Patent application number | Description | Published |
20090088425 | GLUCOCORTICOID RECEPTOR ANTAGONISTS - The present invention relates to compounds of formula I | 04-02-2009 |
20100249124 | 2,3-DIARYL- OR HETEROARYL-SUBSTITUTED 1,1,1-TRIFLUORO-2-HYDROXYPROPYL COMPOUNDS - The present invention relates to compounds of formula I | 09-30-2010 |
20100249139 | 1,1,1-TRIFLUORO-2-HYDROXYPROPYL COMPOUNDS - The present invention relates to compounds of formula I | 09-30-2010 |
20120232071 | 2,3-DIARYL- OR HETEROARYL-SUBSTITUTED 1,1,1-TRIFLUORO-2-HYDROXYPROPYL COMPOUNDS - The present invention relates to compounds of formula I | 09-13-2012 |
20130045972 | GLUCOCORTICOID RECEPTOR ANTAGONISTS - The present invention relates to compounds of formula I | 02-21-2013 |
20130172335 | 2,3-DIARYL- OR HETEROARYL-SUBSTITUTED 1,1,1-TRIFLUORO-2-HYDROXYPROPYL COMPOUNDS - The present invention relates to compounds of formula I | 07-04-2013 |
20150087644 | PYRROLIDINO HETEROCYCLES - The invention relates to compounds of formula I | 03-26-2015 |
20150148332 | TRIAZOLO COMPOUNDS AS PDE10 INHIBITORS - The present invention provides compounds of formula (Ia) and (Ib) | 05-28-2015 |
20150232472 | TRIAZOLO COMPOUNDS - The present invention relates to compounds of formula (I) and its use for the treatment of neurological disorders. | 08-20-2015 |
20160002177 | COMT INHIBITORS - The present invention relates to compounds of formula | 01-07-2016 |
Patent application number | Description | Published |
20110176930 | Turbine vane for a gas turbine and casting core for the production of such - A turbine vane or blade including an interior structure is provided. In addition, turbulence elements connected directly upstream of openings disposed at the rear edge of the blade of the turbine vane or blade are also provided. These are disposed in a sequence, each having a flow side against which a coolant flows and which is at least partially arched in a concave manner. Preferably, the turbulence elements are configured in a crescent-shaped manner. This makes it possible to enlarge the openings without resulting in an increased consumption of coolant. A casting core is also provided. The openings required in the casting core for the production of the webs of a turbine vane or blade may now be placed at further distances than before. | 07-21-2011 |
20110188999 | Axial turbine for a gas turbine with limited play between blades and housing - An axial turbine for a gas turbine including a rotor blade cascade is provided. The rotor blade cascade is formed from rotor blades each including, a front edge, a blade tip, and an annular space wall that surrounds the rotor blade cascade and includes an annular space inner side, enabling the annular space wall to be arranged directly adjacent to the blade tip forming a radial gap between the covering of the blade tip and the annual space inner side. When the turbine is in operation, the area of the blade tip with the highest pressure load is disposed in the region of the front edges, and the rotor blades in the region of their front edges include a radial projection and the annular space wall includes on the annular space inner side, a peripheral radial recess that interacts with the radial projections such that a minimum is established in the direction of the main through-flow of the turbine. | 08-04-2011 |
20110255956 | Gas turbine having cooling insert - A gas turbine including a plurality of rotor blades assembled into rotor blade rows and arranged on a turbine shaft and including a plurality of guide vanes assembled into guide van rows and mounted on a turbine housing by means of a guide van carrier is provided. The guide vane carrier includes a plurality of cooling air holes, and has a particularly high efficiency, while maintaining maximum operating reliability. Therefore, a cooling insert is introduced into a cooling air hole. | 10-20-2011 |
20120039716 | Guide vane system for a turbomachine having segmented guide vane carriers - A turbine guide vane system, in particular for a gas turbine is provided. The turbine guide vane system includes a number of guide vane rows and a guide vane carrier, to enable particularly simple replacement of guide vanes, while maintaining a particularly high degree of efficiency, and thus designed for particularly short repair durations. For this purpose, the guide vane carrier has a number of segments, wherein a segment extends over the entire radial extension of the guide vane carrier and the connection of the remaining segments may be detached, and wherein the turbine guide vane carrier includes at least two sections along the axial extension thereof that are connected to one another and have a different number of segments. | 02-16-2012 |
