Patent application number | Description | Published |
20080226811 | Textured Pea Proteins - The invention relates to granulated pea protein composition characterised in that the protein content expressed in terms of a dry substance ranges from 70 to 95% by dry weight, preferably from 70 to 90% by dry weight, more preferably from 80 to 85% by dry weight, a mean diameter ranges from 150 to 300 μm, a compressibility value determined by the HOSOKAWA method ranges from 5 to 15%, preferably from 8 to 13% and a tamped density determined by the HOSOKAWA method ranges from 0.450 and 0.650 g/ml, preferably from 0.550 and 0.650 g/ml. The method for producing said granulated pea protein composition, the use thereof in the form of a raw material for producing textured pea proteins and the thus obtainable textured pea proteins are also disclosed. | 09-18-2008 |
20100196542 | ENCAPSULATION AGENT COMPRISING A PEA MALTODEXTRIN AND/OR A PEA GLUCOSE SYRUP, COMPOSITIONS CONTAINING IT AND ITS PREPARATION METHOD - A subject of the present invention is the use of a maltodextrin and/or a glucose syrup obtained, by acid or enzymatic hydrolysis, from a leguminous starch having an amylose content comprised between 25% and 50%, expressed as dry weight relative to the dry weight of starch, for the encapsulation of organic compounds. | 08-05-2010 |
20100215825 | FIBER-RICH BAKED PRODUCT AND METHOD FOR THE PRODUCTION THEREOF - A baked product rich in flour-containing fibres includes from 6 to 20% by weight a mixture of at least one type of starch and an improving agent selected from a group consisting of branched maltodextrins, polydextrins and a polydextrose, wherein the percentages are expressed by weight with respect to a final product. | 08-26-2010 |
20110305740 | GRANULATED POWDER CONTAINING VEGETABLE PROTEINS AND MALTODEXTRINS, PROCESS FOR PRODUCING SAME, AND USES THEREOF - The present invention concerns a granulated powder comprising at least one vegetable protein and at least one starch hydrolyzate, characterized in that it has a laser volume average diameter D4,3 of between 10 μm and 500 μm, preferably between 50 μm and 350 μm, and even more preferably between 70 μm and 250 μm, and a dry matter content, determined after stoving at 130° C. for 2 hours, of greater than 80%, preferably greater than 85%, and even more preferably greater than 90%. | 12-15-2011 |
20110311599 | GRANULATED POWDER CONTAINING VEGETABLE PROTEINS AND FIBERS, PROCESS FOR PRODUCING SAME, AND USE THEREOF - The present invention concerns a granulated powder containing at least one vegetable protein and at least one vegetable fiber, characterized in that it has a laser volume mean diameter D4,3 of between 10 μm and 500 μm, preferably between 50 μm and 350 μm, and even more preferably between 70 μm and 250 μm, and a dry matter content, determined after stoving at 130° C. for 2 hours, of greater than 80%, preferably greater than 85%, and even more preferably greater than 90%. The present invention also concerns a process for manufacturing this granulated powder as well as its use in various industrial field, and more particularly in the food-processing field, where it is used as a functional agent such as an emulsifying, overrun, stabilizing, thickening and/or gelling agent, in particular for totally or partially replacing certain animal proteins in the preparation of food products. | 12-22-2011 |
20120015078 | VEGETABLE MILK GRANULATED POWDER, PROCESS FOR PRODUCING VEGETABLE MILK, AND USES THEREOF - The present invention relates to a vegetal milk, in the form of a granulated powder or of a solution, produced from vegetable raw materials and capable of replacing milk of animal origin, and more particularly cow's milk, and also the uses thereof as novel products intended for human foodstuffs. The present invention also relates to a process for preparing such vegetable milk. | 01-19-2012 |
20140370178 | GLUTEN-FREE COOKING PRODUCTS - The present invention relates to a composition for a gluten-free cooking product, and specifically for all products traditionally containing gluten, added as such or by way of bread flour, the products including, in particular, bakery products. The invention likewise relates to totally gluten-free cooking and/or bread products produced using the composition. | 12-18-2014 |
20150237885 | ASSEMBLY OF AT LEAST ONE VEGETABLE PROTEIN AND AT LEAST ONE DAIRY PROTEIN - A method for producing an assembly of at least one dairy protein and at least one vegetable protein, and the assembly obtained by the method. Also, the uses of the assembly, in particular in the food processing field. | 08-27-2015 |
Patent application number | Description | Published |
20120040169 | MACHINABLE COMPOSITE MATERIAL - An assembly that includes a first part composed of a fibrous structure that includes fibers and a cured resin matrix. The fibrous structure has at least one surface and a layer that is located on the surface. The layer includes a discontinuous fiber composite that is composed of randomly oriented short fibers and a cured resin matrix wherein the layer has been machined to provide a machined surface. The assembly also includes a second part that is attached to the first part. The second part includes at least one surface that fits against the machined surface on the first part. | 02-16-2012 |
