Patent application number | Description | Published |
20090206196 | INFLATABLE FOLDING WINGS FOR A VERY HIGH ALTITUDE AIRCRAFT - A foldable wing for use with a very high altitude aircraft capable of operating at an altitude at or above 85,000 feet is disclosed. The foldable wing may employ a spiral fold deployment, wherein a hinge between each segment of the foldable wing is slightly offset from the perpendicular. Successively positioned wing segments fold over one another. Alternatively, the hinges are substantially perpendicular so that each respective wing segment folds linearly against the next wing segment. An inflatable rib, with inflatable arms, can be inflated to provide a force against two adjacent arms, thereby deploying the wing segments through a full 180° of rotation. | 08-20-2009 |
20100237183 | SYSTEM AND METHOD FOR THE RETRIEVAL OF A SMALLER UNMANNED AERIAL VEHICLE BY A LARGER UNMANNED AERIAL VEHICLE - A system and method are provided for using a first aircraft to retrieve a second aircraft. The first aircraft is typically larger than the second aircraft. A minimum airspeed of the first aircraft is typically greater than a maximum airspeed of the second aircraft. The first aircraft flies in a substantially circular pattern and extends a tow line, such that the tow line forms a substantially helical shape behind and below the first aircraft. Due to the helical shape, there is at least one point along the extended tow line at which the speed of the tow line is substantially equal to the speed of the second aircraft. The second aircraft can readily latch onto the tow line at that point, thereby minimizing potential damage otherwise caused by differential airspeeds. | 09-23-2010 |
20110057074 | MODULAR MINIATURE UNMANNED AIRCRAFT WITH VECTORED THRUST CONTROL - An aircraft for unmanned aviation is described. The aircraft includes an airframe, a pair of fins attached to a rear portion of the airframe, a pair of dihedral braces attached to a bottom portion of the airframe, a first thrust vectoring module and a second thrust vectoring module, and an electronics module. The electronics module provides commands to the two thrust vectoring modules. The two thrust vectoring modules are configured to provide lateral and longitudinal control to the aircraft by directly controlling a thrust vector for each of the pitch, the roll, and the yaw of the aircraft. The use of directly articulated electrical motors as thrust vectoring modules enables the aircraft to execute tight-radius turns over a wide range of airspeeds. | 03-10-2011 |
20130068880 | INFLATABLE FOLDING WINGS FOR A VERY HIGH ALTITUDE AIRCRAFT - A foldable wing for use with a very high altitude aircraft capable of operating at an altitude at or above 85,000 feet is disclosed. The foldable wing may employ a spiral fold deployment, wherein a hinge between each segment of the foldable wing is slightly offset from the perpendicular. Successively positioned wing segments fold over one another. Alternatively, the hinges are substantially perpendicular so that each respective wing segment folds linearly against the next wing segment. An inflatable rib, with inflatable arms, can be inflated to provide a force against two adjacent arms, thereby deploying the wing segments through a full 180° of rotation. | 03-21-2013 |
20130175390 | MODULAR MINIATURE UNMANNED AIRCRAFT WITH VECTORED-THRUST CONTROL - An aircraft for unmanned aviation is described. The aircraft includes an airframe, a pair of fins attached to a rear portion of the airframe, a pair of dihedral braces attached to a bottom portion of the airframe, a first thrust-vectoring (“T/V”) module and a second T/V module, and an electronics module. The electronics module provides commands to the two T/V modules. The two T/V modules are configured to provide lateral and longitudinal control to the aircraft by directly controlling a thrust vector for each of the pitch, the roll, and the yaw of the aircraft. The use of directly articulated electrical motors as T/V modules enables the aircraft to execute tight-radius turns over a wide range of airspeeds. | 07-11-2013 |
20130233964 | TETHERED AERIAL SYSTEM FOR DATA GATHERING - A tethered unmanned aerial vehicle (“UAV”) may be outfitted with a sensor payload for data gathering. The tethered UAV may be tethered to a ground station for constricting the flight space of the UAV while also providing the option for power delivery and/or bidirectional communications. The tethered UAV's flight path may be extended by introducing one or more secondary UAVs that cooperate to extend the horizontal flight path of a primary UAV. The ground station, which may be coupled with the tethered aerial vehicle, may comprise a listening switch configured to determine a condition of the tether such that the supply of power to the tether may be terminated when tether damage or a tether severance is detected. | 09-12-2013 |
