A gas turbine engine includes a heat exchanger, a bearing compartment, and a nozzle assembly in fluid communication with the bearing compartment. The heat exchanger exchanges heat with a bleed airflow to provide a conditioned airflow. The bearing compartment is in fluid communication with the heat exchanger. A first passageway communicates the conditioned airflow from the heat exchanger to the bearing compartment. A second passageway communicates the conditioned airflow from the bearing compartment to the nozzle assembly.

A gas turbine engine includes a geared architecture with a multiple of intermediate gears, and a baffle with an oil scavenge scoop adjacent to each of the multiple of intermediate gears. A geared architecture and method are also disclosed.

Footwear with a powerful arch spring made with spring boards that can be utilized by the heel and ball of the foot areas during impact for efficient energy storage and return during walking, running and other forms of self-propelled locomotion. The spring boards can extend into the toe area of the footwear to create a toe spring with efficient energy storage and return. Embodiments of the present invention combine the spring boards which are excellent for storing and returning energy with a shock absorbing material which can also function as a secondary spring in order to achieve high efficiency energy returns while maintaining comfort and stability with the footwear.

Operation of an arbiter in a hardware design is verified. The arbiter receives a plurality of requests over a plurality of clock cycles, including a monitored request and outputs the requests in priority order. The requests received by and output from the arbiter in each clock cycle are identified. The priority of the watched request relative to other pending requests in the arbiter is then tracked using a counter that is updated based on the requests input to and output from the arbiter in each clock cycle and a mask identifying the relative priority of requests received by the arbiter in the same clock cycle. The operation of the arbiter is verified using an assertion which establishes a relationship between the counter and the clock cycle in which the watched request is output from the arbiter.

Arbitration circuitry is provided for arbitrating between requests awaiting servicing. The requests require variable numbers of resources and the arbitration circuitry permits the request to be serviced in a different order to the order in which they were received. Checking circuitry prevents a given request other than a oldest request from being serviced when a number of available resources is less than a threshold number of resources. The threshold number is varied based on the number of resources required for at least one other request awaiting servicing.

In a system where multiple controllers share a link interface but are not all (1) compatible with the same configuration of the physical layer or (2) using the same clocking, a configuration arbitration subsystem intercepts, organizes, and re-clocks configuration-access requests from the various controller agents. Priorities are assigned according to stored policies. The configuration arbiter grants configuration access to the top-priority agent, synchronizing the agent's message with the arbiter's clock. Lower-priority agents' messages are stored in command queues until they ascend to top priority. Besides preventing timing conflicts and streamlining the coordination of clocks, the configuration arbiter may provide access to physical-layer registers beyond the controllers' built-in capabilities to further optimize configuration.

The present invention relates to a fine grained WC-Co cemented carbide. By adding an extremely small amount of Ti, V, Zr, Ta or Nb alone or in combinations, a grain refined cemented carbide structure with less abnormal WC-grains has been obtained.

A low alloy steel ingot contains from 0.15 to 0.30% of C, from 0.03 to 0.2% of Si, from 0.5 to 2.0% of Mn, from 0.1 to 1.3% of Ni, from 1.5 to 3.5% of Cr, from 0.1 to 1.0% of Mo, and more than 0.15 to 0.35% of V, and optionally Ni, with a balance being Fe and unavoidable impurities. Performing quality heat treatment including a quenching step and a tempering step to the low alloy steel ingot to obtain a material, which has a grain size number of from 3 to 7 and is free from pro-eutectoid ferrite in a metallographic structure thereof, and which has a tensile strength of from 760 to 860 MPa and a fracture appearance transition temperature of not higher than 40° C.

An outer blade cutting wheel comprising an annular thin disc base of cemented carbide and a blade section of metal or alloy-bonded abrasive grains on the outer periphery of the base is provided. The abrasive grains are diamond and/or cBN grains having an average grain size of 45-310 μm and a TI of at least 150. The blade section includes overlays having a thickness tolerance (T3max−T3min) of 0.001 mm to 0.1×T2 mm. The blade section has a roundness (ODmax/2−ODmin/2) of 0.001 mm to 0.01×ODmax mm.

The present disclosure is directed to a refractory metal core for use in forming varying thickness microcircuits in turbine engine components, a process for forming the refractory metal core, and a process for forming the turbine engine components. The refractory metal core is used in the casting of a turbine engine component. The core is formed by a sheet of refractory metal material having a curved trailing edge portion integrally formed with a leading edge portion.

The present invention relates to a shock absorbing hammer whose head has housings filled with pellet assembly inside. The pellet assembly includes both rigid pellets and soft pellets to absorb shock from external striking force impacted on the head of the main frame.

