Patent application number | Description | Published |
20120077746 | GLP-1 ANALOGUES PHARMACEUTICAL COMPOSITIONS - The present invention is directed to sustained release liquid pharmaceutical compositions comprising a liquid, a peptide analogue according to the formula [Aib | 03-29-2012 |
20120202743 | SUSTAINED RELEASE FORMULATIONS COMPRISING GnRH ANALOGUES - The present invention relates to pharmaceutical compositions for the controlled and sustained release of active substance comprising a biodegradable polymer or copolymer. Furthermore, the invention relates to pharmaceutical compositions for the controlled and sustained release of at least one active substance such as peptides or hormones and analogues thereof and the manufacturing process of such pharmaceutical compositions. | 08-09-2012 |
20120321714 | SOLID PHARMACEUTICAL COMPOSITION CONTAINING 6-OXO-6,7,8,9,10,11-HEXAHYDROCYCLOHEPTA (C)CHROMEN-3-YL SULFAMATE AND POLYMORPHS THEREOF - The present invention relates to a solid pharmaceutical composition including the active principle 6-oxo-6,7,8,9,10,11-hexahydrocyclohepta[c]chromen-3-yl sulfamate. The present invention also relates to polymorphs of the 6-oxo-6,7,8,9,10,11-hexahydrocyclohepta[c]chromen-3-yl sulfamate compound. | 12-20-2012 |
20140056977 | SOLID PHARMACEUTICAL COMPOSITION CONTAINING 6-OXO-6,7,8,9,10,11-HEXAHYDROCYCLOHEPTA (C)CHROMEN-3-YL SULFAMATE AND POLYMORPHS THEREOF - The present invention relates to a solid pharmaceutical composition including the active principle 6-oxo-6,7,8,9,10,11-hexahydrocyclohepta[c]chromen-3-yl sulfamate. The present invention also relates to polymorphs of the 6-oxo-6,7,8,9,10,11-hexahydrocyclohepta[c]chromen-3-yl sulfamate compound. | 02-27-2014 |
Patent application number | Description | Published |
20100161282 | WORKLOAD PERFORMANCE PROJECTION FOR FUTURE INFORMATION HANDLING SYSTEMS USING MICROARCHITECTURE DEPENDENT DATA - A performance projection system includes a test IHS and a currently existing IHS. The performance projection system includes surrogate programs and user application software. The test IHS or simulator includes a processor with hardware (HW) counter(s) and an L1 cache. The test IHS employs a memory that includes a virtual future IHS, currently existing IHS, surrogate programs, and user application software for determination of runtime and HW counter performance data. The user application software and surrogate programs execute on the currently existing IHS to provide designers with runtime data and HW counter or microarchitecture dependent data. Designers execute surrogate programs on the future IHS to provide runtime and HW counter data. Designers normalize and weight the runtime and HW counter data to provide a representative surrogate program for comparison to user application software performance on the future IHS. Using a scaling factor, designers may generate a projection of runtime performance for the user application software executing on the future IHS. | 06-24-2010 |
20100162216 | WORKLOAD PERFORMANCE PROJECTION VIA SURROGATE PROGRAM ANALYSIS FOR FUTURE INFORMATION HANDLING SYSTEMS - A performance projection system includes a test IHS and multiple currently existing IHSs. The performance projection system includes user application software and surrogate programs that execute on currently existing IHSs. The performance projection system measures user application software and surrogate program performance during execution on currently existing IHSs. The performance projection systems measures runtime program performance during execution of surrogate programs on a future semiconductor die IC design model or virtualized future system. Designers normalize and compare surrogate program runtime performance data with user application software performance data. Designers un-normalize the normalized runtime performance data to generate a projection of runtime performance on the future system. | 06-24-2010 |
20110271283 | ENERGY-AWARE JOB SCHEDULING FOR CLUSTER ENVIRONMENTS - A job scheduler can select a processor core operating frequency for a node in a cluster to perform a job based on energy usage and performance data. After a job request is received, an energy aware job scheduler accesses data that specifies energy usage and job performance metrics that correspond to the requested job and a plurality of processor core operating frequencies. A first of the plurality of processor core operating frequencies is selected that satisfies an energy usage criterion for performing the job based, at least in part, on the data that specifies energy usage and job performance metrics that correspond to the job. The job is assigned to be performed by a node in the cluster at the selected first of the plurality of processor core operating frequencies. | 11-03-2011 |
