Patent application number | Description | Published |
20080309384 | Initialization Circuitry Having Fuse Leakage Current Tolerance - A system for initializing circuitry is presented. The system employs a power-on reset circuit having a threshold voltage and a programmable switch circuit. The power-on reset circuit has a detector circuit for detecting a reference voltage, and a one-sided latch for generating an output voltage reflective of the reference voltage. The detector circuit has a threshold after which the one-sided latch is activated. The programmable switch circuit receives the output voltage of the power-on reset circuit and generates an enable signal arid its complement based on the status of an internal fuse. The switch point of the power-on reset circuit provides for a rapid increase in output voltage, offsetting parasitic leakage current in the programmable switch circuit that can result in improper enable signal output. | 12-18-2008 |
20130241014 | MAGNETORESISTIVE RANDOM ACCESS MEMORY (MRAM) PACKAGE INCLUDING A MULTILAYER MAGNETIC SECURITY STRUCTURE - A magnetoresistive random access memory (MRAM) package may include an MRAM die, a package defining a cavity and an exterior surface, and a magnetic security structure disposed within the cavity or on the exterior surface of the package. The MRAM die may be disposed in the cavity of the package, and the magnetic security structure may include at least three layers including a permanent magnetic layer and a soft magnetic layer. | 09-19-2013 |
20130242646 | MAGNETORESISTIVE RANDOM ACCESS MEMORY (MRAM) DIE INCLUDING AN INTEGRATED MAGNETIC SECURITY STRUCTURE - An MRAM die may include a first write line, a second write line, an MRAM cell disposed between the first write line and the second write line, and a magnetic security structure adjacent to the MRAM cell. The magnetic security structure may include a permanent magnetic layer and a soft magnetic layer. | 09-19-2013 |
20130250662 | TAMPER-RESISTANT MRAM UTILIZING CHEMICAL ALTERATION - A magnetoresistive random access memory (MRAM) die may include an MRAM cell, a reservoir defined by the MRAM die, and a chemical disposed in the reservoir. At least one boundary of the reservoir may be configured to be damaged in response to attempted tampering with the MRAM die, such that at least some of the chemical is released from the reservoir when the at least one boundary of the reservoir is damaged. In some examples, at least some of the chemical is configured to contact and alter or damage at least a portion of the MRAM cell when the chemical is released from the reservoir. | 09-26-2013 |
20130250663 | ANTI-TAMPERING DEVICES AND TECHNIQUES FOR MAGNETORESISTIVE RANDOM ACCESS MEMORY - A system may include circuitry and a magnetoresistive random access memory (MRAM) die including at least one MRAM cell. The circuitry may be configured to detect attempted tampering with the MRAM die and generate a signal based on the detected attempted tampering. The signal may be sufficient to damage or destroy at least one layer of the at least one MRAM cell or a fuse electrically connected to a read line of the at least one MRAM cell. | 09-26-2013 |
Patent application number | Description | Published |
20120166963 | CONVERTING DESKTOP APPLICATIONS TO WEB APPLICATIONS - Technologies are described herein for converting a desktop application to a web application. An interface file is generated based on a user interface of the desktop application. A logic file is generated based on application executables of the desktop application. A data model is generated based on application data and states of the desktop application. The web application is generated based on the interface file, the logic file, and the data model. | 06-28-2012 |
20120167117 | STORING AND RESUMING APPLICATION RUNTIME STATE - Execution of an application is suspended and the runtime state of the application is collected and persisted. Maintenance operations may then be performed on the computer that the application was executing upon. The runtime state might also be moved to another computer. In order to resume execution of the application, the runtime state of the application is restored. Once the runtime state of the application has been restored, execution of the application may be restarted from the point at which execution was suspended. A proxy layer might also be utilized to translate requests received from the application for resources that are modified after the runtime state of the application is persisted. | 06-28-2012 |
20160026478 | Converting Desktop Applications to Web Applications - Technologies are described herein for converting a desktop application to a web application. An interface file is generated based on a user interface of the desktop application. A logic file is generated based on application executables of the desktop application. A data model is generated based on application data and states of the desktop application. The web application is generated based on the interface file, the logic file, and the data model. | 01-28-2016 |
