Abstract: The present invention relates to methods and kits for prognosing, treating, and managing treatment of cancer in a subject. The methods involve selecting a subject having cancer and obtaining, from the selected subject, a sample containing exosomes or an S100 molecule containing sample. The exosomes or S100 molecule containing sample, respectively, are then contacted with one or more reagents suitable to detect higher or lower levels or the presence or absence of one or more integrins on said exosomes or higher or lower levels or the presence or absence of one or more S100 molecules in the S100 molecule containing sample. The cancer is then prognosed, treatment is administered, or treatment is managed.

Abstract: The present invention relates to a use of extracellular membrane vesicles of at least one probiotic for preventing or reducing the formation of a biofilm on the surface of a material. The present invention also relates to a method for treating a surface of a material in order to prevent or reduce the formation of a biofilm on the surface, the method comprising a step of bringing extracellular membrane vesicles derived from at least one probiotic into contact with the surface. The present invention further relates to a material comprising extracellular membrane vesicles of at least one probiotic on its surface, or into which extracellular membrane vesicles of at least one probiotic are incorporated.

Abstract: The present disclosure relates to a natural deep eutectic mixture for extraction of biocomponents comprising two different solvents, wherein a first solvent is selected from a list consisting of: lactic acid, and glycerol, citric acid, maleic acid, and tetrabutylammonium bromide and a second solvent is selected from a list consisting of: sodium lactate, sodium citrate, transcutol, glycine, glycerol, oleic acid, sodium lactate, decanoic acid; further comprising up to 90% (w/w) in water. The disclosure also relates to a method to obtain an extract from a natural source material using the NADES, as well as compositions comprising the NADES, the obtained extract and/or a topical active compound. The use of said compositions as cosmetic formulations is also described.

Abstract: Multiple features of seating assemblies are detailed Innovations in or to tray tables, luggage bars, arm rests, seat backs, and seat frames are included, with features being incorporated into seating assemblies either separately or in any combination. The assemblies are configured principally for passenger aircraft but may be used elsewhere as appropriate or desired.

Abstract: Multiple features of seating assemblies are detailed Innovations in or to tray tables, luggage bars, arm rests, seat backs, and seat frames are included, with features being incorporated into seating assemblies either separately or in any combination. The assemblies are configured principally for passenger aircraft but may be used elsewhere as appropriate or desired.

Abstract: Multiple features of seating assemblies are detailed. Innovations in or to tray tables, luggage bars, arm rests, seat backs, and seat frames are included, with features being incorporated into seating assemblies either separately or in any combination. The assemblies are configured principally for passenger aircraft but may be used elsewhere as appropriate or desired.

Abstract: A turbine or compressor stage for a turbomachine is disclosed. The stage includes a blade wheel surrounded by a sectorized ring carried by a casing. Each ring sector includes a circumferential rim that is clamped radially a casing rail by two clamps of C-shaped section that are engaged on the circumferential end portions of the rim of the ring sector and on the corresponding portions of the casing rail.

Abstract: A turbojet turbine or compressor stage is disclosed. The stage includes at least one rotor disk mounted inside a sectorized ring supported by a casing and including a circumferential flange radially clamped on an annular rail of the casing by a substantially C-shaped cross-section annular locking device which is axially engaged on the casing rail and on the flange of the ring. A substantially cylindrical heat shielding foil is interposed between the ring and the device. The foil or the device includes at least one extra thickness which respectively bears on the device, or the foil, to radially immobilize this foil.

Abstract: A locking member for a device for fastening ring sectors to an aircraft turbine engine casing is disclosed. The member has first and second clamping branches, which are connected together by curving joining portions, via a connecting branch. The joining portion of center thickness E1 has an inside surface of mean radius Rm1, and the joining portion of center thickness E2 has an inside surface of mean radius Rm2. Thickness E1 is strictly smaller than thickness E2, and mean radius Rm1 is strictly smaller than mean radius Rm2.