20140026802 | COMBINED SUBMERSIBLE VESSEL AND UNMANNED AERIAL VEHICLE - A combined submersible vessel and unmanned aerial vehicle preferably includes a body structure, at least one wing structure, at least one vertical stabilizer structure, and at least one horizontal stabilizer structure. A propulsion system is coupled to the body structure and is configured to propel the flying submarine in both airborne flight and underwater operation. Preferably, the propulsion system includes a motor, a gearbox coupled to the motor and configured to receive power generated by the motor and provide variable output power, a drive shaft coupled to the gearbox and configured to transfer the variable output power provided by the gearbox, and a propeller coupled to the drive shaft and configured to accept power transferred to it from the drive shaft. The propeller is further configured to rotate and propel the flying submarine in both an airborne environment and in an underwater environment. | 01-30-2014 |
20150021430 | SYSTEM, APPARATUS AND METHOD FOR LONG ENDURANCE VERTICAL TAKEOFF AND LANDING VEHICLE - A vertical take-off and landing (VTOL) aircraft according to an aspect of the present invention comprises a fuselage, an empennage having an all-moving horizontal stabilizer located at a tail end of the fuselage, a wing having the fuselage positioned approximately halfway between the distal ends of the wing, wherein the wing is configured to transform between a substantially straight wing configuration and a canted wing configuration using a canted hinge located on each side of the fuselage. The VTOL aircraft may further includes one or more retractable pogo supports, wherein a retractable pogo support is configured to deploy from each of the wing's distal ends. | 01-22-2015 |
20150336663 | SYSTEM, APPARATUS AND METHOD FOR LONG ENDURANCE VERTICAL TAKEOFF AND LANDING VEHICLE - A vertical take-off and landing (VTOL) aircraft according to an aspect of the present invention comprises a fuselage, an empennage having an all-moving horizontal stabilizer located at a tail end of the fuselage, a wing having the fuselage positioned approximately halfway between the distal ends of the wing, wherein the wing is configured to transform between a substantially straight wing configuration and a canted wing configuration using a canted hinge located on each side of the fuselage. The VTOL aircraft may further includes one or more retractable pogo supports, wherein a retractable pogo support is configured to deploy from each of the wing's distal ends. | 11-26-2015 |
20150336666 | SYSTEM, APPARATUS AND METHOD FOR LONG ENDURANCE VERTICAL TAKEOFF AND LANDING VEHICLE - A vertical take-off and landing (VTOL) aircraft according to an aspect of the present invention comprises a fuselage, an empennage having an all-moving horizontal stabilizer located at a tail end of the fuselage, a wing having the fuselage positioned approximately halfway between the distal ends of the wing, wherein the wing is configured to transform between a substantially straight wing configuration and a canted wing configuration using a canted hinge located on each side of the fuselage. The VTOL aircraft may further includes one or more retractable pogo supports, wherein a retractable pogo support is configured to deploy from each of the wing's distal ends. | 11-26-2015 |
20150375586 | COMBINED SUBMERSIBLE VESSEL AND UNMANNED AERIAL VEHICLE - A combined submersible vessel and unmanned aerial vehicle preferably includes a body structure, at least one wing structure, at least one vertical stabilizer structure, and at least one horizontal stabilizer structure. A propulsion system is coupled to the body structure and is configured to propel the flying submarine in both airborne flight and underwater operation. Preferably, the propulsion system includes a motor, a gearbox coupled to the motor and configured to receive power generated by the motor and provide variable output power, a drive shaft coupled to the gearbox and configured to transfer the variable output power provided by the gearbox, and a propeller coupled to the drive shaft and configured to accept power transferred to it from the drive shaft. The propeller is further configured to rotate and propel the flying submarine in both an airborne environment and in an underwater environment. | 12-31-2015 |
Patent application number | Description | Published |
