Abstract: A device for mounting a dividing wall for separating the main air stream and the bypass air in a bypass turbojet engine afterburner is disclosed. The device includes an attachment unit which attaches the upstream end of the wall to a guide vane casing and a supporting unit which supports the downstream end of the wall provided on flame holder arms of the afterburner radially on the inside of the dividing wall.

Abstract: An electron gun includes a sealed chamber under vacuum. A cathode having an emitting face is placed inside the chamber. An anode forms a sealed window, formed facing the emitting face in one of the walls of the chamber. The anode is capable of allowing electrons emitted by the emitting face to pass through. A biasing apparatus sets up a voltage between the anode and the cathode, capable of accelerating these electrons towards the anode, the electrons thus accelerated forming a beam that passes through the anode. The anode and the emitting face each have a curvature, the curvature of the anode making it capable of resisting a pressure difference between the inside and the outside of the chamber and being designed to cooperate with the curvature of the emitting face to focus the electron beam outside the chamber.

Abstract: The turbojet of the invention includes a combustion chamber, a channel for heating the gas stream, where the heating channel includes at least one device for injection of fuel into the gas stream, which includes an open chamber, with a U-shaped section, having at least one wall within which extend fuel-injection means, which inject the fuel in at least one direction. It is characterised by the fact that a cooling jacket is provided in the chamber, alongside the wall forming the base of its U-section, and the fuel injection device includes protection means interposed between the fuel-injection means and the wall, in a fuel-injection direction. Thus, as a result of the invention, the fuel injection device, which is bathed in a very hot environment, is protected against thermal shocks due to the projection of colder fuel onto its walls, and its life expectancy is therefore increased.

Abstract: A double flow turbo-jet engine includes a re-heating channel of the primary flow and an ejection nozzle, the secondary flow emerging at least partially in the primary flow upstream of the re-heating channel, the re-heating channel including a burner ring, including a flame holder gutter in the form of a ring portion whereof the upstream section is situated in the secondary flow, receiving a fuel manifold and a protective tubular screen of the manifold. The gutter includes an upstream recess linked with the secondary flow, and the screen includes, on its upstream section, at least one ventilation orifice of the space situated between the screen and the manifold.

Abstract: A device for fastening a fluid duct such as a fuel duct in an orifice of a turbojet casing, the device comprising a ring screwed into the orifice of the casing and having an annular rim coming to bear against a washer at the end of the duct, and a nut screwed onto the end of the duct so as to clamp the annular rim of the ring against the washer of the duct in order to fasten the duct to the casing.

Abstract: Device for mounting a dividing wall (112) for separating the main air stream and the bypass air in a bypass turbojet engine afterburner, comprising means of attaching the upstream end of this wall to a guide vane casing and means (150) for supporting the downstream end of this wall, these means being provided on flame holder arms (130) of the afterburner radially on the inside of the dividing wall.

Abstract: Electron gun with focussing anode, forming a window of this gun, application to irradiation and sterilisation. This gun comprises a chamber (2) under a vacuum, containing a cathode (6) with an emitting face (8) emitting electrons, and an anode (4) formed in one of the walls of the chamber and transparent to electrons. The anode is curved to resist the pressure difference between the inside and the outside of the chamber. The emitting face is also curved and cooperates with the anode to focus electrons outside the chamber.

Abstract: An apparatus for cutting at least one thin layer from a substrate or ingot forming element for an electronic or optoelectronic or optical component or sensor. This apparatus includes a device for directing a pulse of energy into the substrate or forming element wherein the pulse has a duration shorter than or of the same order as that needed by a sound wave to pass through the thickness of the weakened zone, and the energy of the pulse is sufficient to cause cleavage to take place in the weakened zone as the energy of the pulse is absorbed therein. The apparatus also includes an assembly for holding or orienting the substrate or ingot forming element so that the energy pulse is completely uniformly directed over the entire surface, through the face and into the substrate or ingot forming element to cause cleavage to take place in the weakened zone as the energy of the pulse is absorbed therein.

Abstract: An apparatus for cutting at least one thin layer from a substrate or ingot forming element for an electronic or optoelectronic or optical component or sensor. This apparatus includes a device for directing a pulse of energy into the substrate or forming element wherein the pulse has a duration shorter than or of the same order as that needed by a sound wave to pass through the thickness of the weakened zone, and the energy of the pulse is sufficient to cause cleavage to take place in the weakened zone as the energy of the pulse is absorbed therein. The apparatus also includes an assembly for holding or orienting the substrate or ingot forming element so that the energy pulse is completely uniformly directed over the entire surface, through the face and into the substrate or ingot forming element to cause cleavage to take place in the weakened zone as the energy of the pulse is absorbed therein.

Abstract: A method of cutting at least one thin layer from a substrate or ingot forming element for an electronic or optoelectronic or optical component or sensor. This method includes the steps of forming a weakened zone in the substrate or ingot forming element, wherein the weakened zone has a thickness that corresponds to that of the layer that is to be removed; and directing a pulse of energy into the substrate or forming element wherein the pulse has a duration shorter than or of the same order as that needed by a sound wave to pass through the thickness of the weakened zone. The energy of the pulse is sufficient to cause cleavage to take place in the weakened zone as the energy of the pulse is absorbed therein.

