Quach, US
Anderson K. Quach, Seattle, WA US
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20100318964 | SOFTWARE EXTENSION ANALYSIS - Multiple structured extension definitions can be obtained, each structured extension definition corresponding to one or more categories, and each structured extension definition being written in a software extension language. Data representing one or more registrations maintained in a format native to a registration store can be accessed, and this data analyzed based at least in part on the multiple structured definitions. In other aspects, a structured extension definition written in a software extension language is obtained. The registration store includes registrations stored in a format native to the registration store and different from the software extension language, and the registration store is modified based on the obtained structured extension definition. | 12-16-2010 |
Brian Quach, Richardson, TX US
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20140297898 | MULTI-CHANNEL PERIPHERAL INTERCONNECT SUPPORTING SIMULTANEOUS VIDEO AND BUS PROTOCOLS - A method includes generating, by a control unit of a first device, a handshaking signal to be transmitted to a second device via a second channel. The method further includes based on the handshaking signal being acknowledged by the second device, configuring, by the control unit, the second channel to communicate non-display data and configuring a first channel connecting the first device to the second device to selectively communicate either display data or non-display data; and based on the handshaking signal being not acknowledged by the second device, configuring, by the control unit, the first channel to communicate display data. | 10-02-2014 |
Brian H. Quach, Richardson, TX US
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20160062924 | SIMULTANEOUS VIDEO AND BUS PROTOCOLS OVER SINGLE CABLE - Method and systems are disclosed for transporting simultaneous video and bus protocols over a single cable. At least some of the illustrative embodiments are systems including a main switch configured to operate in an enhanced mode where the main switch is configured to transfer data from a first data source and a second data source to a cable, operate in a default mode where the main switch is configured to transfer data from the second data source to the cable without transferring data from the first data source; a multipurpose switch configured to operate in a handshake mode where the multipurpose switch transports handshake data between the cable and a digital logic, operate in a data mode where the multipurpose switch transports bus data between the cable and the second data source; and the digital logic programed to enable modes of operation of the multipurpose switch and the main switch. | 03-03-2016 |
Hai C. Quach, Laredo, TX US
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20140000017 | Toilet Bowl Cleaning Device and Method | 01-02-2014 |
Lesley Quach, Seattle, WA US
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20140122586 | DETERMINATION OF LATENT INTERACTIONS IN SOCIAL NETWORKS - A method including processing social network data to establish a tensor model of the social network data, the tensor model having at least an order of four. The tensor model is decomposed into a plurality of principal factors. A summary tensor is synthesized from a subset of the plurality of principal factors. The summary tensor represents a plurality of relationships among a plurality of entities in the tensor model. A synthesis of relationships is formed and stored. At least one parameter is identified using one of the summary tensor and a single principal factor in the subset. The at least one parameter is selected from the group consisting of: a correlation among the plurality of entities, a similarity between two of the plurality of entities, and a time-based trend of changes in the synthesis of relationships. The at least one parameter is communicated. | 05-01-2014 |
Lilian Mi Quach, Grand Prairie, TX US
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20150309715 | Media Service User Interface Systems and Methods - In an exemplary method, a media service user interface system provides, for display on a screen of a primary display device, a media menu tray user interface view that includes a media menu tray representing a menu of one or more media programs and provides, for display on a display screen of a mobile device while the media menu tray user interface view is provided for display on the display screen of the primary display device, a remote control user interface view dynamically tailored to facilitate remote user interaction with the media menu tray included in the media menu tray user interface view provided for display on the display screen of the primary display device. In certain examples, the remote control user interface view is dynamically tailored based on a current state of the media menu tray user interface view. | 10-29-2015 |
20150312608 | Media Service Personalization Systems and Methods - In an exemplary method, a media service personalization system directs a media service access device to operate in accordance with a shared mode of operation when user interaction with the media service access device is by way of a shared user input device and directs the media service access device to operate in accordance with a personal mode of operation when user interaction with the media service access device is by way of a personal device specific to a user. In certain examples, the media service personalization system may switch between directing the media service access device to operate in accordance with the shared mode of operation and directing the media service access device to operate in accordance with the personal mode of operation based on a status of a remote control session between the personal device and the shared media service access device. | 10-29-2015 |
