| Patent application number | Description | Published |
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| 20090077274 | Multi-Priority Communication in a Differential Serial Communication Link - A circuit includes a high priority circuit and a non-high priority circuit. The high priority circuit is operative to communicate high priority information to a single path of a differential serial communication link. The non-high priority circuit communicates non-high priority information to the single path. The high priority information is communicated prior to the non-high priority information. In one example, the circuit includes a flow control distributor operatively coupled to the high priority circuit and the non-high priority circuit. The flow control distributor distributes a total number of flow control credits into high priority credits and non-high priority credits. The flow control distributor controls communication of the high priority information based on the high priority credits. The flow control distributor controls communication of the non-high priority information based on the non-high priority credits. | 03-19-2009 |
| 20090100278 | Method and Apparatus for Managing Power Consumption Relating to a Differential Serial Communication Link - Briefly, a method, apparatus and system for managing power corresponding to a differential serial communication link that has a link width defined for example by one or more lanes wherein the lanes are adapted to communicate clock recovery information in a data stream, determines, during normal operating conditions, such as conditions other than power on, reset or link fault conditions, a desired link width for the serial communication link and then changes the link width accordingly. | 04-16-2009 |
| 20110057939 | Reading a Local Memory of a Processing Unit - Disclosed herein are systems, apparatuses, and methods for enabling efficient reads to a local memory of a processing unit. In an embodiment, a processing unit includes an interface and a buffer. The interface is configured to (i) send a request for a portion of data in a region of a local memory of an other processing unit and (ii) receive, responsive to the request, all the data from the region. The buffer is configured to store the data from the region of the local memory of the other processing unit. | 03-10-2011 |
| 20110145622 | DEVICE CONFIGURED TO SWITCH A CLOCK SPEED FOR MULTIPLE LINKS RUNNING AT DIFFERENT CLOCK SPEEDS AND METHOD FOR SWITCHING THE CLOCK SPEED - A device configured to switch a clock speed for multiple links running at different clock speeds and a method for switching the clock signals are disclosed. A frequency divider derives a plurality of clock signals at different frequencies from a source clock signal. A clock switching controller selects a maximum data rate among data rates requested by a plurality of ports of links and outputs a transmit clock signal at the selected maximum data rate to the ports along with a clock enabling signal for each of the ports. Each of the clock enabling signals selectively enables the transmit clock signal for matching a data rate requested by each port. The clock speed may be selected and updated as required by the ports glitch-free in a known amount of time without interrupting data transfers on any of the other ports. | 06-16-2011 |
| 20110161547 | METHOD AND DEVICE FOR DISABLING A HIGHER VERSION OF A COMPUTER BUS AND INTERCONNECTION PROTOCOL FOR INTEROPERABILITY WITH A DEVICE COMPLIANT TO A LOWER VERSION OF THE COMPUTER BUS AND INTERCONNECTION PROTOCOL - A method and a device for disabling a lower version of a computer bus and interconnection protocol (e.g., Peripheral Component Interconnect Express (PCIe) 2.0 or higher) for interoperability with a receiver compliant to a lower version of the protocol are disclosed. The device detects a presence of a receiver, and starts link training. During the link training, the number of link training failures or the elapsed time is counted. The device transmits a training sequence including symbols set in accordance with a higher version of the protocol that the device supports on each lane that the receiver is detected as long as the number of link training failures or the elapsed time is below a predetermined threshold. If the number of link training failures or the elapsed time reaches a predetermined threshold, the device transmits a training sequence including symbols set in accordance with a lower version of the protocol. | 06-30-2011 |
| Patent application number | Description | Published |