The present disclosure relates to compositions comprising at least one fluoroolefin and an effective amount of a stabilizer comprising at least one ascorbic acid, terephthalate, or nitromethane, or mixtures thereof. The stabilized compositions may be useful in cooling apparatus, such as refrigeration, air-conditioning, chillers and heat pumps, as well as in applications as foam blowing agents, solvents, aerosol propellants, fire extinguishants, and sterilants.

Embodiments of systems and methods for tuning a turbine are provided. In one embodiment, a method may include receiving at least one of a measured operating parameter or a modeled operating parameter of a turbine during operation; and tuning the turbine during operation. The turbine may be tuned during operation by applying the measured operating parameter or modeled operating parameter or parameters to at least one operational boundary model, applying the measured operating parameter or modeled operating parameter or parameters to at least one scheduling algorithm, comparing the output of the operational boundary model or models to the output of the scheduling algorithm or algorithms to determine at least one error term, and closing loop on the one error term or terms by adjusting at least one turbine control effector during operation of the turbine.

An apparatus for aligning a wind turbine generator is disclosed. Preferably, the apparatus includes at least, but is not limited to, a support flange engaging a securement stud via a securement aperture, and a force displacement plate contacting the support flange. The preferred apparatus further includes an indexing means attached to the securement stud and force displacement plate, the indexing means configured to translate a rotational force to linear force capable of moving the support flange in relation to the securement stud.

The invention relates to a polymer composition which absorbs infrared radiation (IR), containing a transparent thermoplastic plastic, an inorganic infrared absorber, also referred to as IR absorber hereinbelow, at least one inorganic nano-scale pigment, and the combination of at least two organic coloring agents of a specific structure, and to the preparation and use of the polymer compositions according to the invention and to products produced therefrom.

A system includes a SiC semiconductor power device; a power supply board that is configured to provide power to a first gate driver board via a connector; the first gate driver board that is coupled and configured to provide current to the SiC semiconductor power device, wherein the first gate driver board is coupled to the power supply board via the connector, and wherein the first gate driver board is separated from the power supply board; and an interconnect board that is coupled to the first gate driver board, wherein the interconnect board is configured to couple the first gate driver board a second gate driver board.

A ceiling mount intrusion detector with arbitrary direction detection capability is provided. The detector can include a pyroelectric sensor and a unitary Fresnel lens such that the unitary Fresnel lens includes a first piece of a first full Fresnel lens and a second piece of a second full Fresnel lens and such that the first piece and the second piece are spliced together. Due to the dimensions and location of the unitary Fresnel lens relative to the sensor, the sensor can output a signal indicative of an alarm condition when an object passes in front of the lens at any angle relative to the sensor.

Methods of designing zeolite materials for adsorption of CO2. Zeolite materials and processes for CO2 adsorption using zeolite materials.

A system is described, along with the related device and method, for transmission and/or reception of signals having electromagnetic modes with orbital angular momentum (OAM), wherein the device is adapted to receive, at its input, electromagnetic signals from at least one transmitter, and is configured to apply a discrete Fourier transform to the electromagnetic signals in order to generate the signals having electromagnetic modes with orbital angular momentum.

A wind turbine with a tower; a nacelle supported by said tower; at least one unit to be cooled and arranged in the tower or the nacelle; a tower mounted heat exchange structure arranged outside the nacelle and tower; and a circuit facilitating a flow of a fluid medium between the at least one unit and the heat exchange structure. To improve thermal convection with the ambient space, the heat exchange structure comprises a set of panels mutually angled and extending outwards from the tower such that a flow of ambient air can pass transversely trough the panels and thereby cool the unit.

An energy absorbing receiving glove constructed with a substrate having an exterior surface and a complementary interior surface. The substrate is used in constructing a palmar portion of the glove. The glove may incorporates a gripping layer of material affixed to the exterior surface of the substrate. Further, the glove may incorporate an energy absorbing layer of material affixed to the interior surface of the substrate. Additionally, the energy absorbing layer of material may have both a first thickness in a first location and a second thickness in a second location of the substrate. In an embodiment, the energy absorbing material is a silicone gel and the gripping material is a silicone material. Additionally, the varied thicknesses of the energy absorbing material may be effective for covering a palmar side of joints located on a hand wearing the glove.

The present subject matter is directed to a lattice tower covering and/or assembly for a wind turbine. The lattice tower assembly includes a plurality of structural members connected together to define an open lattice tower. The structural members include a plurality of supports, a plurality of inner cross-support members, and a plurality of outer cross-support members. The inner and outer cross-support members are connected between the supports so as to define one or more openings. The lattice tower covering includes one or more panel elements. Each of the panel elements are retained in position between the supports and cover at least a portion of one or more of the openings. Further, the lattice tower covering has a surface area defined by the plurality of supports and the one or more panel elements.

