Patent application number | Description | Published |
20110154684 | METHOD AND APPARATUS FOR THE MANUFACTURE OF TORREFIED LIGNOCELLULOSIC MATERIAL - The present invention relates to a method and an apparatus for the manufacture of torreficated lignocellulosic material. Finely divided lignocellulosic material is exposed in running order for drying, heating to at least 200° C. in the absence of oxygen (the torrefication process itself) and cooling to a temperature preferably being below 130° C. The drying device ( | 06-30-2011 |
20140173929 | Method for Cooling and Increasing Yield of a Torrefied Product - The invention relates to a method and a system for cooling torrefied material, including, applying water to the torrefied material to quench-cool the material and thereafter further cooling the torrefied material and at least part of the torrefaction gases released from the material in a common cooling device, such that components of the torrefaction gases condenses on the torrefied material within the common cooling device. | 06-26-2014 |
20140208995 | COUNTERCURRENT OXYGEN ENHANCED TORREFACTION - The invention relates to a method of torrefaction of an optionally predried biomass in a torrefaction reactor such that torrefied biomass and torrefaction gases are obtained, and wherein an oxygen-containing gas is supplied to the torrefaction reactor at a first position in the reactor such that oxygen reacts with components of the torrefaction gases under the formation of heat and wherein torrefaction gases are withdrawn from the torrefaction reactor at a second position of the torrefaction reactor and wherein the first position is located downstream of the second position in relation to a biomass transport direction in the torrefaction reactor such that the torrefaction gases moves through the torrefaction reactor countercurrent with the biomass transport and wherein the optionally predried biomass has a temperature of between 30° C. and 230° C., preferably between 50° C. and 200° C., most preferably between 60° C. and 180° C. when entering the torrefaction rector. | 07-31-2014 |
20140325900 | METHOD AND AN ARRANGEMENT FOR EFFICIENT TORREFACTION OF BIOMASS - The invention relates to a method and a system for efficient torrefaction of a biomass. Said system comprises a first zone for heating of an optionally pre-dried biomass and an insulated second zone for torrefying the heated biomass. The second zone has an inlet being connected to an outlet of the first zone and means for withdrawing torrefied biomass arranged at the bottom of the second zone, such that the biomass can move downwards through the second zone by means of gravity. Means for heating are arranged at the first zone, but not at the second zone. | 11-06-2014 |
20150107499 | Method of Torrefacation of a Biomass Comprising the Step of Cooling the Torrefaction - The invention relates to a method and an arrangement for torrefaction of a biomass. Said method and arrangements allows for precise control of torrefaction temperature, which is crucial for accurate control of the quality and properties of the torrefied material. The method comprising a step of cooling the torrefaction reaction so as to at least partly counteract a temperature increase derived from the exothermic torrefaction reactions | 04-23-2015 |
Patent application number | Description | Published |
20110170404 | MOBILE COMMUNICATION NETWORK - The present invention provides a method of operating a first node in a radio communication network to reduce un-expected or undesirable operation of user equipments, the method comprising detecting a fault occurring in the operation of a user equipment that is in communication with said first node; and sending a message to the user equipment indicating an action to be performed to stop or mitigate the fault in said user equipment. | 07-14-2011 |
20140126515 | Time Multiplexing Based Common Channel Scheduler Algorithm for Flexible Resource Sharing - The present disclosure relates to embodiments of a node entity and method for scheduling user data packets on a common channel of a base station node. The common channel being shared by a number of mobile telecommunications operators, OPi, i=1,2,3, . . . . The scheduling of the user data packets is performed in consecutive Transmission Time Intervals, TTIs, and in dependence of which operator OPi serving different user packets. During a TTI, the data packets are transmitted according to scheduling determined in the adjacent previous TTI. During the TTI, a scheduler controller calculates and determines the prioritised OPi for the next TTI, said calculation being performed by calculation based on the share of TTIs with competition per operator within a sliding window and a list keeping information based on a predetermined number of previous, consecutive TTIs within the sliding window. | 05-08-2014 |
Patent application number | Description | Published |
20100332614 | FACILITATING SUBSCRIPTION SERVICES IN THE IMS - A method of starting a third party application subscription in a set of Application Servers located within an IP Multimedia Subsystem network. The method comprises receiving a subscription start request at one of said Application Servers, the request including subscription data, starting the subscription data at that Application Server, and storing the subscription data as transparent data in a Home Subscriber Server, from that Application Server over the Sh interface. | 12-30-2010 |
20110314166 | End-to-End Address Transfer - According to a first aspect of the present invention there is provided a method of facilitating the end-to-end transfer of a URI between a plurality of SIP entities. The method comprising generating a SIP message and including the URI to be transferred in a Contact header of the message and including in the Contact header a parameter indicating to a back-to-back user agent that this URI is not to be changed or replaced. | 12-22-2011 |
