Abstract: A comminuting device for comminuting material. The device has a frame and a shear member having a main blade, the shear member movably coupled to the frame with a shear member slide bearing located at least partially inside the frame. A supporting table is coupled to the frame, the supporting table having a counter blade, the supporting table adapted to support the scrap material. The frame has an opening forming an access way to the shear member slide bearing. The main blade and the counter blade cooperate to chop the scrap material when the shear member is moved from a first position to a second position. The shear member slide bearing is removable from inside the frame through the opening without removal of the shear member from the frame.

Abstract: Modular wafer transport and handling facilities are combined in a variety of ways deliver greater levels of flexibility, utility, efficiency, and functionality in a vacuum semiconductor processing system. Various processing and other modules may be interconnected with tunnel-and-cart transportation systems to extend the distance and versatility of the vacuum environment. Other improvements such as bypass thermal adjusters, buffering aligners, batch processing, multifunction modules, low particle vents, cluster processing cells, and the like are incorporated to expand functionality and improve processing efficiency.

Abstract: A propulsive system for an aircraft including an auxiliary jet engine is integrated within a tail cone of a fuselage. Lateral air intakes include each one a scoop movable between a closed position and an opened position are associated with aerodynamic channels to supply with air the auxiliary jet engine. The aerodynamic channels meet at a common channel including a movable flap to balance air flows coming from the air intakes when the operation is not symmetrical.

Abstract: A measurement instrument having a processor, a first sensor and a second sensor. The processor is adapted to output a measurement signal embodying a measurement of a physical quantity. The first sensor and second sensor are connected to the processor and are operable to generate respectively first and second measurements of the physical quantity. The processor defines a first measurement range within which the measurement signal is dependent on the first measurement and not the second measurement. The processor defines a second measurement range within which the measurement signal is dependent on the second measurement and not the first measurement. The first and second ranges meet at a predetermined transition. The first and second measurements are different at the transition and the measurement embodied in the measurement signal crosses the transition without an abrupt change.

Abstract: A securing mast for securing an engine to the wing of an aircraft, wherein the device includes two fasteners, a first end of each fastener being secured to the engine and the second end of each fastener being secured to the wing, wherein the fasteners include hinged junction means capable of modifying the geometry of the aforementioned fasteners in order to modify a distance between the engine and the wing.

Abstract: A wing arrangement of an aircraft has a wing and at least one pylon for suspending an engine below the wing. The wing has a leading edge with a high-lift device, which is able to move between a deployed position in which the high-lift device projects forward of the leading edge, and which is interrupted in a forward intermediate region of the wing located at the leading edge, the pylon having a forward edge extending forward of the leading edge of the wing between a forward upper portion connected to the wing in the forward intermediate region and a forward lower portion connected to a nacelle of the engine. An element of narrow elongate shape protrudes longitudinally from the forward edge and, during flight at a high angle of attack of the aircraft, generates a vortex of aerodynamic flow that is propagated toward the forward intermediate region above the wing.

Abstract: A substrate processing apparatus has a frame and a load port connected to the frame and adapted to mate a substrate transport container to the frame. The apparatus has transportable storage that is adapted to be removably connected to the frame and fit beneath the load port. The storage may be an enclosure housing electrical, mechanical, or electromechanical devices of the substrate processing apparatus.

Abstract: A method and apparatus for performing handover of a terminal in a wireless communication system, the method including obtaining information on neighboring networks from a media independent handover (MIH) server by using a MIH layer if a state of a link connected to a serving network is changed; transmitting a handover initiation request message to the MIH layer of the serving network through the MIH layer; checking handover support information and tunnel state information of the neighboring networks which are received from the MIH layer of the serving network; determining a target network to which handover is performed and performing layer-2 (L2) handover with the target network, by using the handover support information; and performing layer-3 (L3) handover with the target network by using the tunnel state information.

Abstract: A method for optimizing the mass of a composite panel composed of a plurality of uniform thickness zones, each zone defined by a vertical arrangement of plies, each arrangement having a different number of piles, and different orientation angles, where a positioning order of the plies has a given orientation angle with respect to the others in the vertical arrangement, and the proportion of plies has a given orientation angle with respect to all the plies composing the vertical arrangement. The optimization includes defining a lay-up table, and defining a vertical arrangement of plies for each uniform thickness zone, and starting from the lay-up table, building a function describing the physical properties of each zone as a function of the total thickness of each zone, where the total thickness for each zone is adjusted using a discrete variables iteration process, until the mass of the panel is a minimum.