20160103701 | Storing and Resuming Application Runtime State - Execution of an application is suspended and the runtime state of the application is collected and persisted. Maintenance operations may then be performed on the computer that the application was executing upon. The runtime state might also be moved to another computer. In order to resume execution of the application, the runtime state of the application is restored. Once the runtime state of the application has been restored, execution of the application may be restarted from the point at which execution was suspended. A proxy layer might also be utilized to translate requests received from the application for resources that are modified after the runtime state of the application is persisted. | 04-14-2016 |
Patent application number | Description | Published |
20080226462 | CAST FEATURES FOR A TURBINE ENGINE AIRFOIL - An airfoil for a turbine engine includes a structure having a cooling passage that has a generally radially extending cooling passageway arranged interiorly relative to an exterior surface of the structure. The cooling passageway includes multiple cooling slots extending there from toward the exterior surface and interconnected by a radially extending trench. The trench breaks the exterior surface, and the exterior surface provides the lateral walls of the trench. The airfoil is manufactured by providing a core having multiple generally axially extending tabs and a generally radially extending ligament interconnecting the tabs. The structure is formed about the core to provide the airfoil with its exterior surface. The ligament breaks the exterior surface to form the radially extending trench in the exterior surface of the structure. | 09-18-2008 |
20090028702 | BLADE COOLING PASSAGE FOR A TURBINE ENGINE - A blade for a turbine engine includes structure providing spaced apart suction and pressure sides. A cooling passage includes a first passageway near the pressure side and a second passageway in fluid communication with the first passageway. The second passageway is arranged between the first passageway and the suction side. The cooling passage provides a serpentine cooling path that is arranged in a direction transverse from a chord extending between trailing and leading edges of the blade. During use, cooling fluid is supplied to the pressure side through first cooling apertures fluidly connected to the first passageway to the suction side through second cooling apertures fluidly connected to the other passage way. The first passageway is at a higher pressure that then second passageway so that cooling fluid is provided by the cooling passage to the pressure and suction sides in a balanced fashion. | 01-29-2009 |
20100040478 | Cooled Airfoils and Gas Turbine Engine Systems Involving Such Airfoils - Cooled airfoils and gas turbine engine systems involving such airfoils are provided. In this regard, a representative cooled airfoil includes: an exterior surface defining a leading edge, a trailing edge, a suction side and a pressure side; an interior surface defining an interior cavity; trenches in the exterior surface oriented spanwise along the leading edge; and cooling holes communicating between the interior cavity and the trenches such that cooling air provided to the interior cavity flows from the interior cavity though the cooling holes into the trenches, the cooling holes having exterior apertures located in the trenches and interior apertures located at the interior surface. | 02-18-2010 |
20110132876 | ARTICLE HAVING DIFFUSER HOLES AND METHOD OF MAKING SAME - The diffusion opening in the cooling hole of an airfoil is formed by an EDM process in which the outwardly flaring sidewalls of the opening, rather then having surfaces that are approximated to be smooth by having many small ribs formed therein, are formed with a relatively few ribs with both longitudinally extending and radially extending surfaces that are substantially greater in dimension than those as normally formed. In this manner, the machining process is simplified and expedited, while at the same time, the cooling efficiency is increased. | 06-09-2011 |
20120027619 | CAST FEATURES FOR A TURBINE ENGINE AIRFOIL - An airfoil for a turbine engine includes a structure having a cooling passage that has a generally radially extending cooling passageway arranged interiorly relative to an exterior surface of the structure. The cooling passageway includes multiple cooling slots extending there from toward the exterior surface and interconnected by a radially extending trench. The trench breaks the exterior surface, and the exterior surface provides the lateral walls of the trench. The airfoil is manufactured by providing a core having multiple generally axially extending tabs and a generally radially extending ligament interconnecting the tabs. The structure is formed about the core to provide the airfoil with its exterior surface. The ligament breaks the exterior surface to form the radially extending trench in the exterior surface of the structure. | 02-02-2012 |
