Abstract: A gas-turbine axial compressor has a casing 3 and a rotatable shaft 6, which form an annular duct, in which at least one stator 2 and one rotor 4 are arranged. A shroud 21 is arranged at a free end of the stator 2 vanes, which extends over part of the axial length of the stator 2. A rotor platform 23 of at least one rotor 4 extends axially beneath a further part of the axial length of the stator 2, at which no shroud 21 is arranged.

Abstract: Integrated circuits having place-efficient capacitors and methods for fabricating the same are provided. A dielectric layer is formed overlying a conductive feature on a semiconductor substrate. A via opening is formed into the dielectric layer to expose a portion of the conductive feature. A partial opening is etched into the dielectric layer and positioned over the conductive feature. Etch resistant particles are deposited overlying the dielectric layer and in the partial opening. The dielectric layer is further etched using the etch resistant particles as an etch mask to extend the partial opening. A first conductive layer is formed overlying the extended partial opening and electrically contacting the conductive feature. A capacitor insulating layer is formed overlying the first conductive layer. A second conductive layer is formed overlying the insulating layer.

Abstract: A turbine reduces variations in mass flow at throats even when the flow rate of fluid is low or high. The turbine includes a turbine rotor having turbine blades; a turbine housing accommodating the turbine rotor 80 and whose cross-sectional area of a scroll portion formed between the turbine housing and the turbine rotor gradually decreases; a plurality of fixed vanes fixed along a curved line dividing the scroll portion into an inner scroll part and an outer scroll part; throats formed between the adjacent fixed vanes and communicate between the inner scroll part and the outer scroll part; and a switch valve which switches a flow path in the turbine housing either to the inner scroll part or to both the inner scroll part and the outer scroll part, in which flow path areas of the throats are reduced in a downstream direction of the scroll portion.

Abstract: A turbomachine including a variable-pitch stator vane stage is disclosed. A control ring that is coaxial around the casing includes two segments that are assembled together by side connection straps fastened on either side of the segments with mutual insetting and in the vicinity of the ends of the segments.

Abstract: The present invention relates to a fresh gas system (1) for supplying an internal combustion engine (4) with fresh gas, in particular in a motor vehicle, having a charging device (8) for increasing the pressure of the fresh gas and having a swirl generator (12), which is arranged upstream of the charging device (8), for generating a swirl, which rotates about the main flow direction of the fresh gas, in the fresh gas, wherein the swirl generator (12) has guide blades (14) with adjustable angle of incidence. In order to be able to produce the fresh gas system (4) more cost-effectively, the swirl generator (12) has a flow guide body (13) on which the guide blades (14) are integrally formed and which, in order to adjust the angle of incidence of the guide blades (14), can be twisted with elastic deformation about the main flow direction starting from an undeformed initial position.

Abstract: A variable vane arm has a hook portion comprising a radially inner leg connected to a radially outer leg by an arcuate connection, and an actuation lever extending from the hook portion. The hook portion and actuation lever are formed from a singular piece of material.

Abstract: A stator stage of a compressor of a turbomachine including an annular row of variable-pitch vanes is disclosed. Each vane includes an external cylindrical pivot defining the axis of rotation of the vane, and an internal cylindrical pivot mounted in a housing of an internal ring. The internal pivot of each vane extends along an axis substantially parallel to the axis of rotation of the vane and at a distance from this axis, and is mounted in the housing of the ring by a swiveling or a tilting system.

Abstract: A leadframe design for a diode or other semiconductor device that reduces stress on the device and provides increased heat dissipation is provided. According to various embodiments, the leadframe has a contoured profile including a recessed area and a raised surface within the recessed area. The surface supports the device such that the edges of the device extend past the surface. Also provided are device assemblies including the novel leadframes. In certain embodiments, the assemblies include one or more leadframes attached via a solder joint to a device. According to various embodiments, the leadframes are attached to the front side of the device, back side of the device or both. In particular embodiments, the device is a bypass diode for one or more solar cells in a solar module.

Abstract: A lever for rotating about its pivot a turbomachine variable-pitch stator vane: including a first zone for attachment to a lever drive member, a second zone for attachment to the variable-pitch stator vane, and a third zone of elongate shape between the first zone and the second zone is disclosed. A vibration-damping laminate is applied to at least one surface portion of at least one of the zones of the lever. The laminate includes at least one layer of viscoelastic material in contact with the surface portion and a backing layer of rigid material.

