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| 20090105808 | Rapid Exchange Stent Delivery System and Associated Components - A rapid exchange stent delivery catheter includes an inner tubular member having a proximal portion, a distal portion, a stent holding portion located adjacent the distal portion of the inner member, and a guide wire lumen extending from a proximal guide wire opening disposed distal of the proximal portion of the inner member to a distal guide wire opening disposed at a distal end of the inner member. The proximal guide wire opening has a first length. An outer tubular member is slidably disposed about the inner member. The outer member has a proximal portion, a distal portion, and a guide wire opening disposed distal of the proximal portion of the outer member. The guide wire opening of the outer member has a second length that is shorter than the first length and a guide wire ramp extends into, and is movable along the first length. | 04-23-2009 |
| 20090312702 | BIFURCATION CATHETER ASSEMBLY WITH DISTALLY MOUNTED SIDE BALLOON AND METHODS - A catheter assembly and related methods directed to a main balloon and a side balloon, wherein the side balloon is coupled in fluid communication with the main balloon at a location distal of the side balloon. In one example, a side inflation member couples the side balloon in fluid communication to the main balloon at a distal end portion of the main balloon. A side catheter branch of the catheter assembly, which defines a side guidewire lumen, can be operatively mounted to the side balloon at a side balloon connection point to help maintain alignment of the side catheter branch relative to the side balloon. | 12-17-2009 |
| 20100030316 | BIFURCATION CATHETER DUAL BALLOON BOND AND METHODS - A catheter assembly includes a main catheter branch having a catheter shaft and a distal end portion. A main balloon and a side balloon are positioned at the distal end portion of the catheter shaft. The main balloon includes a distal waste portion at a distal end thereof and a proximal waste portion at a proximal end thereof. The side balloon includes an inflatable portion, a proximal waste portion, and a distal waste portion, wherein the proximal and distal waste portions define a side inflation lumen. The proximal waste portion of the side balloon and the proximal waste portion of the main balloon are secured to the distal end portion of the catheter shaft at a single bond or connection point to create a proximal balloon joint, wherein the main inflation lumen is in fluid communication with the main balloon and the side inflation lumen. | 02-04-2010 |
| 20100036477 | STENT EDGE PROTECTION AND METHODS - A catheter assembly and related methods directed to stent edge protection for an edge of a stent. One example stent edge protect member is positioned with a distal end portion of the stent edge protect member arranged proximal of and adjacent to a proximal end of the stent. The stent edge protect member defines an outer surface that transitions from an outer surface of the stent at the proximal end of the stent to an outer surface of the catheter branch on which the stent edge protect member is positioned. The stent edge protect member can be positioned on a single catheter branch or multiple catheter branches. | 02-11-2010 |
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| 20080314044 | HEAT SHIELDS FOR USE IN COMBUSTORS - A combustor includes an inner liner; an outer liner circumscribing the inner liner and forming a combustion chamber with the inner liner; a combustor dome coupled to the inner and outer liners; and a plurality of heat shields coupled to combustor dome. Each of the heat shields includes a heat shield plate defined by a first edge facing the inner liner and a second edge facing the outer liner; and a plurality of baffles extending from the heat shield plate. Each of the plurality of baffles includes two ribs and a connection portion connecting the two ribs to form a closed portion and an opposite open portion. The open portion of each of the plurality of baffles faces the first edge or the second edge. | 12-25-2008 |
| 20100162712 | QUENCH JET ARRANGEMENT FOR ANNULAR RICH-QUENCH-LEAN GAS TURBINE COMBUSTORS - A combustor for a turbine engine includes an outer liner having a first group of air admission holes and defining a plurality of outer liner regions. The combustor further includes an inner liner circumscribed by the outer liner and forming a combustion chamber therebetween, the inner liner having a second group of air admission holes and defining a plurality of inner liner regions. The combustor further includes a plurality of fuel injectors extending into the combustion chamber and configured to deliver an air-fuel mixture to the combustion chamber, each of the plurality of fuel injectors being associated with one of the outer liner regions and one of the inner liner regions. The first group within a respective outer liner region includes air admission holes that circumferentially alternate between approximately a first size and approximately a second size, the first size being different than the second size. | 07-01-2010 |
