Abstract: A valve assembly for high pressure applications includes a pre-charge chamber, at least one inlet for pressurized gas to enter the assembly, a system poppet and an outlet for releasing pressurized gas into a desired environment. Pressurized gas can flow through access channels into a single bellows, which expands to move a shaft connected to the system poppet to open the poppet. In another embodiment, the pre-charge chamber compresses a first bellows to expand a second bellows, and vice versa upon reciprocation. The two bellows are hydraulically connected and filled with incompressible fluid. Each bellows has an internal limiting valve to retain incompressible fluid therewithin, and to preclude the complete nesting of either of the bellows. The retained fluid within the bellows maintains an internal pressure to minimize differential pressure, thereby minimizing the risk of bellows failure.

Abstract: The invention relates to a rear casing for a turbine engine comprising a primary body generating a primary flow (10) to be ejected through a primary nozzle (6), said rear casing (7) being shaped so as to be positioned downstream from the primary body and to define, on the inside of the turbine engine, the path followed by the primary flow downstream from the primary nozzle (6). The tail cone is characterised in that it comprises a connection to a system for supplying a pressurised gas and at least one perforation (8) for injecting the pressurised gas through the perforation and into the primary flow. The casing preferably comprises at least one means for rotating same about the axis of rotation of the mobile elements of the primary body.

Abstract: An angled electrical connector has a body having an engagement portion including a sleeve which extends in a longitudinal first direction for engaging with a mating electrical connector. The sleeve has a cylindrical inner portion at the base of the sleeve and a tapered portion, such that the opening of the sleeve is larger than the base. A corresponding receptacle part is also provided, having a projecting connection port, with a corresponding cylindrical portion at or near the end.

Abstract: An aircraft jet engine with a longitudinal axis, including a wall enclosing a gas flow ejected from a downstream end of the wall in the longitudinal axis, plural ducts being distributed around the periphery of the downstream end of the wall each including a terminal section, including an outlet opening. Each duct can eject a fluid jet through the outlet opening thereof. The ducts are configured to eject the fluid jets essentially parallel to each other, each fluid jet ejected through the corresponding outlet opening forming a lateral angle with the longitudinal axis in a projection view in a plane with the longitudinal axis.

Abstract: Embodiments of the present invention provide apparatuses and methods for identifying computer systems that pose a threat for potential dissemination of confidential information, and thereafter, scanning the computer systems for unauthorized activity related to potential dissemination of confidential information. Embodiments of the invention comprise compiling a list of user computer systems that are at risk of accessing, using, or disseminating confidential information; determining whether the computer systems on the list are available for scanning; and scanning the computer systems on the list to identify an incident related to potential or actual threats or breaches of confidential information.

Abstract: A first electrical connector (1) for terminating an electrical cable (11) and for engaging with a mating electrical connector (51). The first connector comprises a body (5) having an engagement portion including a sleeve (7) whose passage extends along a mating axis (101) for engaging the mating electrical connector. The connector comprises at least one resilient member (15), such as a coil spring, arranged on the sleeve. The resilient member is capable of deforming radial to the mating axis (101) to provide a reaction force for maintaining the engagement of the connector with the mating connector. The first connector can be detached by lifting a boot (13) to pry apart the connectors.

Abstract: Embodiments of the invention relate to risk assessments and, more particularly to performing access risk assessments based on identified outliers.

Abstract: An aircraft jet engine including a wall centered about a longitudinal axis and surrounding a stream of gas ejected at a downstream end of the wall in the direction of the axis, primary ducts distributed at the periphery of the downstream end of the wall configured on command each to eject a jet of primary fluid to interact with the ejected stream of gas, the primary ducts of each pair converging towards one another near the downstream end of the wall so that the primary jets ejected form two sides of a triangle that meet at the vertex thereof in a view projected onto a plane perpendicular to a transverse plane, and secondary ducts each associated with each pair of primary ducts and configured on command to eject a jet of secondary fluid directed into the triangle formed by the primary jets.

Abstract: A jet engine, including a wall surrounding a first gas flow ejected from a downstream end of the wall along a longitudinal axis, a second flow of gas running outside the wall in a direction of ejection of the first gas flow, at least one duct arranged on the periphery of the downstream end of the wall which is desired to eject a gas flow for interacting with one and/or the other gas flow, the at least one duct including a terminal section provided at the free end thereof with an outlet opening through which the fluid is ejected. The terminal section successively includes a first section of straight duct aligned along a median axis and a second duct section forming a bend relative to the straight section, the second portion having a free end provided with the outlet opening and sufficiently close to the median axis of the first section to give the terminal section a reduced restriction in a direction of formation of the bend.

Abstract: An aircraft engine having a longitudinal axis, including a wall surrounding a gas stream that is ejected at a downstream end of the wall along the longitudinal axis, wherein a plurality of conduits distributed at the periphery of the downstream end of the wall are each capable of ejecting, via an outlet orifice, a fluid jet in the form of a sheet, in such a way that the jets thus ejected each form a fluid perturbation around the ejected gas stream.