Linh Quach, Arlington Heights, IL US
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20100298594 | PRODUCTION OF N,N-DIALKLYLAMINOETHYL (METH)ACRYLATES - A method and apparatus for preparing a N,N-dialkylaminoalkyl acrytate in a continuous transesterification reaction. The reaction involves adding alkyl acrylates such as methacrylate or ethacrylate to a reboiler mechanism and efficiently removing alcohol co-products. Because the reaction is continuous, the alkyl acrylates can be added as needed to increase output, decrease output, or fine-tune the reaction dynamics. An entrainer is used to form a volatile azeotrope which contains both alcohol and entrainer and which is easily removed from the reboiler mechanism. This method reduces the amount of entrainer needed per unit of alkyl acrylate used and eliminates any need to purify the end product from entrainer contamination of the resulting N,N-dialkylaminoalkyl acrylate product. | 11-25-2010 |
Minh Van Quach, Fort Collins, CO US
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20080237893 | Anti Pad To Reduce Parasitic Capacitance And Improve Return Loss In A Semiconductor Die And Package - An apparatus for minimizing parasitic capacitance on a semiconductor die includes a semiconductor die having a least one signal line and at least one plane and an anti pad located between the at least one signal line and the at least one plane. | 10-02-2008 |
Natalie Quach, Austin, TX US
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20110035515 | System and Method of Providing a User-Friendly Device Path - A method can include, during a boot flow at an information handling system, receiving an initial device path related to a device that is integrated with or coupled to the information handling system. The method can also include identifying a system-specific device location table based on a node included in the initial device path and receiving a particular alternate location string associated with the node at the system-specific location table. Further, the method can include adding the particular alternate location string to an alternate device path string related to the device and outputting the alternate device path to a user after the alternate device path includes an alternate location string associated with each node of the initial device path. | 02-10-2011 |
Natalie N. Quach, Austin, TX US
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20090292949 | SYSTEM AND METHOD OF MANAGING BIOS TEST ROUTNES - A system and method of a basic input output system (BIOS) test system are disclosed. According to an aspect, a basic input output system (BIOS) test system can include a BIOS test manager configured to enable BIOS testing of multiple information handling systems within a test environment. The BIOS test system can also include a local test harness driver operable to be coupled to the remote BIOS test manager to receive test routines, and a test buffer configured to receive a test routine from the BIOS test manager. The test routine can further be executed using a test engine integrated as a part of a BIOS of a particular information handling system. | 11-26-2009 |
Quyen Quach, Redmond, WA US
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20160071157 | METHOD AND APPARATUS FOR PROVIDING CONTENT IN A COMMUNICATION SYSTEM - Aspects of the subject disclosure may include, for example, a device including a memory and a processor for performing operations including accessing a user persona comprising a plurality of attributes and a plurality of content preferences of a user of a communication device, presenting at an interactive site a plurality of content suggestions that are generated according to the user persona, receiving a content selection from a presentation of the plurality of content suggestions at the interactive site, and updating the plurality of content preferences of the user persona according to the content selection. Other embodiments are disclosed. | 03-10-2016 |
San Quach, East Hartford, CT US
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20130243596 | SHARK-BITE TIP SHELF COOLING CONFIGURATION - An airfoil includes a leading edge, a trailing edge, a suction surface, a pressure surface, and a tip shelf. The suction surface and the pressure surface both extend axially to connect the leading edge to the trailing edge. The suction surface and the pressure surface both extend radially from a root section of the airfoil a tip section of the airfoil. The tip shelf is formed along the tip section, and includes a triangular pocket. | 09-19-2013 |
20130251539 | TRAILING EDGE OR TIP FLAG ANTIFLOW SEPARATION - An airfoil includes a leading edge, a trailing edge region, a suction surface, a pressure surface, a cooling passageway, and a column of flow separators. The suction surface and the pressure surface both extend axially between the leading edge and the trailing edge region, as well as radially from a root section of the airfoil to a tip section of the airfoil to define a central cavity of the airfoil. The cooling passageway is located within the central cavity at the trailing edge region. The column of flow separators is located in the cooling passageway adjacent the trailing edge and includes a first flow separator having a first longitudinal axis and a second flow separator having a second longitudinal axis. The first longitudinal axis is offset at an angle with respect to the first longitudinal axis. | 09-26-2013 |
20130266454 | TURBINE AIRFOIL TIP SHELF AND SQUEALER POCKET COOLING - An airfoil comprises leading and trailing edges with pressure and suction surfaces defining a chord length therebetween. The pressure and suction surfaces extend from a root section of the airfoil to a tip section. A tip shelf is formed along the tip section between the pressure surface and a tip shelf wall spaced between the pressure surface and the suction surface. A squealer pocket is formed along the tip section between the tip shelf wall and a squealer tip wall extending from the suction surface. The tip shelf extends from within 10% of the cord length measured from the leading edge to within 10% of the chord length measured from the trailing edge. The squealer pocket extends from within 10% of the chord length measured from the leading edge to terminate between 10% and 25% of the chord length measured from the trailing edge. | 10-10-2013 |