20090127376 | WING TIP DOCKING SYSTEM FOR AIRCRAFT - A system and method for docking various types of aircraft is disclosed. An aerodynamic lifting structure docking mechanism for docking two or more aircraft is provided comprising an aerodynamic lifting structure. The aerodynamic lifting structure includes a first and second airflow adjustment mechanism. The aerodynamic lifting structure further includes a first hard docking mechanism, and a second hard docking mechanism, and still further includes a soft docking mechanism. The first and second airflow adjustment mechanisms are configured to substantially remove any aerodynamic lifting structure vortices around each of the aerodynamic lifting structure tip areas. The soft docking mechanism is configured to soft dock a first aerodynamic lifting structure with a second aerodynamic lifting structure. The first hard docking mechanism is configured to hard dock with the second hard docking mechanism, thereby temporarily attaching the first aerodynamic lifting structure with the second aerodynamic lifting structure. | 05-21-2009 |
20120061505 | WING TIP DOCKING SYSTEM FOR AIRCRAFT - A system and method for docking various types of aircraft is disclosed. An aerodynamic lifting structure docking mechanism for docking two or more aircraft is provided comprising an aerodynamic lifting structure. The aerodynamic lifting structure includes a first and second airflow adjustment mechanism. The aerodynamic lifting structure further includes a first hard docking mechanism, and a second hard docking mechanism, and still further includes a soft docking mechanism. The first and second airflow adjustment mechanisms are configured to substantially remove any aerodynamic lifting structure vortices around each of the aerodynamic lifting structure tip areas. The soft docking mechanism is configured to soft dock a first aerodynamic lifting structure with a second aerodynamic lifting structure. The first hard docking mechanism is configured to hard dock with the second hard docking mechanism, thereby temporarily attaching the first aerodynamic lifting structure with the second aerodynamic lifting structure. | 03-15-2012 |
20120061506 | WING TIP DOCKING SYSTEM FOR AIRCRAFT - A system and method for docking various types of aircraft is disclosed. An aerodynamic lifting structure docking mechanism for docking two or more aircraft is provided comprising an aerodynamic lifting structure. The aerodynamic lifting structure includes a first and second airflow adjustment mechanism. The aerodynamic lifting structure further includes a first hard docking mechanism, and a second hard docking mechanism, and still further includes a soft docking mechanism. The first and second airflow adjustment mechanisms are configured to substantially remove any aerodynamic lifting structure vortices around each of the aerodynamic lifting structure tip areas. The soft docking mechanism is configured to soft dock a first aerodynamic lifting structure with a second aerodynamic lifting structure. The first hard docking mechanism is configured to hard dock with the second hard docking mechanism, thereby temporarily attaching the first aerodynamic lifting structure with the second aerodynamic lifting structure. | 03-15-2012 |
Patent application number | Description | Published |
20140054423 | MODULAR MINIATURE UNMANNED AIRCRAFT WITH VECTORED-THRUST CONTROL - An aircraft for unmanned aviation is described. The aircraft includes an airframe, a pair of fins attached to a rear portion of the airframe, a pair of dihedral braces attached to a bottom portion of the airframe, a first thrust-vectoring (“T/V”) module and a second T/V module, and an electronics module. The electronics module provides commands to the two T/V modules. The two T/V modules are configured to provide lateral and longitudinal control to the aircraft by directly controlling a thrust vector for each of the pitch, the roll, and the yaw of the aircraft. The use of directly articulated electrical motors as T/V modules enables the aircraft to execute tight-radius turns over a wide range of airspeeds. | 02-27-2014 |
20140061384 | MODULAR MINIATURE UNMANNED AIRCRAFT WITH VECTORED-THRUST CONTROL - An aircraft for unmanned aviation is described. The aircraft includes an airframe, a pair of fins attached to a rear portion of the airframe, a pair of dihedral braces attached to a bottom portion of the airframe, a first thrust-vectoring (“T/V”) module and a second T/V module, and an electronics module. The electronics module provides commands to the two T/V modules. The two T/V modules are configured to provide lateral and longitudinal control to the aircraft by directly controlling a thrust vector for each of the pitch, the roll, and the yaw of the aircraft. The use of directly articulated electrical motors as T/V modules enables the aircraft to execute tight-radius turns over a wide range of airspeeds. | 03-06-2014 |