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| 20090060405 | High speed bearing system with bind-free axial displacement - A rotary bearing system that supports a shaft for rotating machinery in a housing comprises: at least one stationary rotary bearing mounted in the housing for supporting a respective journal of the shaft in a desired axial and radial alignment; at least one slidable rotary bearing, with an outer surface mounted within a respective inner support surface of the housing to form a respective linear bearing such that each slidable bearing may slide axially along the inner support surface of the housing, for supporting another respective journal of the shaft with the desired radial alignment; and at least one layer of a crystalline material that exhibits a high degree of basal cleavage bonded to at least one of the linear bearing surfaces; wherein each layer of crystalline material allows each slidable rotary bearing to slide axially along each respective linear bearing to compensate for differences in the coefficient of expansion of the housing and the shaft so as to prevent the bearing system from binding due to extreme environmental conditions. | 03-05-2009 |
| 20090214331 | Curved tooth coupling for a miniature gas turbine engine - A rotor assembly for a miniature gas turbine propulsion system comprises a centrifugal compressor wheel, a turbine wheel, a shaft and a tie bolt. The centrifugal compressor wheel includes a first curved tooth coupling, and the turbine wheel includes a second curved tooth coupling interconnected with the first curved tooth coupling. The shaft extends from the centrifugal compressor wheel, and the tie bolt extends between the shaft and the turbine wheel to bring the first curved tooth coupling into compression with the second curved tooth coupling. As such, the compressor wheel and the turbine wheel are assembled and remain, over the operational envelope of the propulsion system, in a reliably robust aligned configuration. | 08-27-2009 |
| 20090252604 | THERMAL MANAGEMENT SYSTEM FOR A GAS TURBINE ENGINE - A thermal management system and method for a miniature gas turbine engine includes a forward cover having a filter portion along an axis of rotation of a gas turbine engine, a first lubrication passage and a second lubrication passage. | 10-08-2009 |
| 20100037623 | High Efficiency Turbine Engine - A by-pass turbofan gas turbine engine, comprises: a by-pass fan with a by-pass fan outlet; a generally annular core engine duct with a core engine duct inlet coupled to the by-pass fan outlet and a core engine duct outlet; a generally annular by-pass duct situated in a generally coaxial relationship with the core engine duct with a by-pass duct inlet coupled to the by-pass fan outlet and a by-pass duct outlet; an upstream axial compressor with an axial upstream compressor inlet coupled to the core engine duct outlet and an axial upstream compressor outlet; a downstream radial compressor with an axial downstream compressor inlet coupled to the upstream compressor outlet and a radial downstream compressor outlet; a generally annular recuperator with a cool side inlet coupled to the downstream compressor outlet, a cool side outlet, a warm side inlet and a warm side outlet; a generally annular combustor with a combustor inlet coupled to the recuperator cool side outlet and a combustor outlet; a radial turbine with a radial turbine inlet coupled to the combustor inlet and a turbine outlet coupled to the recuperator warm side inlet; at least one exhaust nozzle with an exhaust nozzle inlet coupled to the recuperator warm side outlet and an exhaust nozzle outlet that discharges into the by-pass duct between the by-pass duct inlet and outlet; and a propelling nozzle coupled to the by-pass duct outlet. | 02-18-2010 |
| 20100276893 | Dynamic Sealing System - A dynamic sealing assembly for a rotating shaft to seal an forward portion of the shaft from an aft portion of the shaft, comprises: a stationary member that has an aperture with a spiral grooved aperture surface that passes through it to receive the shaft; and generally linear shaft surface undulations between the forward and aft portions of the shaft that are at least partially within the sealing member aperture; wherein rotation of the shaft causes the undulations to propagate fluid from between the rotating shaft and the aperture into the grooved aperture surface back toward the forward portion of the shaft. | 11-04-2010 |
| 20110072830 | COMBUSTOR INTERFACE SEALING ARRANGEMENT - A gas turbine engine sealing arrangement which includes a combustor liner establishing a combustion area and a turbine nozzle configured to receive a portion of a combustor liner. A sealing ring arrangement is configured to seal with the turbine nozzle to control fluid flow from the combustion area and reduce leakage. | 03-31-2011 |