20130039777 | AIRFOIL INCLUDING TRENCH WITH CONTOURED SURFACE - A airfoil comprises a wall, a cooling channel, a trench and a plurality of leading edge cooling holes. The wall has a leading edge, a trailing edge, a pressure side, a suction side, an outer diameter end and an inner diameter end to define an interior. The cooling channel extends radially through the interior of the wall between the pressure side and the suction side and along the leading edge. The trench extends radially along an exterior of the wall at the leading edge and is recessed axially into the leading edge to form a back wall. The back wall is contoured to include at least one undulation. The plurality of leading edge cooling holes extends through the back wall of the trench to connect the interior of the wall at the cooling channel to the exterior. | 02-14-2013 |
20130205786 | COOLING HOLE WITH THERMO-MECHANICAL FATIGUE RESISTANCE - A gas turbine engine includes a wall having first and second wall surfaces and a cooling hole extending through the wall. The cooling hole includes an inlet located at the first wall surface, an outlet located at the second wall surface, a metering section extending downstream from the inlet and a diffusing section extending from the metering section to the outlet. The diffusing section includes a first lobe diverging longitudinally and laterally from the metering section, a second lobe diverging longitudinally and laterally from the metering section, an upstream end located at the outlet, a trailing edge located at the outlet opposite the upstream end and generally opposite first and second sidewalls. Each sidewall has an edge extending along the outlet between the upstream end and the trailing edge. Each edge diverges laterally from the upstream end and converges laterally before reaching the trailing edge. | 08-15-2013 |
20130205787 | TRI-LOBED COOLING HOLE AND METHOD OF MANUFACTURE - A gas turbine engine component includes first and second wall surfaces, an inlet located at the first wall surface, an outlet located at the second wall surface and a diffusing section positioned between the inlet and the outlet. The diffusing section includes a first lobe, a second lobe adjacent the first lobe and a third lobe adjacent the second lobe. The first lobe and the second lobe meet at a first ridge and the second lobe and the third lobe meet at a second ridge. | 08-15-2013 |
20130205790 | MULTI-LOBED COOLING HOLE AND METHOD OF MANUFACTURE - A gas turbine engine component includes a cooling hole. The cooling hole includes an inlet, an outlet, a metering section and a diffusing section. The diffusing section extends from the metering section to the outlet and includes a first lobe diverging longitudinally and laterally from the metering section, a second lobe adjacent the first lobe and diverging longitudinally and laterally from the metering section, and a transition region having a portion that extends between the first and second lobes and an end adjacent the outlet. | 08-15-2013 |
20130205792 | COOLING HOLE WITH ASYMMETRIC DIFFUSER - A gas turbine engine component includes a wall having first and second wall surfaces and a cooling hole extending through the wall. The cooling hole includes an inlet located at the first wall surface, an outlet located at the second wall surface, a metering section extending downstream from the inlet and a diffusing section extending from the metering section to the outlet. The diffusing section includes a first lobe diverging longitudinally from the metering section and a second lobe adjacent the first lobe and diverging longitudinally and laterally from the metering section. | 08-15-2013 |
20130205801 | MULTI-LOBED COOLING HOLE AND METHOD OF MANUFACTURE - A gas turbine engine component includes a wall having first and second wall surfaces and a cooling hole extending through the wall. The cooling hole includes an inlet at the first wall surface, an outlet at the second wall surface, a metering section extending downstream from the inlet and a diffusing section extending from the metering section to the outlet. The diffusing section includes a first lobe diverging longitudinally and laterally from the metering section, a second lobe adjacent the first lobe and diverging longitudinally from the metering section, a third lobe adjacent the second lobe and diverging longitudinally and laterally from the metering section, and a transition region having an end adjacent the outlet and a portion that extends between the lobes and the outlet. The first and third lobes each include a curved outer portion. | 08-15-2013 |
20130209269 | GAS TURBINE ENGINE COMPONENT WITH MULTI-LOBED COOLING HOLE - A component for a gas turbine engine includes a wall and a cooling hole extending through the wall. The wall has a first surface and a second surface. The cooling hole includes a metering section extending downstream from an inlet in the first surface of the wall and a diffusion section extending from the metering section to an outlet in the second surface of the wall. The diffusion section includes a first plurality of lobes diverging longitudinally and laterally from the metering section on a first side of a centerline axis of the cooling hole and a second plurality of lobes diverging longitudinally and laterally from the metering section on a second side of the centerline axis. | 08-15-2013 |