Embodiments of the disclosure relate to ultrasonic inspection of turbine components. In one embodiment, a method for ultrasonic inspection of a turbine component can include mounting at least one array of transducer elements to the turbine component, (a) separately pulsing a transducer element of the at least one array of transducer elements to transmit a signal to the turbine component, (b) capturing reflected signals from the turbine component at each transducer element in the at least one array of transducer elements, repeating (a) and (b) for each of the other transducer elements in the at least one array of transducer elements, maintaining a constant relative position of the array of transducer elements with respect to the turbine component, analyzing the captured reflected signals using a computer, generating an image of the interior volume of the turbine component by reconstruction of the captured reflected signals and based at least in part on detecting an anomaly in the image of the interior volume of the turbine component, identifying at least one defect or failure in the turbine component.

A gas turbine that includes: a combustor coupled to a turbine that define a working fluid flowpath; a compressor discharge cavity; a staged injection system that includes the forward injector and a staged injector; a stator blade positioned extending across the working fluid flowpath between an inboard sidewall and an outboard sidewall. A one-way continuous coolant flowpath that includes: an intake section that comprises an upstream port connected to the compressor discharge cavity and a downstream port formed through one of the inboard and outboard sidewalls; an outtake section that comprises a downstream port connected to the staged injector and an upstream port formed through the same one of the inboard and outboard sidewalls; and a cooling circuit extending through an interior of the airfoil of the stator blade and connecting to the downstream port of the intake section and the upstream port of the outtake section.

A component for a gas turbine engine including a gas path wall having a first surface and a second surface. A cooling hole extends through the gas path wall from an inlet in the first surface through a transition to an outlet in the second surface. Cusps are formed on the transition.

A system includes a gas turbine system having a turbine combustor, a turbine driven by combustion products from the turbine combustor, and an exhaust gas compressor driven by the turbine. The exhaust gas compressor is configured to compress and supply an exhaust gas to the turbine combustor. The gas turbine system also has an exhaust gas recirculation (EGR) system. The EGR system is configured to recirculate the exhaust gas along an exhaust recirculation path from the turbine to the exhaust gas compressor. The system further includes a main oxidant compression system having one or more oxidant compressors. The one or more oxidant compressors are separate from the exhaust gas compressor, and the one or more oxidant compressors are configured to supply all compressed oxidant utilized by the turbine combustor in generating the combustion products.

An assistance device for an aircraft free-turbine turbine engine, the device including first electrical power supply for powering a winding of a starter rotary machine, referred to as a “first” winding, in order to provide first assistance in accelerating the gas generator of the engine. The device further includes a monitor for monitoring the first assistance, and a second power supply for electrically powering a second winding of the rotary machine to provide second assistance in accelerating the gas generator if the monitor observes that the first assistance is insufficient.

A method for operating a stationary gas turbine at partial load, having at least one compressor, at least one expansion turbine and a combustion chamber provided with at least one burner, which gas turbine further includes a hydraulic gap adjuster, wherein the method has the following steps: operating the gas turbine at partial load; operating the a hydraulic gap adjuster; during the operation of the hydraulic gap adjuster, increasing the fuel supply to the burner while increasing the temperature of the combustion gases which are guided to the expansion turbine.

A gas turbine engine duct turns radially inwardly in the downstream direction. The duct includes a plurality of radially extending stator vanes. A generally circumferentially extending splitter vane is provided between two circumferentially neighbouring stator vanes. The splitter vane improves the flow near to the radially inner wall of the duct. This can allow greater design freedom in the duct geometry.

A gas turbine engine includes a combustion section arranged between a compressor section and a turbine section that extend in an axial direction. A fan section is arranged upstream from the compressor section. An airfoil is arranged in one of the fan section, the compressor section and the turbine section. The airfoil includes pressure and suction sides extending in a radial direction from a 0% span position at an inner flow path location to a 100% span position at an airfoil tip. The airfoil has a leading edge that is projected onto a plane from various views and the plane is perpendicular to a viewing direction which corresponds to the various views. The plane is parallel with the axial direction in a 0° view. The various views include the 0° view which projects into an axial plane in the axial direction. A 90° view projects into a tangential plane in a tangential direction normal to the axial direction and views between the 0° and 90° views. The airfoil has a maximum leading edge projection in a 20° to 40° view. The radial direction is normal to the axial and tangential directions.