20120195235 | METHOD AND APPARATUS FOR SPECIFYING A USER'S PREFERRED SPOKEN LANGUAGE FOR NETWORK COMMUNICATION SERVICES - A new telecommunication service provides users with the ability to specify and receive spoken-language services in a preferred language that differs from a preferred written or text language. One or more user (e.g., a subscribing entity) preferences for spoken language as well as written language is specified and stored, e.g., in a subscriber database. An application server uses the configured spoken language preference(s) to select the language used for voice announcements, voice prompts, and other voice applications provided in one or more telecommunication services. For example, the server populates the existing SIP Accept-Language header and/or a new SIP P-Media-Language field with the spoken language preference(s) to allow the other servers, e.g., in a home and destination domain, to provide spoken/voice service as well as text-based service to the user according to the user's language preference(s). | 08-02-2012 |
20130039225 | METHOD AND APPARATUS RELATING TO CHARGING IN AN IP MULTIMEDIA SUBSYSTEM - A method relating to the charging of a service in an IP Multimedia Subsystem, IMS. The service is one that is requested by a first subscriber and that involves a second subscriber. A service-related request message is received (S | 02-14-2013 |
20140098716 | End-to-End Address Transfer - According to a first aspect of the present invention there is provided a method of facilitating the end-to-end transfer of a URI between a plurality of SIP entities. The method comprising generating a SIP message and including the URI to be transferred in a Contact header of the message and including in the Contact header a parameter indicating to a back-to-back user agent that this URI is not to be changed or replaced. | 04-10-2014 |
Patent application number | Description | Published |
20130280364 | Apparatus And System For Expanding Expandable Polymeric Microspheres - An apparatus including: (a) a steam generator having a power output of less than or equal to about 6 boiler horsepower; (b) a steam conduit in fluid communication with the steam generator; (c) a fluid material conduit in fluid communication with a source of a fluid material, wherein the fluid material includes unexpanded, expandable polymeric microspheres; (d) a treatment zone in fluid communication with the steam generator via the steam conduit, and with the fluid material conduit, such that the fluid material is contacted by steam within the treatment zone; and (e) a back pressure generator in fluid communication with the treatment zone, capable of increasing pressure in the treatment zone, which results in expansion of the expandable polymeric microspheres when the fluid material exits the treatment zone. | 10-24-2013 |
20150093468 | Apparatus And System For Expanding Expandable Polymeric Microspheres - An apparatus including: (a) a steam generator having a power output of less than or equal to about 6 boiler horsepower; (b) a steam conduit in fluid communication with the steam generator; (c) a fluid material conduit in fluid communication with a source of a fluid material, wherein the fluid material includes unexpanded, expandable polymeric microspheres; (d) a treatment zone in fluid communication with the steam generator via the steam conduit, and with the fluid material conduit, such that the fluid material is contacted by steam within the treatment zone; and (e) a back pressure generator in fluid communication with the treatment zone, capable of increasing pressure in the treatment zone, which results in expansion of the expandable polymeric microspheres when the fluid material exits the treatment zone. | 04-02-2015 |
Patent application number | Description | Published |
20120074265 | NANO-REINFORCED RADIUS FILLER FOR AN AIRCRAFT STRUCTURE AND A METHOD OF PRODUCING AN AIRCRAFT STRUCTURE COMPRISING SUCH FILLER - A composite radius filler for use in an aircraft structure. The aircraft structure includes structural composite parts assembled together to form the aircraft structure. The composite radius filler is arranged between rounded sections of the structural composite parts for filling a gap formed between the structural composite parts. The composite radius filler is made structural by a nanostructure arranged within the composite radius filler for the reinforcement of the interface between the radius filler and the structural composite part. A method for producing an aircraft structure including a nano-reinforced radius filler. | 03-29-2012 |
20120088056 | STRUCTURAL LONGITUDINAL COMPOSITE JOINT FOR AIRCRAFT STRUCTURE - A structural composite part made of pre-impregnated fiber plies. The edges of two adjacent fiber plies are connected via a longitudinal composite joint made structural by a nanostructure arranged within the composite joint. A method of producing a structural composite part made of pre-impregnated fiber plies. The edges of two adjacent fiber plies are connected via a longitudinal composite joint made structural by a nanostructure and an aircraft structure comprising such structural composite parts. | 04-12-2012 |
20120148789 | AIRCRAFT STRUCTURE WITH STRUCTURAL PARTS CONNECTED BY NANOSTRUCTURE AND A METHOD FOR MAKING SAID AIRCRAFT STRUCTURE - An aircraft structure including structural composite parts assembled together to form the aircraft structure. A bonding interlayer material bonds the structural composite parts to each other. The bonding interlayer material includes a nanostructure enhanced material. A method of producing an aircraft structure of assembled structural composite parts, being cured or semi-cured before assembly. | 06-14-2012 |