Abstract: A fabricating method includes adhering an exposed surface of a first solid adhesive film to a first substrate. The second surface of the first solid adhesive film is exposed and adhered to a second substrate. A third substrate is adhered to a second substrate via a patterned second solid adhesive film, and a diaphragm layer is adhered to the third substrate via a patterned third solid adhesive film. A fourth solid adhesive film with a removable release film is adhered to the first substrate covered, followed by slicing to form wafer level lens modules.

Abstract: A semiconductor circuit includes: a first diffusion layer formed on a substrate; a second diffusion layer formed in an upper part of the first diffusion layer; a third diffusion layer formed in an upper part of the second diffusion layer; a fourth diffusion layer formed in the upper part of the first diffusion layer; and a fifth diffusion formed below the third diffusion layer. A sum of a shortest distance from the third diffusion layer to the fifth diffusion layer and a shortest distance from the fifth diffusion layer or the lower end of the first diffusion layer to the fourth diffusion layer is smaller than a shortest distance from the third diffusion layer to the fourth diffusion layer. The substrate, the second and the fifth diffusion layer are a first conductivity type and the others are a second conductivity type.

Abstract: A turbocharger (1) with a variable turbine geometry (VTG), includes a guide baffle (18), which has a blade bearing ring (6) with a plurality of guide blades (7), each of the latter having a blade shaft (8) that is mounted on the blade bearing ring (6). The guide baffle also has an adjusting ring (5), which interacts with the guide blades (7) by means of associated blade levers (20), which are fixed to the blade shafts (8) by one of their ends (21). The other end (22) of each blade lever (20) is provided with a lever head (23), which can be engaged in an associated engagement recess (24) of the adjusting ring (5). Each blade lever (20) is asymmetrical and has a bearing lug (25) in the form of an arched segment on only one side of the central section (26).

Abstract: A flip-chip packaging assembly and integrated circuit device are disclosed. An exemplary flip-chip packaging assembly includes a first substrate; a second substrate; and joint structures disposed between the first substrate and the second substrate. Each joint structure comprises an interconnect post between the first substrate and the second substrate and a joint solder between the interconnect post and the second substrate, wherein the interconnect post exhibits a width and a first height. A pitch defines a distance between each joint structure. The first height is less than half the pitch.

Abstract: A compressor nozzle device comprises a set of adjustable vanes which is interposed between two opposite wall members (3, 5), and a unison ring (7) for actuating said vanes (1). The unison ring (7) is arranged at a side of one of said wall members (3) opposite to the other side thereof facing the vanes (1).

Abstract: A control device of variable pitch vanes in a turbomachine is disclosed. The control device includes a ring surrounding a casing of the turbomachine and connected by links to the variable pitch vanes, and a jack connected to the ring in order to displace it in rotation around the casing. The jack is mounted pivoting on the casing and its piston rod is connected to the ring by a connecting rod. The piston and connecting rods are articulated on an axis which is connected to the casing by a guiding device maintaining it at a substantially constant distance from the casing.

Abstract: A semiconductor device includes a wiring substrate having a mounting surface on which a semiconductor element is mounted. A portion of the mounting surface exposed from the semiconductor element is covered by a solder-resist layer, and an extension portion of the solder-resist layer extends from a dropping-commencing point of a liquid-state under-filling agent on the portion of the mounting surface exposed from the semiconductor element and into an area of the wiring substrate covered by the semiconductor element. A gap between the semiconductor element and the extension portion of the solder-resist layer is formed to be narrower than the gap between the semiconductor element and the mounting surface of the wiring substrate so that liquid drops of the under-filling agent dropped at the dropping-commencing point are sucked into the gap by a capillary phenomenon.

Abstract: A stage of variable-pitch vanes for a turbomachine is disclosed. The vanes include internal pivots engaged in corresponding housings of a sectorized internal ring. Each ring sector includes axial orifices for mounting two pins for the radial retention of the ring sector on the internal pivot of a vane. Each pin includes an immobilization device cooperating by shape coupling with a complementary immobilization device of the other pin in order to rotationally immobilize these pins in the orifices in the ring sectors.

Abstract: A variable stator vane airfoil is mounted on a button centered about a rotational axis and includes circular leading and trailing edges circumscribed about the rotational axis at a button radius. Contoured pressure and suction sides extend from the circular leading edge to the circular trailing edge and are recessed inwardly from a perimeter circumscribed about the rotational axis at the button radius. One of upstream and downstream pressure side portions of the contoured pressure side is straight and another of the upstream and downstream pressure side portions is convexly curved. One of the upstream and downstream suction side portions is straight and another of the upstream and downstream suction side portions is convexly curved. One of the upstream pressure side portion and upstream suction side portion is straight and another of the upstream pressure side portion and upstream suction side portion is convexly curved.