Abstract: An outer seal structure for a rotor assembly includes a stator structure and a non-contact seal assembly. The non-contact seal assembly is fixed relative to the stator structure and includes a plurality of seal shoes, a seal base, a plurality of spring elements, and a shoe support plate. The plurality of seal shoes are arranged about an axis in an annular array. The seal base circumscribes the annular array of the plurality of seal shoes. Each of the plurality of spring elements extend radially between a respective seal shoe of the plurality of seal shoes and the seal base. The shoe support plate is arranged about the axis and mounted to the stator structure and includes a plurality of shoe support tabs extending axially from the shoe support plate. Each shoe support tab of the plurality of shoe support tabs is disposed between each seal shoe.

Abstract: An antenna assembly for a radio frequency identification (RFID) reader includes: a support member having an inner surface and an opposing outer surface; a first bifilar helical antenna element wound about a first helical axis extending from the outer surface of the support member, wherein the first helical axis is exclusive to the first helical antenna element; a first control terminal on the support member, electrically connected with the first bifilar helical antenna element; a second bifilar helical antenna element wound about a second helical axis extending from the outer surface of the support member, wherein the second helical axis is exclusive to the second helical antenna element; and a second control terminal on the support member, electrically connected with the second bifilar helical antenna element.

Abstract: A static structure of a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, an outer platform, an inner platform, an airfoil that extends between the outer platform and the inner platform, a service tube disposed at least partially through the airfoil, and a seal assembly that seals between the service tube and one of the outer platform and the inner platform.

Abstract: A device for measuring tread depth includes: an image sensor; first and second depth sensing modules spaced apart along a separation axis, each including (i) an emitter configured to emit a beam of light, and (ii) an optical assembly configured to direct reflections of the beam of light onto a respective region of the image sensor; a controller connected to the image sensor and configured, responsive to the device traversing a treaded surface, to: receive, from the image sensor, a sequence of images corresponding to sequential positions of the device traversing the treaded surface in a travel direction substantially perpendicular to the separation axis, the sequence of images depicting successive reflections of the beams from the treaded surface; determine, for each image in the sequence of images, a first depth measurement and a second depth measurement; and store, in a memory, the first and second depth measurements.

Abstract: A blade outer air seal (BOAS) is provided. The BOAS comprising: a seal body having a forward side, an aft side opposite the forward side, a radially inward side, and a radially outward side opposite the radially inward side; and a relief gap within the seal body to allow a portion of the radially inward side to expand into the relief gap when the seal body is heated.

Abstract: A turbomachine airfoil element includes an airfoil that has pressure and suction sides spaced apart from one another in a thickness direction and joined to one another at leading and trailing edges. The airfoil extends in a radial direction a span that is in a range of 0.46-0.59 inch (11.8-14.9 mm). A chord length extends in a chordwise direction from the leading edge to the trailing edge at 50% span and is in a range of 0.73-0.86 inch (18.6-21.9 mm). The airfoil element includes at least two of a first mode with a frequency of 5133±15% Hz, a second mode with a frequency of 8542±15% Hz, a third mode with a frequency of 15487±15% Hz, a fourth mode with a frequency of 18774±15% Hz, a fifth mode with a frequency of 24295±15% Hz and a sixth mode with a frequency of 27084±15% Hz.

Abstract: In some embodiments, an upstream facing port device (UFP device) is connected to a DisplayPort source device via a connection that complies with the DisplayPort specifications. A downstream facing port device (DFP device) is connected to a DisplayPort sink device via a connection that complies with the DisplayPort specifications. The UFP device and the DFP device are connected via an extension medium to allow the DisplayPort source device to provide video and/or audio for presentation by the DisplayPort sink device. In some embodiments, the UFP device and/or the DFP device may be configured to provide video extracted from the DisplayPort communication to an external video processing device for processing before and/or after transmission over the extension medium.

Abstract: Disclosed is an apparatus and method for inspecting a component of a gas turbine engine, which includes a sleeve configured to surround a component of a gas turbine engine, the sleeve including: a pair of opposing wall members being secured to each other at at least one of a pair of opposite ends; an internal cavity located between the pair of opposing wall members, wherein the internal cavity extends from one end of the sleeve to an opposite end of the sleeve; and a plurality of orifices extending through the pair of opposing wall members, and wherein a probe is inserted in each orifice in one of the pair of opposing wall members to determine the state of the internal cavities of a gas turbine component and determine the structural integrity of the component.

Abstract: A wireless power transfer system includes: a transmitting side, which includes a resonant transmitting circuit, the resonant transmitting circuit including a transmitter coil; and a receiving side, which includes a resonant receiving circuit, the resonant receiving circuit including a receiver coil for performing induction with the transmitter coil to generate a resonant receiver voltage, wherein the transmitter adjusts a transmitter current of the resonant transmitting circuit according to the resonant receiver voltage such that the resonant receiver voltage is regulated to a target voltage level. The wireless power transfer system determines a shift distance from a present relative position to an optimal relative position according to the adjusted transmitter current of the resonant transmitting circuit.

