Abstract: The invention relates to a circuit (100) able to achieve simultaneous impedance matching between a generator (G) and a load (CH) for a power supply signal comprising at least two distinct frequencies.

Abstract: In one embodiment, the present invention includes an apparatus to heat a body. A first conductive path and/or a second conductive path include a resistive heating element that produces heat from said current. The first conductive path is coupled to redirect the current to the second conductive path and set up complementapy magnetic fields between said first and second layers. A third layer substantially blocks an electric field produced from the resistive heating element included in the first layer and/or second layer.

Abstract: A core structure (10) includes a first core element (16) including a leading edge section (30), a tip section (32), and a turn section (34) joining the leading edge and tip sections (30, 32). The first core element (16) is adapted to be used to form a leading edge cooling circuit (102) in a gas turbine engine airfoil (100). The leading edge cooling circuit (102) includes a cooling fluid passage (104) having a leading edge portion (106) formed by the first core element leading edge section (30), a tip portion (108) formed by the first core element tip section (32), and a turn portion (110) formed by the first core element turn section (34). Each of the leading edge portion (106), the tip portion (108), and the turn portion (110) of the cooling fluid passage (104) are formed concurrently in the airfoil (100) by the first core element (16).

Abstract: An apparatus for patterned processing includes a source of input gas, a source of energy suitable for generating a plasma from the input gas in a plasma region and a grounded sample holder configured for receiving a solid sample. The apparatus includes a mask arranged between the plasma region and the grounded sample holder, the mask having a first face oriented toward the plasma region and a second face oriented toward a surface of the solid sample to be processed, the mask including a mask opening extending from the first face to the second face, and an electrical power supply adapted for applying a direct-current bias voltage to the mask, and the mask opening being dimensioned and shaped so as to generate spatially selective patterned processing on the surface of the solid sample.

Abstract: In one embodiment, the present invention includes an apparatus to heat a body. The apparatus includes a first and second heating element. The first heating element has a first conductive path and is coupled to pass a current. The second heating element has a second conductive path that runs adjacent to the first conductive path. The second heating element terminates an electric field produced within the first heating element. The first conductive path is coupled to redirect the current to the second conductive path and set up complimentary magnetic fields between the first and second heating elements.

Abstract: Disclosed is a yoke-less mover of a homopolar linear synchronous machine. The yoke-less mover may include a cold plate having slots. Ferromagnetic cores are fixed to the cold plate. Each of the ferromagnetic cores may protrude through a respective one of the slots, creating gaps between the ferromagnetic cores. Armature windings are fixed to the cold plate. The armature windings may occupy the gaps between the ferromagnetic cores. The ferromagnetic cores of the yoke-less mover have better ferromagnetic utilization and lower weight. It also enables more flexible topologies in the armature windings.

Abstract: A moving member of a machine can include a cold plate that serves as a primary structural member for the moving member. The cold plate can have one or more cooling channels formed within the cold plate. A plurality of armature windings can be fixed to the cold plate. One or more field windings can be fixed to the cold plate. A plurality of ferromagnetic cores can be fixed to the cold plate, each ferromagnetic core positioned within a loop of at least one of the plurality of armature windings. Other embodiments are described.

Abstract: The invention relates to a circuit (100) able to achieve simultaneous impedance matching between a generator (G) and a load (CH) for a power supply signal comprising at least two distinct frequencies.

Abstract: A method for generating an ion flow asymmetry in a capacitively coupled radiofrequency plasma reactor comprising a step for energization of a first electrode by a radiofrequency voltage waveform. The standardized voltage waveform is an approximate waveform with a degree of approximation of a standardized sawtooth radiofrequency function having different rising and falling slopes. The degree of approximation of the approximate waveform and the pressure P of the gas are sufficiently high for causing the appearance of an asymmetry of the ion flows between the ion flow at the first electrode and the ion flow at a second electrode.

Abstract: Supervision and testing of a carbon monoxide (CO) alarm using an application specific integrated circuit (ASIC) and microcontroller. Wherein an electrochemical CO sensor is isolated from its detection circuit and a voltage charge is changed thereon then the CO sensor is reconnected to the detection circuit, wherein the voltage charge on the CO sensor returns to an equilibrium state over time. From the voltage versus time results a determination is made as to whether the CO sensor and CO detection circuit are functioning properly. All test and control circuits may be provided by the ASIC.

Abstract: Supervision and testing of a carbon monoxide (CO) alarm using an application specific integrated circuit (ASIC) and microcontroller. Wherein an electrochemical CO sensor is isolated from its detection circuit and a voltage charge is changed thereon then the CO sensor is reconnected to the detection circuit, wherein the voltage charge on the CO sensor returns to an equilibrium state over time. From the voltage versus time results a determination is made as to whether the CO sensor and CO detection circuit are functioning properly. All test and control circuits may be provided by the ASIC.