20130302141 | Convective Shielding Cooling Hole Pattern - The cooling system for a turbine may include a plurality of platform cooling openings positioned in a platform of the turbine airfoil. In particular, the first set of cooling openings may create a first cooling path and a second set of cooling openings may be placed in the path of the first cooling path where the first cooling flow will cool the second set of cooling openings. | 11-14-2013 |
20140010666 | AIRFOIL COOLING CIRCUITS - An airfoil includes leading and trailing edges; first and second sides extending from the leading edge to the trailing edge, each side having an exterior surface; a core passage located between the first and second sides and the leading and trailing edges; and a wall structure located between the core passage and the exterior surface of the first side. The wall structure includes a plurality of cooling fluid inlets communicating with the core passage for receiving cooling fluid from the core passage, a plurality of cooling fluid outlets on the exterior surface of the first side for expelling cooling fluid and forming a cooling film along the exterior surface of the first side, and a plurality of cooling passages communicating with the plurality of cooling fluid inlets and the plurality of cooling fluid outlets. At least a portion of one cooling passage extends between adjacent cooling fluid outlets. | 01-09-2014 |
20140033736 | GAS TURBINE ENGINE COMPONENT COOLING CIRCUIT - A component for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a body portion, a cooling circuit disposed within the body portion and including at least a first cavity and a microcircuit in fluid communication with the first cavity. A plunged hole intersects at least a portion of the microcircuit. | 02-06-2014 |
20140064930 | Turbine Engine Transmission Gutter - A turbine engine case defines a centerline and a gaspath within the engine case. A fan is coupled to a fan shaft. A transmission couples the shaft to the fan shaft to drive the fan and comprises a gear system. A gutter system is positioned to capture lubricating fluid slung from the gear system. The gutter system includes a gutter extending partially circumferentially about the centerline having a first circumferential end edge. An inlet channel has an inlet at the gutter first circumferential end edge and locally radially outboard of the gutter. At least one vane is spaced apart from the gutter first circumferential end edge. | 03-06-2014 |
20140165593 | GAS TURBINE ENGINE TURBINE BLADE LEADING EDGE TIP TRENCH COOLING - An airfoil for a gas turbine engine includes pressure and suction walls spaced apart from one another and joined at leading and trailing edges to provide an airfoil having an exterior surface that extends in a radial direction to a tip. A tip trench is provided in the tip and wrapping at least a portion of the airfoil from the pressure side wall around the leading edge to the suction side wall. The tip trench is provided by a recess. | 06-19-2014 |
20140199177 | AIRFOIL AND METHOD OF MAKING - An airfoil includes leading and trailing edges, a first exterior wall extending from the leading edge to the trailing edge and having inner and outer surfaces, a second exterior wall extending from the leading edge to the trailing edge generally opposite the first exterior wall and having inner and outer surfaces, and cavities within the airfoil. A first cavity extends along the inner surface of the first exterior wall and a first inner wall and has an upstream end and a downstream end, and a feed cavity is located between the first inner wall and the second exterior wall. | 07-17-2014 |
20150260048 | COMPONENT WITH COOLING HOLE HAVING HELICAL GROOVE - One exemplary embodiment of this disclosure relates to a component for a gas turbine engine. The component includes a cooling hole having a wall with at least one helical groove formed in the wall. | 09-17-2015 |
20150300180 | GAS TURBINE ENGINE TURBINE BLADE TIP WITH COATED RECESS - A blade for a gas turbine engine includes an airfoil that has a tip with a terminal end surface. The terminal end surface includes a recess that has a depth of less than 40 mils (1.016 mm). The recess is filled with a thermal barrier coating. The recess is without any cooling holes. | 10-22-2015 |
20150300258 | COOLING HOLE ARRANGEMENT FOR ENGINE COMPONENT - A component for a gas turbine engine according to an exemplary aspect of this disclosure includes a surface having a plurality of cooling holes. The surface includes a first region and a second region each having a plurality of cooling holes. The cooling holes within the first region are arranged differently than the cooling holes in the second region. | 10-22-2015 |
20150315929 | GAS TURBINE ENGINE AIRFOIL COOLING PASSAGE CONFIGURATION - An airfoil for a gas turbine engine includes an airfoil body that extends in a radial direction from a support. The airfoil body has pressure and suction side walls joined at leading and trailing edges to provide an exterior airfoil surface. A chord-wise direction extends between the leading and trailing edges and a thickness direction transverse to chord-wise direction and extending between the pressure and suction side walls. Cooling passages extend from the support into the airfoil body. The cooling passages include adjacent passageways in the thickness direction and are separated by a chord-wise wall. One of the adjacent passageways is adjacent to another passageway in the chord-wise direction and is separated by a rib in the thickness direction. The rib is discontinued at a location along the radial direction to provide an opening that fluidly connects one of the adjacent passageways to the other passageway. | 11-05-2015 |