In this podcast, Thomas Domville shows us how to tell if your iPhone is new, refurbished or a replacement.

This story ran on Morning Edition and All Things Considered. Gloria Vanderbilt was an artist, heiress, designer and philanthropist who, for many Americans, may be best remembered for her blue jeans . She died at the age of 95. Vanderbilt's son, Anderson Cooper, announced her death Monday, airing an obituary for her on CNN. Vanderbilt had cancer, he said. "Earlier this month, we had to take her to the hospital. That's where she learned she had very advanced cancer in her stomach, and that it had spread," Cooper said. "What an extraordinary life. What an extraordinary mom. And what an incredible woman," he said, his voice quavering a bit at the end of the remembrance. Vanderbilt had full lips, eyes that turned up at the corners and a patrician bearing. She was, in fact, descended from shipping and railroad tycoon Cornelius Vanderbilt, one of the richest men in American history. She was born in 1924, and her father died shortly thereafter. Vanderbilt was raised by a beloved nurse because

Die Bundesliga startet am 16. Mai in die verbleibende Spielzeit. TSG-Geschäftsführer Dr. Peter Görlich ist sich bewusst, dass man das Vertrauen der Politik zurückzahlen muss.

Bradley and Karen discuss two debates going on in the free and open source software community. One recent and seemingly inflated, and one long and confusing.

Show Notes:

Segment 1 (03:12)

• Bradley wrote a blog post about the Bionic issues that were raised. (03:44)
• On the old oggcast, Karen and Bradley discussed the Android/Linux system and Bionic specifically. (04:09)
• Karen mentioned an old oggcast where permissive vs. copyleft licensing was discussed. (06:19)
• Jake Edge wrote an LWN article that discussed Bionic (07:58)
• Bradley mentioned Raymond Nimmer's blog that started the debate (10:52)
• Bradley also mentioned Edward Naughton's blog post and paper on Bionic. (11:38)
• Raymond Nimmer is not David Nimmer, who is known for writings on copyright (18:10)
• There is now an disturbing group on identica, which is more disturbing than a tag about disturbing. (19:15)
• Joe Brockmeier did some research on Edward Naughton's ties to Microsoft. (20:05)
• Karen mentioned a paper on deep legal analysis of header files and on originality requirements in copyright (24:40)

Segment 2 (26:07)

• Karen wanted to clear up some confusion about the discussion last episode about the “Open Source” and “Free Software” terminology.

Send feedback and comments on the cast to <oggcast@faif.us>. You can keep in touch with Free as in Freedom on our IRC channel, #faif on irc.freenode.net, and by following Conservancy on on Twitter and and FaiF on Twitter.

Free as in Freedom is produced by Dan Lynch of danlynch.org. Theme music written and performed by Mike Tarantino with Charlie Paxson on drums.

The content of this audcast, and the accompanying show notes and music are licensed under the Creative Commons Attribution-Share-Alike 4.0 license (CC BY-SA 4.0).

The drastic decline over the past four decades is linked to widespread drought which is causing bodies of water to disappear, devastating waterbird population numbers.

Authorities say a "perfect storm" has caused a disturbing rise in domestic violence cases, as the parents of murdered woman Hannah Clarke ask Queenslanders to support a vigil to remember victims.

Arbitrage segues smoothly into a psychological thriller, seamlessly weaving the financial finagling into the slow decline and fall of Robert Miller's moral universe.

From balcony book clubs to re-reading, we asked professional readers how and what they're reading through the lockdown.

Gold Coast junior Riley Parsons shares his love of cricket, by refurbishing old gear to give to kids who need it.

Almost a decade ago, Charles Brice was thrown from a motorbike in a trail-riding accident, and spent more than a year in rehab. This week, he completed a 300-kilometre road trip from the crash site.

Pelicans and other waterbirds are dying in the outback and disappearing from waterways, as the effects of drought compound an already-concerning long-term decline in populations.

Researchers monitoring the impact of climate change say golden bowerbirds and other highland rainforest species are being pushed to higher altitudes by temperature rises and fear they'll eventually have nowhere left to go.

A 60-tonne truck carrying part of a wind turbine rolls over in Tasmania's central highlands, leaving a 68-metre blade across the road.

DAILY BRIEFING: A road in the Central Highlands has reopened after a truck carrying a 68-metre-long wind turbine blade lost its load, a 39-year-old woman dies after being hit by a car and CPSU encourages public sector workers to take part in climate protests.

Isabella Corbin can remember sitting on her dad's lap in the cockpit of his helicopter when she was just a baby. Two years after his death, she's determined to keep his legacy alive.