Abstract: Embodiments of the invention relate to risk assessments and, more particularly to performing access risk assessments based on identified outliers.

Abstract: Embodiments of the invention relate to risk review assessments and, more particularly to determining risk review candidates by identifying two or more community categories, determining risk scores for each user/employee across risk categories, normalizing the risk scores based on community averages and community standard deviations and determining risk review candidates by comparing the normalized risk scores to predetermined thresholds. In additional embodiments, an outlier reinforcement score for each user/employee by summing all of the positive-valued normalized risk scores across the two or more communities and comparing the outlier reinforcement score to a predetermined threshold.

Abstract: An electrical connector comprises a dielectric spacing element having elongate through holes and a forward end surface; a plurality of parallel, elongate conductive contacts arranged in respective through holes of the spacing element, the conductive contacts providing electrical connections; an outer body arranged about the spacing element and the conductive contacts, the outer body having a longitudinal position fixed relative to the dielectric spacing element and having a forward end for engagement with a mating connector; and a collar slidably mounted about the outer body. The collar has an engagement position in which a forward surface of the collar is positioned in front of the forward end of the outer body for mechanically coupling the connector with the mating connector and a retracted position in which the forward surface of the collar is positioned behind the forward end surface of the spacing element for cleaning access to the conductive contacts.

Abstract: A nozzle allowing the reduction of noise generated by aircraft jet engines having at least one output ring which disturbs the propulsion jet, and having at least one pair of conduits from which the propulsion of jet air is ejected at the output of the nozzle. The conduits of each pair are disposed convergent with respect to each other in order to generate a triangle of interaction of the air jets at the output ring.

Abstract: A first electrical connector (1) for terminating an electrical cable (11) and for engaging with a mating electrical connector (51). The first connector comprises a body (5) having an engagement portion including a sleeve (7) whose passage extends along a mating axis (101) for engaging the mating electrical connector. The connector comprises at least one resilient member (15), such as a coil spring, arranged on the sleeve. The resilient member is capable of deforming radial to the mating axis (101) to provide a reaction force for maintaining the engagement of the connector with the mating connector. The first connector can be detached by lifting a boot (13) to pry apart the connectors.

Abstract: A jet engine, including a wall surrounding a first gas flow ejected from a downstream end of the wall along a longitudinal axis, a second flow of gas running outside the wall in a direction of ejection of the first gas flow, at least one duct arranged on the periphery of the downstream end of the wall which is desired to eject a gas flow for interacting with one and/or the other gas flow, the at least one duct including a terminal section provided at the free end thereof with an outlet opening through which the fluid is ejected. The terminal section successively includes a first section of straight duct aligned along a median axis and a second duct section forming a bend relative to the straight section, the second portion having a free end provided with the outlet opening and sufficiently close to the median axis of the first section to give the terminal section a reduced restriction in a direction of formation of the bend.

Abstract: An aircraft jet engine including a wall centered about a longitudinal axis and surrounding a stream of gas ejected at a downstream end of the wall in the direction of the axis, primary ducts distributed at the periphery of the downstream end of the wall configured on command each to eject a jet of primary fluid to interact with the ejected stream of gas, the primary ducts of each pair converging towards one another near the downstream end of the wall so that the primary jets ejected form two sides of a triangle that meet at the vertex thereof in a view projected onto a plane perpendicular to a transverse plane, and secondary ducts each associated with each pair of primary ducts and configured on command to eject a jet of secondary fluid directed into the triangle formed by the primary jets.

Abstract: An aircraft jet engine with a longitudinal axis, including a wall enclosing a gas flow ejected from a downstream end of the wall in the longitudinal axis, plural ducts being distributed around the periphery of the downstream end of the wall each including a terminal section, including an outlet opening. Each duct can eject a fluid jet through the outlet opening thereof. The ducts are configured to eject the fluid jets essentially parallel to each other, each fluid jet ejected through the corresponding outlet opening forming a lateral angle with the longitudinal axis in a projection view in a plane with the longitudinal axis.

Abstract: An electrical connector comprises a dielectric spacing element having elongate through holes and a forward end surface; a plurality of parallel, elongate conductive contacts arranged in respective through holes of the spacing element, the conductive contacts providing electrical connections; an outer body arranged about the spacing element and the conductive contacts, the outer body having a longitudinal position fixed relative to the dielectric spacing element and having a forward end for engagement with a mating connector; and a collar slidably mounted about the outer body. The collar has an engagement position in which a forward surface of the collar is positioned in front of the forward end of the outer body for mechanically coupling the connector with the mating connector and a retracted position in which the forward surface of the collar is positioned behind the forward end surface of the spacing element for cleaning access to the conductive contacts.