Abstract: An aircraft center section includes a center part of an aircraft fuselage, a wing section, a center wing box installed at least partly in the fuselage and providing a junction between the wing section and the fuselage, and a ventral fairing partly enveloping the fuselage and the wing section, with the ventral fairing being attached directly to the wing section and to the fuselage by means of structural elements that can make the ventral fairing a working fairing.

Abstract: The invention relates to a method for arranging transaction control in a device management system. A required transaction control operation is defined in a managing device for arranging transaction control of a management task for a managed device. At least one device management command is defined for the transaction control operation. The at least one device management command is transmitted to the managed device. A required transaction control operation is specified in the managed device on the basis of one or more received device management commands, and transaction control for a management task is carried out on the basis of the defined transaction control operation.

Abstract: A system or method is disclosed which employs filters on a satellite whose bandwidth is varied by ground command to restrict interference experienced by a satellite as an auxiliary terrestrial component (ATC) system is increased to a multiplicity of cities and markets. Thus there is provided a novel method and system which optimizes overall MSS and ATC traffic.

Abstract: The presence of a workpiece on an end effector of a vacuum robotic handler is detecting using any of a number of non-contact techniques in which some or all of the detection hardware is positioned outside a vacuum chamber that encloses the vacuum robotic handler. Various deployments include laser beam breaking, analysis of radar reflection signals, or analysis of radio frequency identification tag signatures. By providing non-physical couplings between hardware inside and outside of a vacuum environment, integrity of the vacuum is improved. These non-contact techniques are further adapted as described herein to multi-wafer and multi-end effector environments so that independent detection of multiple wafers (e.g., for each end effector) can be performed.

Abstract: A device for non-destructive testing of a component by analyzing radiation dissipation when the component is stressed by mechanical stresses. The device includes measuring means for determining a surface radiation field of the component. The measuring means are integrated in a flexible housing for covering a region of the surface of the component to be tested. The device enables an initial crack upon stress concentration on a surface of the component and the presence of a crack upon propagation of the crack to be detected. The disclosed embodiments are useful for non-destructive testing of aircraft components, but may be used in all industrial sectors where testing the integrity of components is important, such as the automotive, railway, marine and nuclear industries.

Abstract: In order to protect an integrated circuit provided with a cryptoprocessor from attacks aiming to reveal secrets, it is anticipated to use a component sensitive to the activation of a parasitic (latchup) thyristor and/or to the activation of a parasitic bipolar transistor, or to design a circuit having this property. If the component is stressed due to the presence of this circuit, it is immediately deactivated, actually preventing the revelation of the secrets thereof.

Abstract: A fastening system for fastening a cabin fitting element with at least one electrical installation on a support structure of an aircraft. During installation into the support structure, the cabin fitting element is fixed in succession by at least one loose bearing in at least one degree of translational freedom and then by at least one fixed bearing in the at least one further degree of translational freedom. In order to ensure an improved installation and dismantling of cabin covering panels with electrical installation and to reduce the weight due to the components and also the installation space which is required, according to the disclosed embodiments a contact device with a bush arrangement and a plug arrangement is integrated in the at least one loose bearing and/or the at least one fixed bearing, by which an electrical connection is produced between the support structure and the electrical installation of the cabin fitting element on fixing at least of one degree of translational freedom.

Abstract: A system for opening and closing the flap of a casing for the landing gear of an aircraft includes a mechanical connection between the landing gear and the flap. The connection includes a first connecting rod which is fixed to the landing gear, and a second connecting rod which is fixed to the flap, the first and second connecting rods being connected by an articulation mechanism.

Abstract: A substrate transport apparatus comprising a drive mechanism, a movable arm assembly, and an end effector with an active edge gripper. The apparatus is configured to avoid the need to provide cables to the end effector for power or communication. In one aspect, the gripper is actuated when a motion sensor senses motion of the end effector. In another aspect, communication signals are wirelessly transferred to the end effector to control the active gripper. In another aspect, power is wirelessly transferred to the end effector to power actuation of the gripper.

Abstract: The disclosed embodiments relates to a jet engine for an aircraft, characterized in that it bears at least one stabilizer, the stabilizer being fastened on the rigid structure of said jet engine so as to form a one-piece assembly. The jet engine can also bear one or more auxiliary devices required for the operation of the jet engine. The disclosed embodiments also relates to an aircraft provided with such a jet engine, and to a method of mounting such a jet engine on an aircraft.

Abstract: A method of fluid sealing a workpiece is provided. The method includes providing a force to cause a ring to form a barrier to fluid entry with the workpiece and preventing fluid from crossing the barrier to fluid entry by forming a pressure differential across the barrier.