| 20100212324 | DUAL WALLED COMBUSTORS WITH IMPINGEMENT COOLED IGNITERS - A combustor for a gas turbine engine includes an inner liner and an outer liner circumscribing the inner liner and forming a combustion chamber with the inner liner. The outer liner is a dual walled liner with a first wall and a second wall. The combustor includes a fuel igniter comprising a tip portion configured to ignite an air and fuel mixture in the combustion chamber and an igniter tube positioning the fuel igniter relative to the combustion chamber. The igniter tube includes a plurality of holes configured to direct cooling air toward the tip portion of the fuel igniter. | 08-26-2010 |
| 20100218503 | PLUNGED HOLE ARRANGEMENT FOR ANNULAR RICH-QUENCH-LEAN GAS TURBINE COMBUSTORS - A combustor may include an outer liner having a first row and a second row of circumferentially distributed air admission holes. The second row of the outer liner may be downstream of the first row of the outer liner, and the air admission holes of the first row of the outer liner may be larger than the air admission holes of the second row of the outer liner. An inner liner is circumscribed by the outer liner and has a third and fourth row of circumferentially distributed air admission holes. The air admission holes of the third row of the inner liner may be larger than the air admission holes of the fourth row of the inner liner. The inner and outer liners may form a combustion chamber, and at least a portion of the air admission holes of the first, second, third, or fourth rows may be plunged. | 09-02-2010 |
| 20100218504 | ANNULAR RICH-QUENCH-LEAN GAS TURBINE COMBUSTORS WITH PLUNGED HOLES - A combustor may include an outer liner having a first group of air admission holes and defining a plurality of outer liner regions. The combustor may further include an inner liner having a second group of air admission holes and defining a plurality of inner liner regions. The first group of air admission holes within a respective outer liner region may include a first plunged air admission hole approximately axially aligned with the respective fuel injector, a second plunged air admission hole approximately on the outer boundary line between the respective outer liner region and a first adjacent outer liner region, the first air admission hole being downstream of the second air admission hole, and a third plunged air admission hole approximately on the outer boundary line between the respective outer liner region and a second adjacent outer liner region. | 09-02-2010 |
| 20110185739 | GAS TURBINE COMBUSTORS WITH DUAL WALLED LINERS - A combustor for a turbine engine includes a hot wall and a cold wall forming a dual walled liner and a liner cavity with the hot wall. The cold wall defines a plurality of impingement cooling holes configured to deliver an impingement cooling flow. A first downstream end terminates the hot wall and is configured to receive the impingement cooling flow from the plurality of impingement cooling holes, and a second downstream end terminates the cold wall and is longer in a generally downstream direction than the first downstream end. A combustion chamber is formed with the dual walled liner and the liner and faces an opposite side of the hot wall relative to the combustion chamber. The combustion chamber has a longitudinal axis and is configured to receive an air-fuel mixture in the generally downstream direction along the longitudinal axis. | 08-04-2011 |
| 20110219774 | CIRCUMFERENTIALLY VARIED QUENCH JET ARRANGEMENT FOR GAS TURBINE COMBUSTORS - A combustor for a turbine engine is provided. The combustor includes a first liner; a second liner positioned relative to the first liner to form a combustion chamber therebetween, the combustion chamber configured to receive a fuel-air mixture; an igniter positioned relative to the combustion chamber and configured to ignite the fuel-air mixture; a first group of air admission holes positioned in the first liner and forming a regular circumferential pattern around the first liner; and a second group of air admission holes positioned in the first liner at a first circumferential position corresponding to the igniter, the second group of air admission holes departing from the regular circumferential pattern. | 09-15-2011 |