20140190654 | CAST FEATURES FOR A TURBINE ENGINE AIRFOIL - A core assembly for a turbine engine blade includes a generally radially extending trunk interconnected to multiple generally axially extending tabs. The tabs are interconnected by a generally radially extending ligament. Multiple generally axially extending protrusions are interconnected to the ligament opposite the trunk. A mold is configured to define an exterior surface of an airfoil. The core is arranged within the mold and is configured such that the tabs and the ligament break through at the exterior surface. | 07-10-2014 |
20140219815 | MULTI-LOBED COOLING HOLE - A gas turbine engine component subjected to a flow of high temperature gas includes a wall having first and second wall surfaces and a cooling hole extending through the wall. The cooling hole includes an inlet located at the first wall surface, an outlet located at the second wall surface, a metering section extending downstream from the inlet and a diffusing section extending from the metering section to the outlet. The diffusing section includes a first lobe, a second lobe and a transition region. The first lobe diverges longitudinally and laterally from the metering section and has a first shape. The second lobe is generally opposite the first lobe and diverges longitudinally and laterally from the metering section and has a second shape different from the first shape. The transition region is positioned between the first and second lobes and includes a downstream end adjacent the outlet. | 08-07-2014 |
20150226085 | BAFFLE WITH FLOW AUGMENTATION FEATURE - One exemplary embodiment of this disclosure relates to a component for a gas turbine engine. The component includes a baffle provided in an internal cavity of the component. The baffle includes a wall having an orifice therethrough, and the baffle further includes a lobe extending from the wall and at least partially covering the orifice. | 08-13-2015 |
20150354365 | GAS TURBINE ENGINE AIRFOIL WITH LARGE THICKNESS PROPERTIES - An airfoil for a gas turbine engine includes an airfoil with pressure and suction sides that are joined at leading and trailing edges. The airfoil extends a span from a support to an end in a radial direction. 0% span and 100% span positions respectively correspond to the airfoil at the support and at the end. The leading and trailing edges are spaced apart from one another an axial chord in an axial direction. A cross-section of the airfoil at a span location has a diameter tangent to the pressure and suction sides. The diameter corresponds to the largest circle fitting within the cross-section. A ratio of the diameter to the axial chord is at least 0.4 between 50% and 95% span location. | 12-10-2015 |
20160047251 | COOLING HOLE HAVING UNIQUE METER PORTION - A gas turbine engine component has a cooling hole with a metering section. The metering section includes a convex surface and a concave surface, with a first arcuate channel connecting an end of the convex surface and an end of the concave surface. The end of the convex surface and the end of the concave surface define a dimension that is smaller than a diameter of the arcuate channel. | 02-18-2016 |
Patent application number | Description | Published |
20110048637 | HIGH PERFORMANCE ADHESIVE COMPOSITIONS - Thermosetting adhesive compositions formed from an epoxy resin containing nano-sized core-shell particles, one or more thermoplastic toughening agent containing an amine-terminated polyethersulfone, and at least one multi-functional epoxy resin, together with at least one amine curing agent to allow full cure of the adhesive composition up to 400° F. are provided herein. Such compositions are useful for forming adhesive films that can bond composite/metal/honeycomb structures for aerospace including bonding of aircraft leading or trailing edges, acoustic nacelle structures, horizontal and vertical tail, and various other structures, as well as for other high performance industrial applications. | 03-03-2011 |
20140187672 | CORROSION-INHIBITING MICROGELS AND NON-CHROMATED PRIMER COMPOSITIONS INCORPORATING THE SAME - Corrosion-inhibiting microgels that are suitable for use in non-chromated primer compositions. Each discrete microgel is composed of a cross-linked polymer network and organic corrosion-inhibiting compounds entrapped or immobilized within the polymer network. | 07-03-2014 |
20150056433 | BONDING OF COMPOSITE MATERIALS - Peel ply for surface preparation and a method of surface preparation prior to adhesive bonding. A resin-rich peel ply is applied onto a curable, resin-based composite substrate, followed by co-curing. After co-curing, the composite substrate is fully cured but the matrix resin in the peel ply remains partially cured. When the peel ply is removed, a roughened, bondable surface with chemically-active functional groups is revealed. The composite substrate with the chemically-active, bondable surface may be bonded to another composite substrate to form a covalently-bonded structure. | 02-26-2015 |