20130101406 | HIGH PRESSURE MOLDING OF COMPOSITE PARTS - Composite pre-forms are molded at high pressure to form composite parts that can be used in place of metal-based high performance parts, such as the outlet guide vanes found in turbofan jet engines. The composite pre-forms include two different fiber orientations that are co-molded in a resin matrix at high pressures to provide composite outlet guide vanes and other high performance parts. Chambers within the composite part are optionally formed during molding of the pre-form at high pressures. | 04-25-2013 |
20130285284 | MODULE FOR HOLDING AT LEAST ONE BUSHING | 10-31-2013 |
20130309435 | OVER-MOLDING OF LOAD-BEARING COMPOSITE STRUCTURES - A load-bearing composite structure for connection to a support body or structure. The load-bearing structure includes a load-bearing element that is made up of continuous reinforcing fibers and a resin matrix. The load-bearing element has an attachment portion for connection to the support body. The load-bearing composite structure further includes a connection element that is formed using a molding material which is composed of discontinuous fibers and a resin matrix. The molding material is molded over the surface of the attachment portion of the load-bearing element. | 11-21-2013 |
20140377556 | METHOD FOR MAKING A DISCONTINUOUS FIBER MOLDING COMPOUND - A method for making a discontinuous fiber molding compound from carbon fiber tow. The method involves using remnants of carbon fiber tows from spent carbon fiber spools. The remnants are chopped into pieces to form an assembly of chopped carbon fiber tows that are from 1 cm to 10 cm long. The chopped carbon fiber tows are then mixed with a powdered resin to form a blend of chopped carbon fiber tows and powdered resin. The blend is heated to soften/melt the particles of resin and then cooled to form a discontinuous fiber molding compound. | 12-25-2014 |
20150355111 | TRACERS FOR USE IN COMPRESSION MOLDING OF UNIDIRECTIONAL DISCONTINUOUS FIBER COMPOSITE MOLDING COMPOUND - Tracking or tracing of both the global and local movements of unidirectional discontinuous fiber composite (UD-DFC) chips during compression molding of UD-DFC molding compound. The tracking capability is provided by including tracer chips in the UD-DFC molding compound. The tracer chips include a resin matrix and at least one unidirectional carbon tow which is made up of a plurality of carbon filaments. The tracer chip further includes a unidirectional tracer yarn which is made up of a plurality of unidirectional filaments that are detectable by x-ray or other radiation-based scanning technique. | 12-10-2015 |
20150375481 | MULTI-COMPONENT COMPOSITE STRUCTURES - A composite assembly that can be cured to form a multi-component composite structure which does not have micro cracks along the boundaries between the various components. The composite assembly includes a structural component and a moldable component wherein the coefficients of thermal expansion of the structural component and the moldable component at the interface or boundary between the two components are such that micro cracks do not form along the interface when the composite assembly is cured to form the multi-component composite structure. | 12-31-2015 |
Patent application number | Description | Published |
20100108812 | AEROSPACE ARTICLES MADE FROM QUASI-ISOTROPIC CHOPPED PREPREG - Quasi-isotropic chopped prepreg is used to make parts found in aerospace vehicles. Exemplary aerospace parts that are made using quasi-isotropic chopped prepreg include aircraft window frames, wing fairing supports, flange supports, frame gussets, rudder actuator brackets, shear ties, seat pedestals, cargo floor flange supports, storage bin fittings, antenna supports, torque tube pans, handle boxes, side guide fittings, wing box covers and intercostals. | 05-06-2010 |
20110011975 | Aerospace articles made from quasi-isotropic chopped prepreg - Quasi-isotropic chopped prepreg is used to make parts found in aerospace vehicles. Exemplary aerospace parts that are made using quasi-isotropic chopped prepreg include aircraft window frames, wing fairing supports, flange supports, frame gussets, rudder actuator brackets, shear ties, seat pedestals, cargo floor flange supports, storage bin fittings, antenna supports, torque tube pans, handle boxes, side guide fittings, wing box covers and intercostals. | 01-20-2011 |
20120055006 | AEROSPACE ARTICLES MADE FROM QUASI-ISOTROPIC CHOPPED PREPREG - Quasi-isotropic chopped prepreg is used to make parts found in aerospace vehicles. Exemplary aerospace parts that are made using quasi-isotropic chopped prepreg include aircraft window frames, wing fairing supports, flange supports, frame gussets, rudder actuator brackets, shear ties, seat pedestals, cargo floor flange supports, storage bin fittings, antenna supports, torque tube pans, handle boxes, side guide fittings, wing box covers and intercostals. | 03-08-2012 |
20120223183 | AEROSPACE ARTICLES MADE FROM QUASI-ISOTROPIC CHOPPED PREPREG - Quasi-isotropic chopped prepreg is used to make parts found in aerospace vehicles. Exemplary aerospace parts that are made using quasi-isotropic chopped prepreg include aircraft window frames, wing fairing supports, flange supports, frame gussets, rudder actuator brackets, shear ties, seat pedestals, cargo floor flange supports, storage bin fittings, antenna supports, torque tube pans, handle boxes, side guide fittings, wing box covers and intercostals. | 09-06-2012 |