20140061390 | MODULAR MINIATURE UNMANNED AIRCRAFT WITH VECTORED-THRUST CONTROL - An aircraft for unmanned aviation is described. The aircraft includes an airframe, a pair of fins attached to a rear portion of the airframe, a pair of dihedral braces attached to a bottom portion of the airframe, a first thrust-vectoring (“T/V”) module and a second T/V module, and an electronics module. The electronics module provides commands to the two T/V modules. The two T/V modules are configured to provide lateral and longitudinal control to the aircraft by directly controlling a thrust vector for each of the pitch, the roll, and the yaw of the aircraft. The use of directly articulated electrical motors as T/V modules enables the aircraft to execute tight-radius turns over a wide range of airspeeds. | 03-06-2014 |
Patent application number | Description | Published |
20090254841 | APPARATUS, METHOD, AND COMPUTER PROGRAM PRODUCT FOR CHARACTERIZING USER-DEFINED AREAS - A method of specifying a boundary for an area is provided, which includes receiving a first input from a first user regarding a first configuration of a boundary of an area. The first input may serve to establish an area of arbitrary and possibly irregular configuration, such as an area that is apolitical or otherwise legally undetermined. A second input may be received from a second user regarding a second boundary configuration. The second input may serve to modify the boundary of an area established by the first input. A particular configuration of the boundary based at least partially on the first and second inputs can then be determined. For example, the particular configuration of the boundary may be determined, in part, by spatially averaging the first and second configurations. In some embodiments, demographic data for an area defined by the particular configuration of the boundary may be compiled. | 10-08-2009 |
20090265285 | APPARATUS, METHOD, AND COMPUTER PROGRAM PRODUCT FOR CHARACTERIZING USER-DEFINED AREAS - A method of specifying a boundary for an area is provided, which includes receiving a first input from a first user regarding a first configuration of a boundary of an area. The first input may serve to establish an area of arbitrary and possibly irregular configuration, such as an area that is apolitical or otherwise legally undetermined. A second input may be received from a second user regarding a second boundary configuration. The second input may serve to modify the boundary of an area established by the first input. A particular configuration of the boundary based at least partially on the first and second inputs can then be determined. For example, the particular configuration of the boundary may be determined, in part, by spatially averaging the first and second configurations. In some embodiments, demographic data for an area defined by the particular configuration of the boundary may be compiled. | 10-22-2009 |
20090265323 | APPARATUS, METHOD, AND COMPUTER PROGRAM PRODUCT FOR CHARACTERIZING USER-DEFINED AREAS - A method of specifying a boundary for an area is provided, which includes receiving a first input from a first user regarding a first configuration of a boundary of an area. The first input may serve to establish an area of arbitrary and possibly irregular configuration, such as an area that is apolitical or otherwise legally undetermined. A second input may be received from a second user regarding a second boundary configuration. The second input may serve to modify the boundary of an area established by the first input. A particular configuration of the boundary based at least partially on the first and second inputs can then be determined. For example, the particular configuration of the boundary may be determined, in part, by spatially averaging the first and second configurations. In some embodiments, demographic data for an area defined by the particular configuration of the boundary may be compiled. | 10-22-2009 |
20090265452 | APPARATUS, METHOD, AND COMPUTER PROGRAM PRODUCT FOR CHARACTERIZING USER-DEFINED AREAS - A method of specifying a boundary for an area is provided, which includes receiving a first input from a first user regarding a first configuration of a boundary of an area. The first input may serve to establish an area of arbitrary and possibly irregular configuration, such as an area that is apolitical or otherwise legally undetermined. A second input may be received from a second user regarding a second boundary configuration. The second input may serve to modify the boundary of an area established by the first input. A particular configuration of the boundary based at least partially on the first and second inputs can then be determined. For example, the particular configuration of the boundary may be determined, in part, by spatially averaging the first and second configurations. In some embodiments, demographic data for an area defined by the particular configuration of the boundary may be compiled. | 10-22-2009 |