20120251741 | Method for adjusting the coolant consumption within actively cooled components, and component - A method for adjusting the coolant consumption within actively cooled components is produced. The components include an interior with at least one duct with different regions which have different cross sections of flow. A greater increase in the wall thickness is produced in the region having the smaller cross section of flow by a first diffusion process and a lesser increase in the wall thickness is produced in the region having the larger cross section of flow by a second diffusion process which is different from the first. By using different diffusion coatings in a component, it is possible to adjust the flow of coolant through a component in a controlled way. | 10-04-2012 |
20120321825 | Method for assessing the coolant consumption within actively cooled components - A process for setting the average flow rate within a hollow component is provided. The process includes setting a relatively small wall thickness in a first region with a relatively large flow cross section using a first diffusion coating process and setting a relatively large wall thickness by a second different diffusion process in a second region with a relatively small flow cross section. The use of different diffusion coatings in a component allows the flow of coolant through a component to be set in a controlled manner. | 12-20-2012 |
Patent application number | Description | Published |
20080232956 | Turbine Blade and Gas Turbine Equipped with a Turbine Blade - The invention relates to a turbine blade ( | 09-25-2008 |
20090016881 | TURBINE BLADE AND GAS TURBINE EQUIPPED WITH A TURBINE BLADE - The invention relates to a turbine blade comprising a vane that runs along a blade axis and a platform region, which is located at the root of the vane and has a platform that extends transversally to the blade axis. The aim of the invention is to guarantee the improved cooling of a platform region and the transition region from a turbine blade to a platform of a turbine blade, thus ensuring the cooling of the delimitation of a flow channel in a gas turbine. To achieve this, the platform comprises a first platform wall that does not support the vane and a second platform wall that supports said vane. According to the inventive concept, at the root of the vane and over the course of the transition region from the turbine blade to the platform, said first platform wall is aerodynamically curved and the course of the second platform wall has a receding shoulder in relation to the first platform wall, as a continuation of the vane. | 01-15-2009 |
20100008773 | Turbine blade and gas turbine equipped with a turbine blade - The invention relates to a turbine blade comprising a vane that runs along a blade axis and a platform region, located at the root of the vane having a platform that extends transversally to the blade axis. The aim of the invention is to configure a delimitation of a flow channel of a gas turbine in the simplest possible manner. Therefore, the platform is configured by an elastic sheet metal part that rests on the vane. Said part leads to a gas turbine comprising a flow conduit that runs along an axis of the gas turbine, said conduit having an annular cross-section for a working medium and a second vane stage that is situated downstream of a first vane stage, which runs along the axis. | 01-14-2010 |
Patent application number | Description | Published |
20110208185 | METHOD AND SYSTEM FOR ASSISTING A WIRE GUIDE TO CROSS OCCLUDED DUCTS - A method and a system for assisting a wire guide to cross obstructed ducts in mammalian body are described. The method and system is based on applying pulsed energy to occlusion obstructing the duct. The pulsed energy is applied by means of an auxiliary probe. The auxiliary probe is relatively displaceable with respect to the wire guide along a lumen provided within the probe. The distal region of the probe is provided with enhanced flexibility comparing with the reminder portion of the probe. | 08-25-2011 |
20110208206 | METHOD AND SYSTEM FOR DESTROYING OF UNDESIRABLE FORMATIONS IN MAMMALIAN BODY - A method and a system for destruction of an undesirable formation in a mammalian body are described. The invention is based on inserting a probe into mammalian body; said probe is electrically connectable to a control unit and upon bringing the probe in physical contact with the formation supplying pulses of energy from the control unit to the probe in order to destroy the formation. The invention further comprises counting amount of pulses being supplied to the probe and establishing a remaining service life of the probe by subtracting the amount of pulses being supplied to the probe from an amount of pulses corresponding to initial service life of the probe. The treatment session is automatically terminates as soon as amount of pulses being supplied to the probe approaches at least a fraction of the established remaining service life of the probe. The established remaining service life of the probe is stored for new treatment session. Delivery of pulses automatically terminates when the remaining service life is exhausted and use of such probe becomes impossible. | 08-25-2011 |
