a temperature leading to the deposition of catalyst particles and the catalytic growth of a carbon nanotube bundle, and preferably between 500° C. and 1000° C.

Abstract: A method for preparing carbon nanotubes, nanofibres or nanofilaments by decomposition of at least one carbon precursor in the presence of a catalyst, in which method continuously:—a first gas stream comprising a precursor of a catalyst is brought into contact with a porous substrate (43);—a second gas stream comprising at least one carbon precursor is brought into contact with said porous substrate (43);—said porous substrate (43) is heated to a temperature leading to the deposition of catalyst particles and to the catalytic growth of carbon nanotubes.

Abstract: The invention relates to a method for continuously manufacturing aligned nanostructures on a running support, which comprises conveying the support through a heated space and synthesising, in this space, aligned nanostructures on the support by catalytic chemical vapour deposition. The heated space is divided into n consecutive zones in the conveying direction of the support (n being an integer ?2), and the synthesis of the nanostructures results from heating and injection operations, in each of these n zones, of a flux of an aerosol containing a catalytic precursor and a source precursor of the material of the nanostructures to be formed, carried by a carrier gas. The injection operations are made by modifying, in at least two of the n zones, at least one parameter chosen among the flow rate of the carrier gas flux, the chemical composition of the carrier gas, the mass concentration of the catalytic precursor in the catalytic precursor and source precursor mixture.

Abstract: A method for preventing, reducing and/or eliminating the fouling of a composite material is provided, the composite material comprising (1) a plurality of conductive or semiconductive nanotubes, which are aligned parallel to one another, and (2) a matrix arranged between the conductive or semiconductive nanotubes, the composite material in the form of an isoporous membrane with nanopores which correspond to the pores of the conductive or semiconductive nanotubes and optionally to the pores of the matrix arranged between the conductive or semiconductive nanotubes, the method comprising applying an electric field to the composite material, wherein the fouling is prevented, reduced and/or eliminated at the surface, at and in the pores of the composite material.

Abstract: An aircraft engine module handling assembly including a carriage, a pivoting portion at a top of the carriage, a module support tooling, and an additional mechanism for assembly of the tooling on the pivoting portion, such that the module can be rotated from an original vertical position, observed when it reaches an assembly shop in a crate, to a horizontal position suitable for its assembly with another module of an engine.

Abstract: A device for cutting a structure including nanotubes, including: a mechanism to polarize linearly laser pulses emitted in a direction of the structure, wherein a duration of the laser pulses is roughly between 1 femtosecond and 300 femtoseconds; and a mechanism to focus the linearly polarized laser pulses on the structure.

Abstract: The present invention concerns a device comprising (i) a composite material comprising (1) a plurality of conductive or semiconductive nanotubes, and (2) a matrix arranged between these nanotubes and (ii) means allowing said composite material to be subjected to an electric field. The present invention also concerns the uses of said device in particular to defoul or to modify a composite material and to electroporate at least one cell.

Abstract: A carriage configured to transport an aircraft engine module from a preparation station to an assembly station includes, on a dolly, a reinforcement structure configured to be made horizontally mobile by sliding on balls, two vertically mobile brackets, and moving fingers to slide under the module's supports. The module is then supported by the carriage in a safe manner, can be raised and transported, and can also be temporarily overturned to check that its interior is empty.

Abstract: A device for cutting a structure including nanotubes, including: a mechanism to polarize linearly laser pulses emitted in a direction of the structure, wherein a duration of the laser pulses is roughly between 1 femtosecond and 300 femtoseconds; and a mechanism to focus the linearly polarized laser pulses on the structure.

Abstract: The present invention relates to a material comprising (i) nanotubes or nanowires aligned with each other in a vertical matrix and (ii) a matrix arranged between the nanotubes or the nanowires, at least one organic polymer being covalently grafted to at least two of said nanotubes or to at least two of said nanowires. The present invention also relates to a method for preparing such a material or to its uses.

Abstract: A carriage configured to transport an aircraft engine module from a preparation station to an assembly station includes, on a dolly, a reinforcement structure configured to be made horizontally mobile by sliding on balls, two vertically mobile brackets, and moving fingers to slide under the module's supports. The module is then supported by the carriage in a safe manner, can be raised and transported, and can also be temporarily overturned to check that its interior is empty.

Abstract: An aircraft engine module handling assembly including a carriage, a pivoting portion at a top of the carriage, a module support tooling, and an additional mechanism for assembly of the tooling on the pivoting portion, such that the module can be rotated from an original vertical position, observed when it reaches an assembly shop in a crate, to a horizontal position suitable for its assembly with another module of an engine.