Abstract: A monitoring camera that includes: an optical sensor; a light source; first and second printed circuit boards, attached to the optical sensor and the light source respectively; a first electrical device, attached to the first printed circuit board and connected to the optical sensor; a second electrical device, attached to the second printed circuit board and connected to the light source; a casing joined to the first and second printed circuit boards; and an electrical connector. The first printed circuit board has a through cut; and the electrical connector is arranged in the cut so as to be connected simultaneously to the first and second electrical devices.

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 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 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 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.