Patent application number | Description | Published |
20100209690 | CO-CURABLE, CONDUCTIVE SURFACING FILMS FOR LIGHTNING STRIKE AND ELECTROMAGNETIC INTERFERENCE SHIELDING OF THERMOSET COMPOSITE MATERIALS - Embodiments of the present disclosure present electrically conductive, thermosetting compositions for use in surfacing films and adhesives. The surfacing films possess enhanced electrical conductivity, comparable to metals, without the use of embedded metal screens or foils. Such surfacing films may be incorporated into composite structures (e.g., prepregs, tapes, and fabrics), for example, by co-curing, as an outermost surface layer. In particular, compositions formed using silver flakes as conductive fillers are found to exhibit very high electrical conductivity. For example, compositions including greater than 45 wt. % silver flake exhibit resistivities less than about 55 mΩ/sq. In this manner, the surfacing films as an outermost conductive layer may provide lighting strike protection (LSP) and electromagnetic interference (EMI) shielding when used in applications such as aircraft components. | 08-19-2010 |
20100247922 | Water Based Non-Chromated Primers for Structural Bonding Applications - Non-chromated corrosion inhibiting primer formulations having one or more active corrosion inhibitors covalently anchored, or optionally covalently anchored, onto an organic and/or inorganic reactive specie are provided herein. | 09-30-2010 |
20120171477 | METHOD OF FABRICATING A COMPOSITE STRUCTURE WITH A CONDUCTIVE SURFACE - A method of fabricating a composite structure having a conductive surface is disclosed herein. The composite structure is formed by laminating a self-surfacing, conductive prepreg to one or prepreg plies or tapes to form a layup. The self-surfacing, conductive prepreg comprises a conductive surfacing film with a conductivity of less than 20 milliOhms formed on at least one surface of a prepreg ply or tape. Furthermore, the self-surfacing, conductive prepreg is suitable for use in an Automated Fiber Placement (AFP) process. | 07-05-2012 |
20120190773 | COMPOSITE SURFACING FILM WITH ULTRAVIOLET LIGHT AND ABRASION RESISTANCE - The present invention is a one-part ultraviolet light and abrasion resistant pigmented surfacing film composition adapted for co-curing with an amine cured composite prepreg material using a chain extended base cycloaliphatic epoxy resin. The chain extended cycloaliphatic epoxy resin is formed through the pre-reaction of a base cycloaliphatic epoxy resin with a chain extension agent such as bisphenol and a high molecular weight elastomer in the presence of triphenyl phosphine to chain link the base cycloaliphatic epoxy resin to form a film formable cycloaliphatic resin prereact capable of low temperature curing when added to a latent amine based epoxy curing agent; an amine catalyst; at least one filler; at least one pigment; and a flow control agent to form surfacing film composition. The surfacing film composition adapted for co-curing with an amine curable composite from about 180° F. to about 350° F. | 07-26-2012 |
20130101833 | CO-CURABLE, CONDUCTIVE SURFACING FILMS FOR LIGHTNING STRIKE AND ELECTROMAGNETIC INTERFERENCE SHIELDING OF THERMOSET COMPOSITE MATERIALS - Embodiments of the present disclosure present electrically conductive, thermosetting compositions for use in surfacing films and adhesives. The surfacing films possess enhanced electrical conductivity, comparable to metals, without the use of embedded metal screens or foils. Such surfacing films may be incorporated into composite structures (e.g., prepregs, tapes, and fabrics), for example, by co-curing, as an outermost surface layer. In particular, compositions formed using silver flakes as conductive fillers are found to exhibit very high electrical conductivity. For example, compositions including greater than 45 wt. % silver flake exhibit resistivities less than about 55 mΩ/sq. In this manner, the surfacing films as an outermost conductive layer may provide lighting strike protection (LSP) and electromagnetic interference (EMI) shielding when used in applications such as aircraft components. | 04-25-2013 |
20130115442 | STRUCTURAL ADHESIVE AND BONDING APPLICATION THEREOF - A structural adhesive composition that is suitable for high-strength bonding of metals and aerospace structural materials. In one embodiment, the structural adhesive composition based on a two-part system, which is curable at or below 200° F. (93° C.). The two-part system is composed of a resinous part (A) and a catalyst part (B), which may be stored separately at room temperature until they are ready to be used. The resinous part (A) includes at least two different multifunctional epoxy resins, toughening components, and inorganic filler particles. The catalyst part (B) includes an aliphatic or cyclic amine compound as a curing agent and inorganic filler. In another embodiment, the structural adhesive composition is based on a one-part system, which includes the components of the resinous part (A) mixed with a latent amine curing agent. The one-part system may further include an imidazole and/or an aliphatic amine. | 05-09-2013 |