20090271718 | APPARATUS, METHOD, AND COMPUTER PROGRAM PRODUCT FOR CHARACTERIZING USER-DEFINED AREAS - A method of specifying a boundary for an area is provided, which includes receiving a first input from a first user regarding a first configuration of a boundary of an area. The first input may serve to establish an area of arbitrary and possibly irregular configuration, such as an area that is apolitical or otherwise legally undetermined. A second input may be received from a second user regarding a second boundary configuration. The second input may serve to modify the boundary of an area established by the first input. A particular configuration of the boundary based at least partially on the first and second inputs can then be determined. For example, the particular configuration of the boundary may be determined, in part, by spatially averaging the first and second configurations. In some embodiments, demographic data for an area defined by the particular configuration of the boundary may be compiled. | 10-29-2009 |
Patent application number | Description | Published |
20090155579 | ELECTROSTATIC COATINGS AND ARTICLES COMPRISING POLYTHIOPHENES - Electrostatic dissipation coatings based on regioregular polythiophenes including blends and block copolymers. The compositions can be soluble in organic solvents. Excellent film formation, transparency, stability, and conductivity control can be achieved. | 06-18-2009 |
20120001127 | HOLE TRANSPORT COMPOSITIONS AND RELATED DEVICES AND METHODS (I) - A composition comprising: at least one compound comprising a hole transporting core, wherein the core is covalently bonded to a first arylamine group and also covalently bonded to a second arylamine group different from the first, and wherein the compound is covalently bonded to at least one intractability group, wherein the intractability group is covalently bonded to the hole transporting core, the first arylamine group, the second arylamine group, or a combination thereof, and wherein the compound has a molecular weight of about 5,000 g/mole or less. Blended mixtures of arylamine compounds, including fluorene core compounds, can provide good film formation and stability when coated onto hole injection layers. Solution processing of OLEDs is a particularly important application. | 01-05-2012 |
20120003790 | HOLE TRANSPORT COMPOSITIONS AND RELATED DEVICES AMD METHODS (II) - A composition comprising: at least one compound comprising a hole transporting core, wherein the core is covalently bonded to a first arylamine group and also covalently bonded to a second arylamine group different from the first, and wherein the compound is covalently bonded to at least one intractability group, wherein the intractability group is covalently bonded to the hole transporting core, the first arylamine group, the second arylamine group, or a combination thereof, and wherein the compound has a molecular weight of about 5,000 g/mole or less. Blended mixtures of arylamine compounds, including fluorene core compounds, can provide good film formation and stability when coated onto hole injection layers. Solution processing of OLEDs is a particularly important application. | 01-05-2012 |
20130344648 | HOLE TRANSPORT COMPOSITIONS AND RELATED DEVICES AND METHODS (II) - A composition comprising: at least one compound comprising a hole transporting core, wherein the core is covalently bonded to a first arylamine group and also covalently bonded to a second arylamine group different from the first, and wherein the compound is covalently bonded to at least one intractability group, wherein the intractability group is covalently bonded to the hole transporting core, the first arylamine group, the second arylamine group, or a combination thereof, and wherein the compound has a molecular weight of about 5,000 g/mole or less. Blended mixtures of arylamine compounds, including fluorene core compounds, can provide good film formation and stability when coated onto hole injection layers. Solution processing of OLEDs is a particularly important application. | 12-26-2013 |