Abstract: Multiple features of seating assemblies are detailed. Innovations in or to tray tables, luggage bars, arm rests, seat backs, and seat frames are included, with features being incorporated into seating assemblies either separately or in any combination. The assemblies are configured principally for passenger aircraft but may be used elsewhere as appropriate or desired.

Abstract: A stage of a turbine or compressor for a turbomachine including at least a vane disk surrounded with a sectorized ring supported by a casing and including a circumferential flange radially clamped on a rail of the casing by substantially C-shaped cross-section locks which are axially engaged on the casing rail and the flange of the ring is disclosed. The inner and outer walls of each lock includes radial bearing surfaces on the flange of the ring and the casing rail, respectively. The bearing surfaces only extend on a part of the width of the lock.

Abstract: This invention relates to a locking member (24) for a device for fastening ring sectors to an aircraft turbine engine casing. The member has first and second clamping branches (28, 30), which are connected together by means of curving joining portions (36a, 36b), via a connecting branch (32), the joining portion (36a) of centre thickness E1 having an inside surface (36a?) of mean radius Rm1, and the joining portion (36b) of centre thickness E2 having an inside surface (36b?) of mean radius Rm2. According to the invention, thickness E1 is strictly smaller than thickness E2, and mean radius Rm1 is strictly smaller than mean radius Rm2.

Abstract: A turbojet turbine or compressor stage, comprising at least one rotor disk mounted inside a sectorized ring (120) supported by a casing (116) and comprising a circumferential flange (132) radially clamped on an annular rail (136) of the casing by a substantially C-shaped cross-section annular locking device (138) which is axially engaged on the casing rail and on the flange of the ring, a substantially cylindrical heat shielding foil (146) being interposed between the ring and the device, the foil, or the device, comprising at least one extra thickness (150) which respectively bears on the device, or the foil, to radially immobilize this foil.

Abstract: A stage of a turbine or compressor for a turbomachine, comprising at least a vane disk (18) surrounded with a sectorised ring (20) supported by a casing (16) and comprising a circumferential flange (34) radially clamped on a rail (38) of the casing by substantially C-shaped cross-section locks (40, 140) which are axially engaged on the casing rail and the flange of the ring, the inner (144) and outer (142) walls of each lock comprising radial bearing means (150, 148) on the flange of the ring and the casing rail, respectively, those bearing surfaces only extending on a part of the width (L) of the lock.

Abstract: A turbine or compressor stage for a turbomachine, the stage comprising a blade wheel surrounded by a sectorized ring carried by a casing, each ring sector including a circumferential rim that is clamped radially a casing rail by two clamps of C-shaped section that are engaged on the circumferential end portions of the rim of the ring sector and on the corresponding portions of the casing rail.

Abstract: An electric motor comprising a rotor secured to a shaft, a stator comprising a cylindrical shell receiving at one at least of the ends a flange provided with a roller bearing for the rotor shaft, the flange being fixed to the cylindrical shell by a fixing means having a bayonet-type assembly, wherein the assembling of the flange onto the shell being achieved through a relative displacement in an axial translation and a rotary relative motion.

Abstract: An electric motor comprising a rotor secured to a shaft, a stator comprising a cylindrical shell receiving at one at least of the ends a casing end flange provided with a roller bearing for the rotor shaft, the said flange being fixed to the cylindrical shell by fixing means, characterized in that the fixing means comprise a bayonet-type assembly, the assembling of the flange onto the shell being achieved through a relative displacement in axial translation and a rotary relative motion.

Abstract: The invention proposes a handle for the door of an automobile vehicle, of the type in which the handle comprises an external gripping lever that is designed to be moved by a user from a rest position to an open position to control a lock that is associated with a lock cylinder of the type comprising a stator, one end of which is accessible from the outside so that a key can be inserted in the lock cylinder through a slit that opens out into the end of the cylinder, wherein the gripping lever comprises a protective cap and/or trim covering the lock cylinder that is assembled so that it is free to slide with respect to the gripping lever between a normal assembly position in which the cap conceals at least the slit in the lock cylinder when the gripping lever is in its rest position, and a displaced position enabling access to the key insertion slit.