20150330228 | AIRFOIL TIP POCKET WITH AUGMENTATION FEATURES - A component according to an exemplary aspect of the present disclosure includes, among other things, an airfoil that includes a pressure sidewall and a suction sidewall that meet together at both a leading edge and a trailing edge. The airfoil extends to a tip. A tip pocket is formed in the tip and terminates prior to the trailing edge. A heat transfer augmentation device is formed in the tip pocket. | 11-19-2015 |
20150354372 | GAS TURBINE ENGINE COMPONENT WITH ANGLED APERTURE IMPINGEMENT - A component for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a body portion that includes a first wall spaced apart from a second wall. At least one rib extends between the first wall and the second wall and at least one aperture extends through the at least one rib. The at least one aperture is angled relative to a radial axis of the at least one rib. | 12-10-2015 |
20160003053 | GAS TURBINE ENGINE COMPONENT HAVING TRANSVERSELY ANGLED IMPINGEMENT RIBS - A component for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a body portion that includes a first wall spaced apart from a second wall and disposed about a centerline axis. At least one rib extends between the first wall and the second wall. The at least one rib extends along a rib axis that is transversely angled relative to the centerline axis. At least one impingement hole extends through the at least one rib. | 01-07-2016 |
20160040534 | DISK LUG IMPINGEMENT FOR GAS TURBINE ENGINE AIRFOIL - A component for a gas turbine engine includes a root with a neck that extends into a fir tree with at least one tooth, the root includes a feed passage in communication with a multiple of cooling passages that extend through the neck and fir tree. | 02-11-2016 |
20160069189 | SPLAYED TIP FEATURES FOR GAS TURBINE ENGINE AIRFOIL - A component for a gas turbine engine includes a trailing edge tip corner that at least partially defines a trailing edge cavity and a multiple of corner features within the trailing edge cavity, the multiple of corner features splayed along the trailing edge tip corner. | 03-10-2016 |
San Quach, Southington, CT US
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20150292334 | TURBINE AIRFOIL TIP SHELF AND SQUEALER POCKET COOLING - An airfoil includes a pressure surface and a suction surface extending from a root section of the airfoil to a tip section of the airfoil. The airfoil also includes a leading edge and a trailing edge defining a chord length of the airfoil therebetween. The airfoil further includes a tip shelf formed along the tip section of the airfoil between the pressure surface and a tip shelf wall. The tip shelf wall is spaced between the pressure surface and the suction surface and the tip shelf extends from within 10% of the chord length measured from the leading edge to within 10% of the chord length measured from the trailing edge. | 10-15-2015 |
Tan Dinh Quach, Grand Blanc, MI US
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20080198077 | MOBILE WIDEBAND ANTENNAS - In various exemplary embodiments, a wideband antenna assembly includes a stamped monopole antenna mast having two or more conductors combined to a single feed. The conductors are combined at a predetermined height above the point of connection with the single feed. The conductors further have a predetermined spacing between the conductors. | 08-21-2008 |
Thanh H. Quach, Macomb, MI US
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20080258442 | Method and apparatus for placing an inflatable curtain in a stored condition - An apparatus ( | 10-23-2008 |
20080258445 | Inflatable curtain module with push-in fastener - An apparatus ( | 10-23-2008 |
Trung Quach, Bonney Lake, WA US
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20090235704 | DEADBOLT LOCK KNOB RESISTOR - A deadbolt knob restrictor used to prevent the rotation of the inside knob on the deadbolt lock. The restrictor includes a ring member designed to fit between the cover plate located on the inside surface of the door. Attached to the ring member are two perpendicularly aligned support arms with a pin-style hinge formed on their distal ends. Attached to the hinge is an L-shaped latch. Formed on the latch is a cam surface which presses against a spring loaded piston disposed between the cam surface and the support arm. The latch includes a long leg that may be disposed transversely over the ring member, and a short leg that may be placed adjacent to the wide surface of the deadbolt lock's turn knob to prevent its rotation. During assembly, the ring member is placed under the locks inside cover plate. During use the piston forcibly holds the latch in a locked or unlocked position against the turn knob. The latch may be rotated in the opposite direction so that the turn knob is free to rotate to the unlock position. | 09-24-2009 |
Trung T. Quach, Surprise, AZ US
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20150023170 | TRAFFIC MEASUREMENT SYSTEM FOR WIRELESS SERVICE PROVIDERS - A device receives packet information associated with a traffic flow and a network segment. The network segment includes a portion of a network via which the traffic flow is transmitted. The device associates the received packet information with a period of time. The device determines that the period of time has expired, and aggregates the received packet information based on determining that the period of time has expired. The device determines a network performance parameter associated with the traffic flow over the network segment based on the aggregated packet information. The device generates performance information that identifies the network performance parameter, the traffic flow, and the network segment. The device provides the performance information. | 01-22-2015 |