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| 20110320700 | Concurrent Refresh In Cache Memory - Concurrent refresh in a cache memory includes calculating a refresh time interval at a centralized refresh controller, the centralized refresh controller being common to all cache memory banks of the cache memory, transmitting a starting time of the refresh time interval to a bank controller, the bank controller being local to, and associated with, only one cache memory bank of the cache memory, sampling a continuous refresh status indicative of a number of refreshes necessary to maintain data within the cache memory bank associated with the bank controller, requesting a gap in a processing pipeline of the cache memory to facilitate the number of refreshes necessary, receiving a refresh grant in response to the requesting, and transmitting an encoded refresh command to the bank controller, the encoded refresh command indicating a number of refresh operations granted to the cache memory bank associated with the bank controller. | 12-29-2011 |
| 20110320701 | OPTIMIZING EDRAM REFRESH RATES IN A HIGH PERFORMANCE CACHE ARCHITECTURE - Optimizing refresh request transmission rates in a high performance cache comprising: a refresh requestor configured to transmit a refresh request to a cache memory at a first refresh rate, the first refresh rate comprising an interval, the interval comprising receiving a plurality of first signals, the first refresh rate corresponding to a maximum refresh rate, and a refresh counter operatively coupled to the refresh requestor and configured to reset in response to receiving a second signal, increment in response to receiving each of a plurality of refresh requests from the refresh requestor, and reset and transmit a current count to the refresh requestor in response to receiving a third signal, wherein the refresh requestor is configured to transmit a refresh request at a second refresh rate, in response to receiving the current count from the refresh counter and determining that the current count is greater than a refresh threshold. | 12-29-2011 |
| 20110320729 | CACHE BANK MODELING WITH VARIABLE ACCESS AND BUSY TIMES - Various embodiments of the present invention manage access to a cache memory. In one embodiment, a set of cache bank availability vectors are generated based on a current set of cache access requests currently operating on a set of cache banks and at least a variable busy time of a cache memory includes the set of cache banks. The set of cache bank availability vectors indicate an availability of the set of cache banks. A set of cache access requests for accessing a set of given cache banks within the set of cache banks is received. At least one cache access request in the set of cache access requests is selected to access a given cache bank based on the a cache bank availability vectors associated with the given cache bank and the set of access request parameters associated with the at least one cache access that has been selected. | 12-29-2011 |
| 20110320730 | NON-BLOCKING DATA MOVE DESIGN - A mechanism for data buffering is provided. A portion of a cache is allocated as buffer regions, and another portion of the cache is designated as random access memory (RAM). One of the buffer regions is assigned to a processor. A data block is stored to the one of the buffer regions of the cache according an instruction of the processor. The data block is stored from the one of the buffer regions of the cache to the memory. | 12-29-2011 |
| 20110320778 | CENTRALIZED SERIALIZATION OF REQUESTS IN A MULTIPROCESSOR SYSTEM - Serializing instructions in a multiprocessor system includes receiving a plurality of processor requests at a central point in the multiprocessor system. Each of the plurality of processor requests includes a needs register having a requestor needs switch and a resource needs switch. The method also includes establishing a tail switch indicating the presence of the plurality of processor requests at the central point, establishing a sequential order of the plurality of processor requests, and processing the plurality of processor requests at the central point in the sequential order. | 12-29-2011 |
| 20110320862 | Edram Macro Disablement in Cache Memory - Embedded dynamic random access memory (EDRAM) macro disablement in a cache memory includes isolating an EDRAM macro of a cache memory bank, the cache memory bank being divided into at least three rows of a plurality of EDRAM macros, the EDRAM macro being associated with one of the at least three rows, iteratively testing each line of the EDRAM macro, the testing including attempting at least one write operation at each line of the EDRAM macro, determining if an error occurred during the testing, and disabling write operations for an entire row of EDRAM macros associated with the EDRAM macro based on the determining. | 12-29-2011 |