Abstract: The present disclosure provides a turbine blade (12) comprising a leading edge cooling circuit (30), a trailing edge cooling circuit (34), a mid-section cooling circuit (32) comprising a first channel (32a), an intermediate channel (32b), and a final channel (32c), and an axial tip cooling circuit (56). The leading edge, mid-section, and trailing edge cooling circuits (30, 32, 34) each receive a cooling airflow (CF) from a cooling air supply. A radially outer portion of each of the leading edge and mid-section cooling circuits (30, 32) further comprises at least one outlet (62, 64) in fluid communication with the axial tip cooling circuit (56) such that substantially all of a leading edge cooling airflow (LEF) exiting the leading edge cooling circuit (30) and substantially all of a mid-section cooling airflow (MSF) exiting the mid-section cooling circuit (32) is directed to the axial tip cooling circuit (56).

Abstract: When presenting information to a user via a display, an animated timeline (18) is provided on which a user selects a tick mark (74, 92) representing a time on the timeline (18), to view data collected at that time. A time window (72) of a predetermined width (e.g., an hour) is centered on the selected tick mark (74, 92), and the timeline (18) is then animated as it shifts the selected tick mark (74, 92) to the center of the timeline (18). Data (e.g., images, measured parameters, etc.) corresponding to the time window is identified (e.g., via timestamp information) and presented to the user on a display along with the timeline (18).

Abstract: Disclosed is a plasma generating apparatus, for manufacturing devices having patterned layers, including a first electrode assembly and a second electrode assembly placed in a plasma reactor chamber, an electrical power supply for generating a voltage difference between the first electrode assembly and the second electrode assembly. The first electrode assembly includes a plurality of protrusions and a plurality of recesses, the protrusions and recesses being dimensioned and set at respective distances from the surface of the substrate so as to generate a plurality of spatially isolated plasma zones located selectively either between the second electrode assembly and the plurality of recesses or between the second electrode assembly and the plurality of protrusions.

Abstract: An airfoil (10) is disclosed for a gas turbine engine in which the airfoil (10) includes an internal cooling system (14) with one or more converging-diverging exit slots (20) configured to increase the effectiveness of the cooling system (14) at the trailing edge (34) of the airfoil (10) by increasing the contact of cooling fluids with internal surfaces (24, 30) of the pressure and suction sides (36, 38) of the airfoil (10). In at least one embodiment, the trailing edge cooling channel (18) may include one or more converging-diverging exit slots (20) to further pressurize the trailing edge cooling channel (18) and may be formed by a first and second ribs (80, 82) extending between an outer walls (13, 12) forming the pressure and suction sides (36, 38).

Abstract: Disclosed are systems and methods for generating and offering to customers rewards in exchange for the customer's continued presence in a retail environment. An example rewards system may receive, from a detection system, a notification that a computing device associated with the customer is in a retail environment and, in response, transmit an offer to the computing device that offers the customer a reward in exchange for remaining in the retail environment for at least a predetermined amount of time. The rewards system may receive, from the detection system, real-time data indicating a behavior of the customer in the retail environment, and, from a third-party server, non-real-time data associated with the customer. The rewards system may generate the reward based on the real-time data and the non-real-time data. After the predetermined amount of time, the rewards system may transmit the reward to the computing device.

Abstract: Feedthroughs for antenna or other cables are described. At least some versions of the feedthroughs may, but need not necessarily, be employed as part of passive armor systems for lightweight vehicles used by, for example, special operations forces of the United States military. The feedthroughs may provide non-linear cable paths in areas near openings of vehicle hulls and avoid creating direct pathways for bullets to enter the openings.

Abstract: Turbine and compressor casing/housing abradable component embodiments for turbine engines, have abradable surfaces with asymmetric forward and aft ridge surface area density. The forward ridges have greater surface area density than the aft ridges to compensate for greater ridge erosion in the forward zone during engine operation and reduce blade tip wear in the aft zone. Some abradable component embodiments increase forward zone ridge surface area density by incorporating wider ridges than those in the aft zone.

Abstract: An airfoil (10) is disclosed for a gas turbine engine in which the airfoil (10) includes an internal cooling system (14) with one or more converging-diverging exit slots (20) configured to increase the effectiveness of the cooling system (14) at the trailing edge (34) of the airfoil (10) by increasing the contact of cooling fluids with internal surfaces (24, 30) of the pressure and suction sides (36, 38) of the airfoil (10). In at least one embodiment, the trailing edge cooling channel (18) may include one or more converging-diverging exit slots (20) to further pressurize the trailing edge cooling channel (18) and may be formed by a first and second ribs (80, 82) extending between an outer walls (13, 12) forming the pressure and suction sides (36, 38).

Abstract: A cooling system (10) for a turbine airfoil (12) of a turbine engine having one or more mid-chord cooling channels (16) that extend through both the airfoil (32) and a platform (18) of the airfoil (12) to provide adequate cooling the platform (18) while cooling the airfoil (32) is disclosed. The mid-chord cooling channel (16) may be formed from an airfoil portion (20) extending generally spanwise within the airfoil (32) and a platform portion (22) extending into a platform (18) of the airfoil (12) with a larger cross-sectional area than a cross-sectional area of the airfoil portion (20). The mid-chord cooling channel (16) may also extend into the platform (18) of the airfoil (12) a distance laterally outside of a silhouette (60) of the airfoil (32) defined by the leading edge (24), trailing edge (26), pressure side (28) and suction side (30) of the airfoil (32). Thus, the mid-chord cooling channel (16) extends laterally into the platform (18) to provide adequate cooling the platform (18).