20130079797 | DEVICE AND METHOD FOR FRAGMENTING AND REMVOING CONCRETIONS FROM BODY DUCTS AND CAVITIES - A medical device and method for breaking a concretion in a body into smaller pieces and removing the pieces from the body are described. The device comprises a dilator sheath, a lithotripsy probe, a tubular member, and a retrieval basket. The dilator sheath adapted to penetrate into a passage of the body to reach the location where the concretion is located. The lithotripsy probe is configured for shattering the concretion into smaller pieces. The tubular member is mounted within the dilator sheath adapted to permit the lithotripsy probe to be inserted into the tubular member. The retrieval basket is coupled to the tubular member, and configured for entrapping the concretion and the smaller pieces for their extraction from the body. The retrieval basket comprises a structure constituted by a plurality of filaments extending from a basket proximal end towards a basket distal end, and then returning to the proximal end after forming a plurality of filament loops in the basket distal portion, and a plurality of filament strands at the basket proximal portion. | 03-28-2013 |
20140288571 | METHOD AND SYSTEM FOR DESTROYING OF UNDESIRABLE FORMATIONS IN MAMMALIAN BODY - A method and a system for destruction of an undesirable formation in a mammalian body are described. The invention is based on inserting a probe into mammalian body; said probe is electrically connectable to a control unit and upon bringing the probe in physical contact with the formation supplying pulses of energy from the control unit to the probe in order to destroy the formation. The invention further comprises counting amount of pulses being supplied to the probe and establishing a remaining service life of the probe by subtracting the amount of pulses being supplied to the probe from an amount of pulses corresponding to initial service life of the probe. The treatment session is automatically terminates as soon as amount of pulses being supplied to the probe approaches at least a fraction of the established remaining service life of the probe. The established remaining service life of the probe is stored for new treatment session. Delivery of pulses automatically terminates when the remaining service life is exhausted and use of such probe becomes impossible. | 09-25-2014 |
Patent application number | Description | Published |
20110087885 | METHOD AND APPARATUS FOR EFFICIENT AND SECURE CREATING, TRANSFERRING, AND REVEALING OF MESSAGES OVER A NETWORK - An encryption based method of enabling a plurality of parties to share, create, hide, or reveal message or token information over a network includes a commutative group cipher (CGC), where the underlying CGC is secure against ciphertext-only attack (COA) and plaintext attacks (KPA), and is deterministic. The protocols doe not require a trusted third party (TTP), and execute rapidly enough on ordinary consumer computers as to be effective for realtime play among more than two players. Protocols are defined which include VSM-L-OL, VSM-VL, VSM-VPUM, and VSM-VL-VUM, wherein the letters V, O, SM, P, and UM represent, respectively, Verified, Locking Round, Open, Shuffle-Masking Round, Partial, and Unmasking Round. | 04-14-2011 |
20110202766 | METHOD AND APPARATUS FOR EFFICIENT AND SECURE CREATING, TRANSFERRING, AND REVEALING OF MESSAGES OVER A NETWORK - An encryption based method of enabling a plurality of parties to share, create, hide, or reveal message or token information over a network includes a commutative group cipher (CGC), where the underlying CGC is secure against ciphertext-only attack (COA) and plaintext attacks (KPA), and is deterministic. The protocols do not require a trusted third party (TTP), and execute rapidly enough on ordinary consumer computers as to be effective for realtime play among more than two players. Protocols are defined which include VSM-L-OL, VSM-VL, VSM-VPUM, and VSM-VL-VUM, wherein the letters V, O, SM, P, and UM represent, respectively, Verified, Locking Round, Open, Shuffle-Masking Round, Partial, and Unmasking Round. | 08-18-2011 |