Abstract: The invention concerns a cooling system for a post combustion jet nozzle, The jet nozzle includes a primary gas duct allowing a primary flow of gas, and a secondary air duct allowing a secondary flow of air. The secondary air duct surrounds the primary gas duct and is separated from it by a protective thermal shroud. The secondary air duct has a downstream end, and dampers surrounding an output section of the primary gas duct. The system includes a protective thermal shell in the secondary air duct, at the downstream end of said duct. The protective thermal shell bears an annular diaphragm extending out in front of the dampers and being provided with support sectors and inter-sector zones equipped with slots. The inter-sector zones define spaces between the diaphragm and the protective thermal shroud.

Abstract: A high frequency transformer may include an integrated rectifier cell with flat windings and/or slotted copper segments stacked on a core branch to provide alternating primary and secondary windings. This reduces inductance leakage and thus increases the operating frequency of the transformer. Rectifying diodes of the rectifier cell may be arranged according to various configurations between the copper segments, and the collection plates may form one of the rectifier outputs. The other output may be provided by connecting all the midpoints of the windings with conductive spacers pressed together along a first axis. The invention is particularly advantageous in static converters, and, more particularly, in spot welding machines, for example.

Abstract: The invention concerns a cooling system for a post combustion jet nozzle (1), said jet nozzle comprising a primary gas duct (2) allowing a primary flow of gas, a secondary air duct (3) allowing a secondary flow of air, said secondary air duct surrounding the primary gas duct and separated from it by a protective thermal shroud (4), said secondary air duct having a downstream end (3a), dampers (5) surrounding an output section of the primary gas duct, the system comprising a protective thermal shell (7) in the secondary air duct, at the downstream end of said duct. According to the invention, the protective thermal shell bears an annular diaphragm (8) extending out in front of the dampers and being provided with support sectors (11) and inter-sector zones equipped with slots, said inter-sector zones defining spaces between the diaphragm and the protective thermal shroud.

Abstract: A method of cutting at least one thin layer from a substrate or ingot forming element for an electronic or optoelectronic or optical component or sensor. This method includes the steps of forming a weakened zone in the substrate or ingot forming element, wherein the weakened zone has a thickness that corresponds to that of the layer that is to be removed; and directing a pulse of energy into the substrate or forming element wherein the pulse has a duration shorter than or of the same order as that needed by a sound wave to pass through the thickness of the weakened zone. The energy of the pulse is sufficient to cause cleavage to take place in the weakened zone as the energy of the pulse is absorbed therein.

Abstract: A high frequency transformer may include an integrated rectifier cell with flat windings and/or slotted copper segments stacked on a core branch to provide alternating primary and secondary windings. This reduces inductance leakage and thus increases the operating frequency of the transformer. Rectifying diodes of the rectifier cell may be arranged according to various configurations between the copper segments, and the collection plates may form one of the rectifier outputs. The other output may be provided by connecting all the midpoints of the windings with conductive spacers pressed together along a first axis. The invention is particularly advantageous in static converters, and, more particularly, in spot welding machines, for example.

Abstract: In order to form separate particles from a flowable mass, the flowable mass is fed through a pipe and extruded through holes formed along a longitudinal axis thereof. The pipe is oscillated by an agitator in a direction transversely of the longitudinal axis to cause the extruded mass to be sheared-off in the form of particles. Stop members can be positioned adjacent respective sides of the pipes to be contacted by the pipe and thereby define change-of-direction points for the pipe during its oscillation. The agitator may include piezoelectric ceramics attached to the stop members.

Abstract: An electron accelerator for accelerating a first electron beam includes a resonant cavity, a source of electromagnetic energy for supplying the resonant cavity at a resonant frequency of the resonant cavity and for forming a second electron beam and injecting the second electron beam into the resonant cavity. The second electron beam is decelerated by the electromagnetic fields of the resonant cavity and the first electron beam is in phase opposition to the second electron beam.

Abstract: Electrostatic accelerator includes an accelerating column (20), a high voltage terminal (18) located at one end of said accelerating column and electric charge transport means, said transport means incorporating a high frequency accelerator such as a high frequency electron accelerator (54) able to supply an electron beam and means (56) for supplying the electron beam to the high voltage terminal, said electric charges being constituted by the electrons supplied by said high frequency accelerator.

Abstract: An electric pulse generator for the formation of high power electric pulses. The generator includes a capacitor having coaxial electrodes and a coaxial electrode shaping line. Magnetic compression means include the capacitor for charging the shaping line and a magnetic switch with a saturable inductor for discharging the shaping line. This arrangement reduces parasitic inductances and provides a generator having a compact, simple structure which is less expensive than known generators.

Abstract: Electric pulse generator having at least one capacitor in the form of a coaxial line section and a saturatable inductance coil serving as a switch. According to the invention, the saturatable inductance coil is located within the internal conductor of the coaxial line.