20140054509 | SULFONATION OF CONDUCTING POLYMERS AND OLED, PHOTOVOLTAIC, AND ESD DEVICES - Conducting polymer systems for hole injection or transport layer applications including a composition comprising: a water soluble or water dispersible regioregular polythiophene comprising (i) at least one organic substituent, and (ii) at least one sulfonate substituent comprising sulfonate sulfur bonding directly to the polythiophene backbone. The polythiophene can be water soluble, water dispersible, or water swellable. They can be self-doped. The organic substituent can be an alkoxy substituent, or an alkyl substituent. OLED, PLED, SMOLED, PV, and ESD applications can be used. | 02-27-2014 |
Patent application number | Description | Published |
20080248313 | Sulfonation of conducting polymers and OLED, photovoltaic, and ESD devices - Conducting polymer systems for hole injection or transport layer applications including a composition comprising: a water soluble or water dispersible regioregular polythiophene comprising (i) at least one organic substituent, and (ii) at least one sulfonate substituent comprising sulfonate sulfur bonding directly to the polythiophene backbone. The polythiophene can be water soluble, water dispersible, or water swellable. They can be self-doped. The organic substituent can be an alkoxy substituent, or an alkyl substituent. OLED, PLED, SMOLED, PV, and ESD applications can be used. | 10-09-2008 |
20090230361 | MODIFIED PLANARIZNG AGENTS AND DEVICES - A composition comprising: at least one conjugated polymer, at least one second polymer comprising repeat units represented by: (I) optionally, —[CH | 09-17-2009 |
20100043876 | SOLVENT SYSTEM - Improved organic photovoltaic cells including a composition useful for forming an active layer which comprises (a) at least one p-type material, (b) at least one n-type material, (c) at least one first solvent and (d) at least one second solvent, wherein the first solvent is different from the second solvent, and the first solvent comprises at least one alkylbenzene or benzocyclohexane, and the second solvent comprises at least one carbocyclic compound. The second solvent can be used in lesser amounts but can improve efficiency in cells. | 02-25-2010 |
20100174032 | Barrier Coating Comprising a Polyurethane Dispersion and Elastomeric Material - A barrier coating comprising a polyurethane dispersion and an elastomeric material is disclosed. The polyurethane comprises at least 30 weight percent of meta-substituted aromatic material. Methods for improving barrier using the coatings are also disclosed. | 07-08-2010 |
20110095275 | ORGANIC ELECTRONIC DEVICES, COMPOSITIONS, AND METHODS - Organic electronic devices, compositions, and methods are disclosed that employ electrically conductive nanowires and conducting materials such as conjugated polymers such as sulfonated regioregular polythiophenes which provide high device performance such as good solar cell efficiency. Devices requiring transparent conductors that are resilient to physical stresses can be fabricated, with reduced corrosion problems. | 04-28-2011 |
20120037852 | SULFONATION OF CONDUCTING POLYMERS AND OLED, PHOTOVOLTAIC, AND ESD DEVICES - Conducting polymer systems for hole injection or transport layer applications including a composition comprising: a water soluble or water dispersible regioregular polythiophene comprising (i) at least one organic substituent, and (ii) at least one sulfonate substituent comprising sulfonate sulfur bonding directly to the polythiophene backbone. The polythiophene can be water soluble, water dispersible, or water swellable. They can be self-doped. The organic substituent can be an alkoxy substituent, or an alkyl substituent. OLED, PLED, SMOLED, PV, and ESD applications can be used. | 02-16-2012 |
20130320313 | ORGANIC ELECTRONIC DEVICES, COMPOSITIONS, AND METHODS - Organic electronic devices, compositions, and methods are disclosed that employ electrically conductive nanowires and conducting materials such as conjugated polymers such as sulfonated regioregular polythiophenes which provide high device performance such as good solar cell efficiency. Devices requiring transparent conductors that are resilient to physical stresses can be fabricated, with reduced corrosion problems. | 12-05-2013 |
20140323637 | MODIFIED PLANARIZNG AGENTS AND DEVICES - A composition comprising: at least one conjugated polymer, at least one second polymer comprising repeat units represented by: (I) optionally, —[CH | 10-30-2014 |