20140075448 | ENERGY-AWARE JOB SCHEDULING FOR CLUSTER ENVIRONMENTS - A job scheduler can select a processor core operating frequency for a node in a cluster to perform a job based on energy usage and performance data. After a job request is received, an energy aware job scheduler accesses data that specifies energy usage and job performance metrics that correspond to the requested job and a plurality of processor core operating frequencies. A first of the plurality of processor core operating frequencies is selected that satisfies an energy usage criterion for performing the job based, at least in part, on the data that specifies energy usage and job performance metrics that correspond to the job. The job is assigned to be performed by a node in the cluster at the selected first of the plurality of processor core operating frequencies. | 03-13-2014 |
20140196054 | ENSURING PERFORMANCE OF A COMPUTING SYSTEM - A system includes a plurality of computing systems, wherein each computing system comprises memory, a network interface and a processor. At least one computing system is configured to issue a command to run abbreviated measurements of performance for one or more computing nodes to determine whether a number of the computing nodes is adequate to perform a computing job. The at least one computing system is configured to assign the computing job to a set of the number of computing nodes if each of the set of the number of computing nodes is adequate to perform the computing job according to performance measurement results of the abbreviated measurements. For any of the one or more computing nodes that is inadequate to perform the computing job according to performance measurement results of the abbreviated measurements, the at least one computing system is configured to indicate those computing nodes as low performing. | 07-10-2014 |
Patent application number | Description | Published |
20140064950 | Lateral propulsion unit for aircraft comprising a turbine engine support arch - A propulsion unit for an aircraft, comprising one turbine engine and a mounting device for a turbine engine designed to be added laterally on an aircraft structure and comprising a rigid mounting structure. The rigid mounting structure supports at least one arch which is concave towards the longitudinal axis of the propulsion unit and which has a distal end at an angular distance of between 45 and 120 degrees from a vertical plane passing through the axis, on the other side of the structure, and supporting a distal connecting element connecting the turbine engine to the arch. | 03-06-2014 |
20140183297 | BOOMERANG LINK WITH VIBRATION FILTERING ABILITY AND AIRCRAFT ENGINE MOUNT PROVIDED WITH SUCH LINK - A boomerang link for aircraft engine mounts, including a first orifice and a second orifice both designed to connect the boomerang link to an aircraft pylon, and a third orifice designed to connect the boomerang link to an aircraft engine. The third orifice is offset relative to a plane passing simultaneously through an axis of the first orifice and through an axis of the second orifice. When the boomerang link is seen in section in any plane orthogonal to the axes, a straight line segment extending from the axis of the second orifice to an axis of the third orifice crosses a region external to the boomerang link. This conformation confers on the boomerang link a flexibility enabling it to filter transverse vibrations between an engine and an aircraft pylon. | 07-03-2014 |
20140183298 | FLEXIBLE LINKING DEVICE FOR AN AIRCRAFT PROPULSION SYSTEM - A linking device including two hinge pins and having flexibility allowing vibrations between these two shafts to be filtered. The device includes a stack of plates connected to one another by layers of elastomer material. Plates of a first type are coupled to one of the shafts in relation to the movements parallel to the plates, while the plates of a second type are coupled to the other shaft in relation to the movements parallel to the plates, so as to allow relative movement of the shafts parallel to the plates. This linking device may be used in particular as a connecting rod, spreader beam or three-point shackle used in connecting a turbine engine to a pylon in a propulsion system of an aircraft such as an airplane. | 07-03-2014 |