20130129957 | Peel Ply, Method of Surface Preparation and Bonding Composite Structures Using the Same - A resin-rich peel ply that does not leave behind residual fibers after peeling and can work well with different resin-based composite substrates. The resin-rich peel ply is composed of a woven fabric impregnated with a resin matrix different from the resin matrix of the composite substrate. The peel ply is designed such that, upon manual removal of the peel ply from the composite substrate's surface, a thin film of the peel ply resin remains on the composite substrate's surface to create a bondable surface capable of bonding with another composite substrate, but no fibrous material from the woven fabric remains on the same surface. | 05-23-2013 |
20130149934 | Surfacing Film for Composite Structures and Method of Making the Same - A surfacing film is formed from a curable resin composition containing an epoxy novolac resin, a tri-functional or tetra-functional epoxy resin, ceramic microspheres, an amine-based curing agent, particulate inorganic fillers; and a toughening component. The surfacing film exhibits high T | 06-13-2013 |
20140154496 | CONDUCTIVE SURFACING MATERIAL FOR COMPOSITE STRUCTURES - An electrically conductive surfacing material capable of providing sufficient conductivity for lightning strike protection (LSP) and/or electromagnetic interference (EMI) shielding is disclosed. The conductive surfacing material is a multi-layered structure having a very thin conductive layer (e.g. solid metal foil) and a resin film formed on at least one surface of the conductive layer. The resin film is formed from a curable resin composition containing an epoxy novolac resin, a tri-functional or tetra-functional epoxy resin, ceramic microspheres, a latent amine-based curing agent, particulate inorganic fillers; and a toughening component. Optionally, the resin film further includes conductive additives to increase electrical conductivity of the surfacing material. The resin film exhibits high T | 06-05-2014 |
20150030844 | STRUCTURAL ADHESIVE AND BONDING APPLICATION THEREOF - A structural adhesive composition that is suitable for high-strength bonding of metals and aerospace structural materials. In one embodiment, the structural adhesive composition based on a two-part system, which is curable at or below 200° F. (93° C.). The two-part system is composed of a resinous part (A) and a catalyst part (B), which may be stored separately at room temperature until they are ready to be used. The resinous part (A) includes at least two different multifunctional epoxy resins with different functionality selected from difunctional, trifunctional, and tetrafunctional epoxy resins, certain toughening components, and inorganic filler particles as a rheology/thixotrophy modifying component. The toughening components include core-shell rubber particles with different particle sizes and at least one of an elastomeric polymer and a polyethersulfone polymer. The catalyst part (B) includes an aliphatic or cyclic amine compound as a curing agent and inorganic filler as a rheology/thixotropy modifying component. The weight ratio of part (A) to part (B) is within the range of 3:2 to 10:2. In another embodiment, the structural adhesive composition is based on a one-part system which includes the components of the resinous part (A) in the two-part system mixed with a latent amine curing agent. The one-part system may further include an imidazole and/or an aliphatic amine. The one-part system is curable within the temperature range of 140-300° F. (60-150° C.). The paste adhesive disclosed herein has film-like properties and is particularly useful in rapid-assembly aerospace structure bonding applications. | 01-29-2015 |
Patent application number | Description | Published |
20100124519 | Particulate Filter and Method of Making - A particulate filter includes first and second honeycomb substrates. An outlet face of a first substrate is positioned against an inlet face of a second substrate such that channels extending longitudinally through the substrates are aligned to form continuous channels. A continuous skin is joined to each of the substrates to form a unified substrate. A portion of the continuous channels are selectively plugged to form a wall flow filter. | 05-20-2010 |
20110267697 | ANTI-GLARE SURFACE AND METHOD OF MAKING - A glass article including: at least one anti-glare surface having haze, distinctness-of-image, surface roughness, and uniformity properties, as defined herein. A method of making the article having an anti-glare surface includes, for example, forming a protective film on selected portions of at least one surface of the article; contacting the at least one surface with a liquid etchant; and removing the protective film from the surface of the article to form the anti-glare surface. A display system that incorporates the glass article, as defined herein, is also disclosed. | 11-03-2011 |