20120292439 | ARTICLE WITH DE-ICING/ANTI-ICING FUNCTION - A structural article including an outer surface that serves as an aerodynamic surface when the structural article is subjected for an air stream. A resin matrix laminate includes an upper ply and a bottom ply. A heating element is arranged in contact with the bottom ply and coupled to a power supply unit in purpose to deice/anti-ice the outer surface. Each ply includes a thermally conductive filament structure having a filament orientation such that the prolongation of the filaments has an extension essentially perpendicular to the extension of the laminate. The thermally conductive filament structure of the upper ply is embedded in the upper ply in such way that at least a portion of the thermally conductive filament structure is exposed in the outer surface. | 11-22-2012 |
20130028738 | MULTIFUNCTIONAL DE-ICING/ANTI-ICING SYSTEM OF A WIND TURBINE - A de-icing/anti-icing system including at least two conductive structures embedded in a wind turbine blade. An outer surface is designed as an aerodynamic surface. At least one of the conductive structures is arranged adjacent the outer surface. A control unit adapted to control the energy supply to the conductive structures for generating heat to the outer surface. One conductive structure includes a first conductive nano structure. A conductive property of the conductive structure differs from a conductive property of the other conductive structure including a second conductive nano structure, for achieving different degrees of heat depending on the needed mode of the system. | 01-31-2013 |
20130028744 | AERODYNAMIC SURFACE WITH IMPROVED PROPERTIES - An article including an outer surface that serves as an aerodynamic surface when the article is subjected for an air stream. A resin matrix made of a polymeric composite laminate of at least one ply includes the outer surface. The at least one ply includes a nano structure embedded therein such that nano filaments of the nano structure in the ply essentially have the same angular orientation relative the plane of the outer surface. The outer ply is a ply of a laminate including at least two plies. Each ply includes large fibers having an orientation different from or identical to the orientation of large fibers of an adjacent ply. | 01-31-2013 |
20130034447 | WIND TURBINE BLADE HAVING AN OUTER SURFACE WITH IMPROVED PROPERTIES - A wind turbine blade including an outer surface that serves as an aerodynamic surface when the blade is subjected for an air stream. A resin matrix made of a laminate of at least one ply includes the outer surface. The outer ply includes a nano structure embedded therein such that the filaments of the nano structure in the ply have essentially the same angular orientation relative a plane of the outer surface. | 02-07-2013 |
20130043342 | MULTIFUNCTIONAL DE-ICING/ANTI-ICING SYSTEM - A de-icing/anti-icing system including at least two conductive structures embedded in an article that includes an outer surface designed as an aerodynamic surface. At least one of the conductive structures is arranged adjacent the outer surface. A control unit adapted to control the energy supply to the conductive structures for generating heat to the outer surface. A first of the conductive structures includes a first conductive nano structure and a second of the conductive structures includes a second conductive nano structure. A conductive property of the first of the conductive structures differs from a conductive property of the second of the conductive structures. The first conductive nano structure serves as a heating conductor and the second conductive nano structure serves as a heating element. The first and second conductive nano structures are embedded in a common plane of a resin layer forming the outer surface. | 02-21-2013 |
20130129968 | COMPOSITE ARTICLE COMPRISING PARTICLES AND A METHOD OF FORMING A COMPOSITE ARTICLE - A composite article having a longitudinal direction and a transversal direction. The article includes a stack of plies wherein one ply is a bottom ply and one ply is a top ply. Most or all of the plies include fibers. A plurality of plies have fibers substantially in an orthogonal direction and substantially in a same direction as the longitudinally direction of the article. The bottom ply and the top ply have fibers in a substantially orthogonal direction to the longitudinal direction of the article. At least one ply has the fibers substantially in the same direction as the longitudinal direction of the article. At least one of the plies having fibers substantially in the longitudinal direction includes particles selected from the group of thermoplastic tougheners, nano particles, micro particles, elastic particles, elastomer particles and polymer particles or a combination. Also a method of forming an article on a tool. | 05-23-2013 |
20130240110 | SMOOTH SURFACE FORMING TOOL AND MANUFACTURE THEREOF - An aircraft article composite forming tool and a method for producing the tool. The aircraft article to be formed includes a composite material including an outer surface. The aircraft article composite forming tool includes a matrix laminate made of at least an upper ply including a forming surface for forming the aircraft article and outer surface. The upper ply includes a nano filament structure embedded therein. | 09-19-2013 |
20130291979 | PLASMA-ENHANCED ACTIVE LAMINAR FLOW ACTUATOR SYSTEM - The invention regards a plasma-enhanced active laminar flow actuator system ( | 11-07-2013 |