Abstract: An active clearance control system for a gas turbine engine includes an annular piston with a multiple of piston lift lugs. A method of active blade tip clearance control for a gas turbine engine includes translating axial movement of an annular piston to radial movement of a multiple of blade outer air seal segments.

Abstract: A network device supporting TRILL protocol includes a memory, a processor, and a communication interface. The memory includes a lookup table stored therein. The processor is coupled to the memory. The communication interface is coupled to the processor. The communication interface includes a trunk port and an access port and is configured to receive a first packet. When the processor determines that an output port corresponding to a destination address of the first packet is the trunk port, and determines that there is a lack of nickname information corresponding to the destination address according to the look up table, a second packet is transmitted through the trunk port of the communication interface. The second packet includes an enable local bit. The second packet and the first packet include the same payload information.

Abstract: Three-dimensional (3D) depth imaging systems and methods are disclosed for assessing an orientation with respect to a container. A 3D-depth camera captures 3D image data of a shipping container. A container feature assessment application determines a representative container point cloud and (a) converts the 3D image data into 2D depth image data; (b) compares the 2D depth image data to one or more template image data; (c) performs segmentation to extract 3D point cloud features; (d) determines exterior features of the shipping container and assesses the exterior features using an exterior features metric; (e) determines interior features of the shipping container and assesses the interior features using an interior features metric; and (f) generates an orientation adjustment instruction for indicating to an operator to orient the 3D-depth camera in a second direction for use during a shipping container loading session, wherein the second direction is different than the first direction.

Abstract: A sub-word line driver circuit includes a substrate, a plurality of gate lines, at least one gate tab, and a variable-thickness gate dielectric. The substrate includes an isolation area and an active area. The gate lines are arranged in a first direction and extend in a second direction perpendicular to the first direction. The gate tab extends in the first direction to cover the isolation area, in which the gate lines and the gate tab form at least one gate region on the substrate. The variable-thickness gate dielectric includes a thick gate dielectric region disposed over a first portion of the active area, and a thin gate dielectric region disposed over a second portion of the active area.

Abstract: A vane according to an exemplary aspect of the present disclosure includes, among other things, a platform extending from an edge face and between spaced apart lateral faces and an airfoil extending outwardly from the platform. The platform includes at least one ejection port in the edge face and at least one passage connected to the at least one ejection port. A method of cooling a component is also disclosed.

Abstract: An electronic device is provided. The electronic device includes a substrate, at least one contact pad disposed on the substrate, and a redistribution layer including a strip-shaped portion. The redistribution layer is electrically connected to the contact pad. The strip-shaped portion includes at least two strip-shaped steps, and each of the strip-shaped steps includes a plurality of peaks and valleys.

Abstract: A fuel injection system may comprise a mixer and a fuel injector disposed within the mixer. The mixer may comprise an outer housing with an exit port and a bluff body extending across the exit port of the outer housing. A flared surface of the mixer may match a contour of the bluff body.

Abstract: The present disclosure provides a semiconductor structure including a substrate, a bottom gate portion disposed in the substrate, a top gate portion stacked over the bottom gate portion, a first channel layer sandwiched between the top gate portion and the bottom gate portion, and a source/drain region disposed in the substrate at two opposite sides of the top gate portion.

Abstract: A method can include receiving values of an inversion based at least in part on seismic amplitude variation with azimuth (AVAz) data for a region of a geologic environment; based at least in part on the received values, computing values that depend on components of a second-rank tensor aij; selecting a fracture height for fractures in the geologic environment; selecting an azimuth for a first fracture set of the fractures; based at least in part on the values for the second-rank tensor aij, the fracture height and the selected azimuth, determining an azimuth for a second fracture set of the fractures; and generating a discrete fracture network (DFN) for at least a portion of the region of the geologic environment where the discrete fracture network (DFN) includes fractures of the first fracture set and fractures of the second fracture set.

Abstract: An airfoil according to an example includes, among other things, a suction sidewall and a pressure sidewall. A tip wall extends from a leading edge to a trailing edge and joins respective outer ends of the suction and pressure sidewalls. A tip rib extends along a pressure side of the tip wall. A tip leakage control channel is provided at the tip wall and has a floor that extends between a first control channel vane sidewall and a second control channel vane sidewall established by a corresponding tip leakage control vane. Each of the tip leakage control vanes is contiguous with and extending from a suction side surface of the tip rib. The tip leakage channel extends toward the trailing edge while extending toward the suction sidewall. One or more of an internal cavity, a channel cooling aperture, and a sidewall microcircuit may be provided.

Abstract: A turbine section according to an example of the present disclosure includes, among other things, a component including a coating on a substrate, and at least one sensor positioned a distance from the component, the at least one sensor configured to detect radiation emitted from at least one localized region of the coating at a first wavelength and configured to detect radiation emitted from the substrate corresponding to the at least one localized region at a second, different wavelength. The first wavelength and the second wavelength are utilized to determine a heat flux relating to the at least one localized region. A method of measuring a gas turbine engine component is also disclosed.