20110267698 | ANTI-GLARE SURFACE TREATMENT METHOD AND ARTICLES THEREOF - A glass article including: at least one anti-glare surface having haze, distinctness-of-image, surface roughness, and uniformity properties, as defined herein. A method of making the glass article includes, for example, depositing sacrificial particles on a surface of the article; and contacting the resulting particulated surface with an etchant. A display system that incorporates the glass article, as defined herein, is also disclosed. | 11-03-2011 |
20150114041 | METHOD OF MAKING A COVER GLASS - A method of making a strengthened glass article includes providing a flat glass article having a select contour and a glass surface covered by a protective coating layer. The protective coating layer is removed from the glass surface without touching the glass surface with any solid object. Immediately after the protective coating layer is removed from the glass surface, the flat glass article is subjected to an ion-exchange process to strengthen the flat glass article and improve the resistance of the flat glass article to subsequent damage. | 04-30-2015 |
20150160376 | ANTI-GLARE GLASS ARTICLE AND DISPLAY SYSTEM - A glass article including: at least one anti-glare surface having haze, distinctness-of-image, surface roughness, and uniformity properties, as defined herein. A method of making the article having an anti-glare surface includes, for example, forming a protective film on selected portions of at least one surface of the article; contacting the at least one surface with a liquid etchant; and removing the protective film from the surface of the article to form the anti-glare surface. A display system that incorporates the glass article, as defined herein, is also disclosed. | 06-11-2015 |
20150368149 | TRANSITION METAL-CONTAINING, ION EXCHANGEABLE COLORED GLASSES - Glasses that can be chemically strengthened and are colored by transition metals. Most of the glasses are black, with some having high damage resistance and compressive surface layers having high compressive stress and depth of layer after ion exchange. These colored glasses do not require a post-forming heat treatment to produce color and are formable by fusions drawing, rolling, slot drawing, and float glass processes. | 12-24-2015 |
Patent application number | Description | Published |
20110287002 | ANTIBODIES AGAINST EPIDERMAL GROWTH FACTOR RECEPTOR (EGFR) AND USES THEREOF - Anti-EGFR antibodies, therapeutic compositions comprising combinations of anti-EGFR antibodies, as well as methods for using such antibodies and compositions to treat EGFR-related disorders (e.g., cancers), are disclosed. | 11-24-2011 |
20120244163 | BISPECIFIC BINDING AGENTS TARGETING IGF-1R AND ERBB3 SIGNALLING AND USES THEREOF - Disclosed are bispecific binding agents that specifically target both of the IGF-1 and the ErbB intracellular signaling pathways. For example, bispecific binding agents that comprise an anti-IGF-1R antibody and an anti-ErbB3 antibody connected by a linker are described herein. These bispecific agents are capable of antagonizing signal transduction by both of the IGF-1 and the ErbB signaling pathways and are useful in inhibiting the proliferation of tumor cells whose growth involves the signaling activity of both pathways. | 09-27-2012 |
20120269812 | MONOSPECIFIC AND BISPECIFIC ANTI-IGF-1R AND ANTI-ERBB3 ANTIBODIES - Provided herein are novel monospecific and bispecific antibodies that are useful as anti-neoplastic agents and that bind specifically to human IGF-1R and human ErbB3. Exemplary antibodies inhibit signal transduction through either or both of IGF-1R and ErbB3. Exemplary polyvalent proteins comprise at least one anti-IGF-1R binding site and at least one anti-ErbB3 binding site. In certain embodiments the binding sites may be linked through an immunoglobulin constant region. Novel antiErbB3 and anti-IGF-1R antibodies (e.g., monoclonal antibodies) are also provided. | 10-25-2012 |
20130236459 | MONOSPECIFIC AND BISPECIFIC ANTI-IGF-1R AND ANTI-ERBB3 ANTIBODIES - Provided are monospecific and bispecific antibodies that are useful as anti-neoplastic agents and that bind specifically to human IGF-1R and human ErbB3. Exemplary antibodies inhibit signal transduction through either or both of IGF-1R and ErbB3. Exemplary polyvalent proteins comprise at least one anti-IGF-1R binding site and at least one anti-ErbB3 binding site. In certain embodiments the binding sites may be linked through an immunoglobulin constant region. AntiErbB3 and anti-IGF-1R antibodies (e.g., monoclonal antibodies) are also provided. | 09-12-2013 |
20140127207 | ANTIBODIES AGAINST EPIDERMAL GROWTH FACTOR RECEPTOR (EGFR) AND USES THEREOF - Anti-EGFR antibodies, therapeutic compositions comprising combinations of anti-EGFR antibodies, as well as methods for using such antibodies and compositions to treat EGFR-related disorders (e.g., cancers), are disclosed. | 05-08-2014 |