20150290845 | SMOOTH SURFACE FORMING TOOL AND MANUFACTURE THEREOF - A method of manufacture of a composite aircraft article aerodynamic surface by forming the composite aircraft article aerodynamic surface on an aircraft article composite forming tool. The aircraft article composite forming tool includes a matrix laminate including an upper ply including a forming surface for forming the composite aircraft article aerodynamic surface. The upper ply of the aircraft article composite forming tool includes a nano filament structure embedded therein. A blank is conformed onto the aircraft article composite forming tool. The aircraft article is formed on the upper ply of the forming surface. The forming surface of the aircraft article composite forming tool is adapted to form an aerodynamic surface of the aircraft article. The blank is cured into the aircraft article. The composite aircraft article is finished. | 10-15-2015 |
20150292074 | A POROUS COATING APPLIED ONTO AN AERIAL ARTICLE - An aerial article including a composite skin, a leading edge facing an airflow during use of the aerial article, an erosion resistant coating including a metallic material, and an aerodynamic surface. The coating at least partly covers the composite skin of the aerial article. The coating has a porosity sufficiently high to provide an open area, diffusion passage way, so as to permit moisture transportation from the composite skin to the aerodynamic surface of the coating. A method of applying an erosion resistant coating including a metallic material to a composite skin of an aerial article. An erosion resistant coating material is provided onto the composite skin over a selected area of the article. The coating is porous. The outer surface of the coating is polished to achieve a smooth aerodynamic surface. | 10-15-2015 |
20150298787 | AN AIRFRAME LEADING EDGE - An airframe leading edge part designed to be replaceable fixed to a structural portion which during use moves through the air. The airframe leading edge part includes first and second longitudinal joint edges adapted to fit the structural portion. At least one joint is provided between the structural portion and at least one of the longitudinal joint edges. The joint is adapted to break in the event of a object strikes and deforms the airframe leading edge part during use. The joint is designed to break at beforehand determined maximum joint strength of the joint. Also a repair method for exchanging a damaged leading edge. | 10-22-2015 |
20150298791 | MULTIFUNCTIONAL EROSION PROTECTION STRIP - An airfoil article including a composite skin having a first surface and a second surface opposite first surface, forming a leading edge. The leading edge is during use subjected to an airflow meeting the leading edge at stagnation points. The leading edge includes an elongated member. The outer surface of the elongated member is arranged flush with the first surface of the composite skin such that an essentially smooth aerodynamic surface of the leading edge is formed. The elongated member is adapted to serve as an erosion protection of the leading edge and to function as an electrode of a plasma generating system. | 10-22-2015 |
Patent application number | Description | Published |
20100274344 | Stent Delivery System Having Stent Securement Apparatus - A system/assembly for delivery and deployment of an inflation expandable stent within a vessel, comprising a catheter having proximal and distal ends; a stent, inflation expandable from a delivery diameter to a deployment diameter, such that the delivery diameter is reduced from the deployment diameter for conforming the stent to the catheter, such that the stent, in its delivery diameter, is coaxially mounted on the catheter near the catheter distal end; an expandable inflation means coaxially mounted on the catheter axially within the stent, for expansion of the stent from the delivery diameter to the deployment diameter upon application of fluid deployment pressure to the inflation means; and a securement component coaxially mounted on the catheter, axially within the expandable inflation means, the securement component designed and adapted to provide a securement pressure to the stent in the delivery diameter to maintain the stent in position on the catheter during delivery to the deployment site. | 10-28-2010 |
20130060317 | STENT DELIVERY SYSTEM HAVING STENT SECUREMENT APPARATUS - Medical devices and methods for making and using medical devices are disclosed. An example medical device may include an elongate shaft including a first tubular member and a second tubular member. A balloon may be coupled to the shaft. A first member may be coupled to the first tubular member and positioned within the balloon. A second member may be coupled to the first tubular member and positioned within the balloon. A medical implant may be coupled to the shaft and positioned adjacent to the balloon. | 03-07-2013 |
20140222128 | STENT DELIVERY SYSTEM HAVING STENT SECUREMENT APPARATUS - A system/assembly for delivery and deployment of an inflation expandable stent within a vessel, comprising a catheter having proximal and distal ends; a stent, inflation expandable from a delivery diameter to a deployment diameter, such that the delivery diameter is reduced from the deployment diameter for conforming the stent to the catheter, such that the stent, in its delivery diameter, is coaxially mounted on the catheter near the catheter distal end; an expandable inflation means coaxially mounted on the catheter axially within the stent, for expansion of the stent from the delivery diameter to the deployment diameter upon application of fluid deployment pressure to the inflation means; and a securement component coaxially mounted on the catheter, axially within the expandable inflation means, the securement component designed and adapted to provide a securement pressure to the stent in the delivery diameter to maintain the stent in position on the catheter during delivery to the deployment site. | 08-07-2014 |