20150159030 | GRAPHENIC CARBON PARTICLE DISPERSIONS AND METHODS OF MAKING SAME - Dispersions of graphenic carbon particles are produced using a polymeric dispersant. The polymeric dispersant includes an anchor block comprising glycidyl (meth)acrylate, 3,4-epoxycyclohexylmethyl(meth)acrylate, 2-(3,4-epoxycyclohexyl)ethyl(meth)acrylate, allyl glycidyl ether and mixtures thereof, reacted with a carboxylic acid comprising 3-hydroxy-2-naphthoic acid, para-nitrobenzoic acid, hexanoic acid, 2-ethyl hexanoic acid, decanoic acid and/or undecanoic acid. The polymeric dispersant also includes at least one tail block comprising at least one (meth)acrylic acid alkyl ester. | 06-11-2015 |
Patent application number | Description | Published |
20140143049 | SYSTEMS AND METHODS FOR AN INTEGRATED AND FRICTIONLESS CALL TRACKING SERVICE - The field of the invention relates to systems and methods for operation of a call tracking service, and more particularly to systems and methods that provide a call tracking service that does not require landing pages operated by the advertisers and still provide granular visibility into the actual ad impressions. In a preferred embodiment, the system includes a call tracking server system, a webserver, an advertiser system coupled to a public network and accessible to one or more users. The call tracking server system includes a database that stores user profile data associated with the one or more users. The system is configured to provide one or more URLs that replace one or more URLs supported by the advertiser system, create a user profile storing data received from and related to the user and the device operated by the user, provide a tracking number, acting as an identifier, for display at a device operated by a user, forward call from the user to the advertiser system, and update the user profile with information relating to the call. | 05-22-2014 |
20150120438 | SYSTEMS AND METHODS FOR AN INTEGRATED AND FRICTIONLESS CALL TRACKING SERVICE - The field of the invention relates to systems and methods for operation of a call tracking service, and more particularly to systems and methods that provide a call tracking service that does not require landing pages operated by the advertisers and still provide granular visibility into the actual ad impressions. In a preferred embodiment, the system includes a call tracking server system, a webserver, an advertiser system coupled to a public network and accessible to one or more users. The call tracking server system includes a database that stores user profile data associated with the one or more users. The system is configured to provide one or more URLs that replace one or more URLs supported by the advertiser system, create a user profile storing data received from and related to the user and the device operated by the user, provide a tracking number, acting as an identifier, for display at a device operated by a user, forward call from the user to the advertiser system, and update the user profile with information relating to the call. | 04-30-2015 |
Patent application number | Description | Published |
20100259037 | Method and Apparatus for Superposed Application of Shipping Labels over Packing Slips - The invention provides a method and apparatus for applying shipping labels over both folded or non-folded packing slips, or the like, at a single print-and-apply station, either through use of a label configured for application to a substrate and also in a superposed registered manner to another label of identical construction previously attached to the substrate, or by using a shipping label having a non-aggressive adhesive applied to a removable center section of the shipping label for attachment of the packing list, or the like, to the shipping label prior to application of the shipping label to the substrate. | 10-14-2010 |
20140283988 | Method and Apparatus for Superposed Application of Shipping Labels over Packing Slips - A process for automating placement of a shipping label onto a carton on a conveyor system includes moving a carton on the conveyor system to the induction scanner, electronically scanning the carton to obtain identification information from a bar code associated with the carton, accessing electronic shipping information corresponding to the identification information, and transmitting the shipping information to a controller coupled to the conveyor system. The process also includes printing indicia, corresponding the identification information, onto the shipping label and a packing slip at the print-and-apply station, mechanically coupling the packing slip to a non-aggressive adhesive on the shipping label, and mechanically applying the shipping label and attached packing slip to the carton, such that the shipping label covers the packing slip and the packing slip is exposed when a portion of the shipping label is removed along a line of weakness in the shipping label. | 09-25-2014 |