Patent application number | Description | Published |
20080275129 | Methods and Pharmaceutical Compositions for the Treatment of Neurological Damage - The invention relates to a method of treating neurological damage, preferably spinal chord injury, said treatment comprising the topical administration of guanabenz. The invention also relates to the use of guanabenz for the preparation of a medicament for the treatment of neurological damage, preferably spinal chord injury, wherein said treatment comprises the topical administration of guanabenz to the site of said neurological damage. The invention is also directed to pharmaceutical compositions comprising guanabenz wherein said compositions are in the form of an aqueous gel or non-aqueous ointment. | 11-06-2008 |
20090018183 | N-phenylpyrrole guanidine derivatives as melanocortin receptor ligands - The present invention provides novel compounds of the general Formula (I) as ligands to the melanocortin receptors and/or for treatment of disorders in the melanocortin system: | 01-15-2009 |
20100056641 | Novel Aminoguanidines as Melanocortin Receptor Ligands - There are described compounds of general formula (I) and isomeric forms thereof wherein n is 0, 1, 2 or 3, saturated or unsaturated; most preferably at least one of R | 03-04-2010 |
20100098629 | Novel Amides Acting on the Adenosine Receptors - There are described Compounds of formula (I) in which R | 04-22-2010 |
20110082183 | PHENYL PYRROLE AMINOGUANIDINE DERIVATIVES - The present invention relates to phenyl pyrrole aminoguanidine derivatives of the general formula (I): (I) including tautomeric forms thereof, wherein n is 1, 2 or 3; or a pharmaceutically acceptable salt thereof. The present invention further relates to the use of such phenyl pyrrole aminoguanidine derivatives for the treatment of diseases associated with the melanocortin receptors or related systems, e.g. the melanocyte stimulating hormones. | 04-07-2011 |
20120190751 | COMPOUNDS FOR TREATMENTS OF INFLAMMATION - The present invention relates to the use of benzylideneaminoguanidines for the treatment of inflammation and pain. In one preferred embodiment, the invention relates to the use of N-(2-chloro-3,4-dimethoxybenzylideneamino)guanidine for the treatment of rheumatoid arthritis. | 07-26-2012 |
Patent application number | Description | Published |
20080216315 | Method of Producing an Engine Wall Structure - A method is provided for producing an engine wall structure that includes an inner wall, to which hot gas is admitted during engine operation, an outer wall, which is colder than the inner wall during engine operation, and at least two webs that connect the inner wall with the outer wall and delimit a cooling duct between the walls. The engine wall structure is produced by wire-electro discharge machining the duct out of a solid sheet forming the entire engine wall structure including the inner wall, the outer wall and the webs. | 09-11-2008 |
20080276596 | Engine Wall Structure and a Method of Producing an Engine Wall Structure - An engine wall structure includes an inner wall to which hot gas is admitted during engine operation, an outer wall, which is colder than the inner wall during engine operation, and at least two webs that connect the inner wall with the outer wall and delimit a cooling duct between the walls. The webs are mainly formed by a first material and the inner wall is mainly formed by a second material of other composition and other heat conductivity than the first material. | 11-13-2008 |
20100037589 | COMPONENT CONFIGURED FOR BEING SUBJECTED TO HIGH THERMAL LOAD DURING OPERATION - A component configured for being subjected to a high thermal load during operation includes a wall structure with cooling channels adapted for handling a coolant flow. At least one first cooling channel is adapted to convey the coolant from a first portion of the component to a second portion of the component. At least one second cooling channel in the second portion is closed so that the coolant is at least substantially-prevented from entering the closed second cooling channel from a cooling channel in the first portion. | 02-18-2010 |
20100116792 | METHOD OF JOINING PIECES OF METAL MATERIAL AND A WELDING DEVICE - A welding device includes at least one beam-reflecting side element arranged so as to reflect at least a part of a high energy density beam towards a region in which a weld joint is to be generated in a piece of material, wherein the beam-reflecting side element protrudes from a surface of said piece of material. | 05-13-2010 |
20100180575 | ENGINE WALL STRUCTURE AND A METHOD OF PRODUCING AN ENGINE WALL STRUCTURE - An engine wall structure includes an inner wall to which hot gas is admitted during engine operation, an outer wall, which is colder than the inner wall during engine operation, and at least two webs that connect the inner wall with the outer wall and delimit a cooling duct between the walls. The webs are mainly formed by a first material and the inner wall is mainly formed by a second material of other composition and other heat conductivity than the first material. | 07-22-2010 |
20100229565 | WALL OF A ROCKET ENGINE - A wall configured to withstand a high thermal load, said wall having a surface that is turned away from a heat source and provided with at least one strengthening element that, from a base portion thereof, protrudes from said surface. Said at least one strengthening element presents a decreasing width from its base portion towards a top portion thereof. The wall is an engine wall of a thrust nozzle of a rocket engine. | 09-16-2010 |
20100278641 | LINER FOR A TURBINE SECTION, A TURBINE SECTION, A GAS TURBINE ENGINE AND AN AEROPLANE PROVIDED THEREWITH - A liner for a turbine section includes a first wall, a plurality of webs interconnected with and projecting from the first wall, and a plurality of cooling channels, each of the cooling channels being delimited by two adjacent webs and the first wall, wherein each cooling channel presents a height corresponding to the height of its delimiting webs, and a width corresponding to the distance between its delimiting webs. At least one of the cooling channels has a width/height ratio of below 5 or/and the material of the webs has a higher thermal conductivity than the material of the first wall. A turbine section, a gas turbine engine and an aeroplane provided with such a liner are also disclosed. | 11-04-2010 |