20140234314 | ANTIBODIES AGAINST EPIDERMAL GROWTH FACTOR RECEPTOR (EGFR) AND USES THEREOF - Anti-EGFR antibodies, therapeutic compositions comprising combinations of anti-EGFR antibodies, as well as methods for using such antibodies and compositions to treat EGFR-related disorders (e.g., cancers), are disclosed. | 08-21-2014 |
20140294834 | TANDEM FC BISPECIFIC ANTIBODIES - Provided herein are tandem Fcs and tandem Fc antibodies (“TFcAs”), e.g., tandem Fc bispecific antibodies (“TFcBAs”), which comprise one or at least two binding sites that specifically bind to one or more cell surface receptors. The binding sites are connected through a TFc, which TFc comprises a first Fc region and a second Fc region, wherein the first and the second Fc regions are linked through a TFc linker to form a contiguous polypeptide and dimerize to form an Fc dimer. Exemplary TFcBAs inhibit signal transduction through the cell surface receptor(s) for which the binding sites of the TFcBA are specific. | 10-02-2014 |
20140302035 | ANTI-C-MET Tandem Fc Bispecific Antibodies - Provided herein are tandem Fcs and tandem Fc antibodies (“TFcAs”), e.g., tandem Fc bispecific antibodies (“TFcBAs”), which comprise one or at least two binding sites that specifically bind to one or more cell surface receptors. The binding sites are connected through a TFc, which TFc comprises a first Fc region and a second Fc region, wherein the first and the second Fc regions are linked through a TFc linker to form a contiguous polypeptide and dimerize to form an Fc dimer. Exemplary TFcBAs bind to the cell surface receptors c-Met and EpCam and inhibit signal transduction through the cell surface receptor(s) for which the binding sites of the TFcBA are specific. | 10-09-2014 |
20150368346 | ANTIBODIES AGAINST EPIDERMAL GROWTH FACTOR RECEPTOR (EGFR) AND USES THEREOF - Anti-EGFR antibodies, therapeutic compositions comprising combinations of anti-EGFR antibodies, as well as methods for using such antibodies and compositions to treat EGFR-related disorders (e.g., cancers), are disclosed. | 12-24-2015 |
20150368347 | ANTIBODIES AGAINST EPIDERMAL GROWTH FACTOR RECEPTOR (EGFR) AND USES THEREOF - Anti-EGFR antibodies, therapeutic compositions comprising combinations of anti-EGFR antibodies, as well as methods for using such antibodies and compositions to treat EGFR-related disorders (e.g., cancers), are disclosed. | 12-24-2015 |
20150368361 | ANTIBODIES AGAINST EPIDERMAL GROWTH FACTOR RECEPTOR (EGFR) AND USES THEREOF - Anti-EGFR antibodies, therapeutic compositions comprising combinations of anti-EGFR antibodies, as well as methods for using such antibodies and compositions to treat EGFR-related disorders (e.g., cancers), are disclosed. | 12-24-2015 |
20150376284 | ANTIBODIES AGAINST EPIDERMAL GROWTH FACTOR RECEPTOR (EGFR) AND USES THEREOF - Anti-EGFR antibodies, therapeutic compositions comprising combinations of anti-EGFR antibodies, as well as methods for using such antibodies and compositions to treat EGFR-related disorders (e.g., cancers), are disclosed. | 12-31-2015 |
20160002339 | ANTIBODIES AGAINST EPIDERMAL GROWTH FACTOR RECEPTOR (EGFR) AND USES THEREOF - Anti-EGFR antibodies, therapeutic compositions comprising combinations of anti-EGFR antibodies, as well as methods for using such antibodies and compositions to treat EGFR-related disorders (e.g., cancers), are disclosed. | 01-07-2016 |
Patent application number | Description | Published |
20140107865 | SYSTEM, APPARATUS, AND METHOD FOR ACTIVE DEBRIS REMOVAL - Systems, apparatuses, and methods for removal of orbital debris are provided. In one embodiment, an apparatus includes a spacecraft control unit configured to guide and navigate the apparatus to a target. The apparatus also includes a dynamic object characterization unit configured to characterize movement, and a capture feature, of the target. The apparatus further includes a capture and release unit configured to capture a target and deorbit or release the target. The collection of these apparatuses is then employed as multiple, independent and individually operated vehicles launched from a single launch vehicle for the purpose of disposing of multiple debris objects. | 04-17-2014 |
20160023783 | SYSTEM, APPARATUS, AND METHOD FOR ACTIVE DEBRIS REMOVAL - Systems, apparatuses, and methods for removal of orbital debris are provided. In one embodiment, an apparatus includes a spacecraft control unit configured to guide and navigate the apparatus to a target. The apparatus also includes a dynamic object characterization unit configured to characterize movement, and a capture feature, of the target. The apparatus further includes a capture and release unit configured to capture a target and deorbit or release the target. The collection of these apparatuses is then employed as multiple, independent and individually operated vehicles launched from a single launch vehicle for the purpose of disposing of multiple debris objects. | 01-28-2016 |