Patent application number | Description | Published |
20090311452 | PROCESS OF DECORATING A TRANSPARENT OR TRANSLUCENT BOTTLE - A method for decorating a glass or plastic transparent or translucent bottle, for the cosmetic field, for containing a cosmetic product such as a perfume, or the like, the decoration of which is carried out inside the bottle, and which consists in making at least one coating onto the inner surface of the bottle, by spraying a liquid mist inside the bottle, characterised in that the liquid is chemically inert with a characteristic close to glass so that the inner coating forms a barrier protecting layer for protecting the cosmetic product from any possible migration detrimental to the fragrance and/or colour as wells as the preservation thereof. | 12-17-2009 |
20130118947 | PROCESS OF DECORATING A TRANSPARENT OR TRANSLUCENT BOTTLE - A method for decorating a glass or plastic transparent or translucent bottle, for the cosmetic field, for containing a cosmetic product such as a perfume, or the like, the decoration of which is carried out inside the bottle, and which consists in making at least one coating onto the inner surface of the bottle, by spraying a liquid mist inside the bottle, characterised in that the liquid is chemically inert with a characteristic close to glass so that the inner coating forms a barrier protecting layer for protecting the cosmetic product from any possible migration detrimental to the fragrance and/or colour as wells as the preservation thereof. | 05-16-2013 |
Patent application number | Description | Published |
20140368408 | SUBREFLECTOR OF A DUAL-REFLECTOR ANTENNA - A subreflector of a dual-reflector antenna comprises a first extremity comprising a convex inner surface, a second extremity adapted for coupling to the extremity of a waveguide, and a body extending between the first extremity and the second extremity. The body comprises a first dielectric part having a portion penetrating into the waveguide and a portion outside the waveguide, and a second metallic part comprising a first cylindrical portion, contiguous with the first extremity of the subreflector, whose diameter is greater than the portion outside the waveguide of the first dielectric part, and a second cylindrical portion, adjacent to the first cylindrical portion, extended by a conical portion that penetrates into the first dielectric part. The first cylindrical portion features a flat ring-shaped surface that forms an angle less than 90° with the axis of the subreflector so as to face the primary reflector. | 12-18-2014 |
20150249281 | JOINING DEVICE FOR FASTENING A RADOME ONTO AN ANTENNA REFLECTOR - A joining device to enable the fastening of a rigid flat radome onto a circular-opening reflector comprises an upper brace applied to one outward-turned side of the radome and covering the peripheral segment of the reflector and radome, a lower brace placed against the face of the reflector opposite the radome, and a rigid spacer comprising and joined with a pad disposed between the reflector and the radome, at least one cylinder leaving a through-hole for a means of fastening the radome onto the reflector, and at least one peg mating with the radome. The upper brace covers the peg and comprises an orifice for putting the cylinder through. In an antenna comprising a circular-opening reflector, a rigid flat radome comprising a plurality of holes on its periphery, and such a joining device, only some of the holes of the radome are used to allow a means of fastening through. | 09-03-2015 |
20160087345 | RADOME FOR AN ANTENNA WITH A CONCAVE-REFLECTOR - A radome for a concave-reflector antenna is fastened directly onto the reflector's edge. The inner surface of the radome comprises at least one absorbent part partially covering its surface area and disposed along its peripheral edge. The surface area of the radome covered by the absorbent part(s) is less than 15% of the total surface area. The radome may comprise two absorbent parts in diametrically opposite positions. Each absorbent part may have a substantially triangular shape, the base of the absorbent part being rounded along the radome's edge, and a portion of its surface area having been removed laterally from each side of the triangle in a circular arc cut-out. | 03-24-2016 |
Patent application number | Description | Published |
20110076133 | TURBOMACHINE COMPRESSOR WITH AN AIR INJECTION SYSTEM - A turbomachine or high pressure compressor including a stator casing housing a plurality of compression stages that are spaced apart in an axial direction along the central axis of the turbomachine, each compression stage including a row of rotor blades followed by a row of stator vanes. The compressor further includes an air injection system including at least one air injection passage through the casing and including an outlet segment that opens out in an inclined manner upstream from and directed towards a row of rotor blades into a set-back zone of the inside face of the casing. | 03-31-2011 |
20120003085 | COMPRESSOR CASING WITH OPTIMIZED CAVITIES - The invention relates to a compressor for a turbine engine including a casing ( | 01-05-2012 |
20120201654 | TURBINE ENGINE COMPRESSOR HAVING AIR INJECTIONS - A turbine engine compressor, including a first housing for supporting injectors, a second housing arranged around the first housing while forming with the first housing an annular space therewith, and a plurality of air injectors each mounted in recesses. Each air injector includes at least one inner air injection channel which leads, on one side, into an outflow jet of the gas stream and, on the other side, into the space formed between the recesses, and, at an upstream end, an upstream rim having an inner surface radially bearing against an upstream rim of the corresponding recess of the first housing and an outer surface radially bearing against an inner surface of the second housing. A mechanism clamping the upstream rim of the air injectors between the housings enables the air injectors to be held in position in the recesses of the first housing. | 08-09-2012 |
20130022452 | ENGINE COMPRESSOR, PARTICULARLY AIRCRAFT JET ENGINE COMPRESSOR, FITTED WITH AN AIR BLEED SYSTEM - A compressor including at least one cascade of fixed vanes, the vanes of which are mounted on a wall and between them form air-flow passages, and an air bleed system which bleeds air from the passages between two vanes, through openings made in the wall, the openings being discontinuous and each including a plurality of orifices arranged one behind the other in a direction of the air flow. An upstream orifice of each opening has a larger cross-sectional area than downstream orifices of the opening, and a number and cross section of the downstream orifices are adjusted to suit a predetermined bleed-off flow rate. | 01-24-2013 |