Patent application number | Description | Published |
20090065653 | Fast Track Switch - A system for sequentially switching a plurality of guide ways to accommodate at least one vehicle with a plurality of ground engaging portions following a plurality of plural track segments is provided. The system includes a primary guide way to receive at least one of the plurality of ground engaging portions of the at least one vehicle and a secondary guide way located in proximity to the primary guide way. The secondary guide way may be configured to receive another of the plurality of ground engaging portions of the at least one vehicle. The system may also include a controller configured to sequentially switch the primary guide way and the secondary guide way whereby the at least one vehicle may travel in one direction or in another direction. A method of switching a plurality of guide ways is also presented. | 03-12-2009 |
20110260009 | Fast Track Switch - A system for sequentially switching a plurality of guide ways to accommodate at least one vehicle with a plurality of ground engaging portions following a plurality of plural track segments is provided. The system includes a primary guide way to receive at least one of the plurality of ground engaging portions of the at least one vehicle and a secondary guide way located in proximity to the primary guide way. The secondary guide way may be configured to receive another of the plurality of ground engaging portions of the at least one vehicle. The system may also include a controller configured to sequentially switch the primary guide way and the secondary guide way whereby the at least one vehicle may travel in one direction or in another direction. A method of switching a plurality of guide ways is also presented. | 10-27-2011 |
20150252844 | SYSTEM AND METHOD FOR LUBRICATING PLAIN BEARINGS - A system includes a plain bearing assembly configured to enable rotation of a shaft about a bearing system axis of the shaft. The plain bearing assembly includes the shaft, a cylindrical intermediate bearing disposed about the shaft, and an external bearing disposed about the intermediate bearing. The plain bearing assembly is configured to facilitate oscillatory motion of the shaft relative to the external bearing such that, when the shaft rotates in a first direction about the bearing system axis, the intermediate bearing rotates about the bearing system axis in the first direction, and when the shaft rotates in a second direction opposite the first direction about the bearing system axis, rotation of the intermediate bearing about the bearing system axis is resisted or prevented. | 09-10-2015 |
20150252850 | SYSTEM AND METHOD FOR LUBRICATING ROLLING BEARING ELEMENTS - A system includes a rolling bearing element assembly configured to enable rotation of a rotary element relative to a stationary element, the rotation being about a bearing system axis of the rolling bearing element assembly. The rolling bearing element assembly includes an inner race, an outer race, and a plurality of rolling bearing elements disposed between the inner and outer races. The rolling bearing element assembly is configured to facilitate oscillatory motion of the rotary element relative to the stationary element such that, when the rotary element rotates in a first direction about the bearing system axis, the rolling bearing elements revolve about the bearing system axis in the first direction, and when the rotary element rotates in a second direction opposite the first direction about the bearing system axis, revolution of the rolling bearing elements about the bearing system axis in the second direction is resisted or prevented. | 09-10-2015 |
20150352452 | MOVING SHOW DOOR - A ride attraction system utilizes a robotic actuation system to move a curved door of a curved enclosure wall between a first position and a second position via a compound trajectory. In the first position, the door is mated with the wall, and in the second position, the door leaves an opening in the wall. The door and the wall may both include display surfaces that enable images to be displayed to occupants of a ride moving toward the wall and through the opening. | 12-10-2015 |
Patent application number | Description | Published |
20090087844 | METHODS AND COMPOSITIONS FOR CORRELATING GENETIC MARKERS WITH CARDIOVASCULAR DISEASE - The present invention provides methods of identifying a subject having an increased or decreased risk of developing cardiovascular disease, comprising:
| 04-02-2009 |
20110171630 | METHODS AND COMPOSITIONS FOR CORRELATING GENETIC MARKERS WITH CARDIOVASCULAR DISEASE - The present invention provides methods of identifying a subject having an increased or decreased risk of developing cardiovascular disease, comprising: a) correlating the presence of one or more genetic markers in chromosome 3q13.31 with an increased or decreased risk of developing cardiovascular disease; and b) detecting the one or more genetic markers of step (a) in the subject, thereby identifying the subject as having an increased or decreased risk of developing cardiovascular disease. Also provided are methods of identifying subjects with cardiovascular disease as having a good or poor prognosis, as well as methods of identifying effective treatment regimens for cardiovascular disease, based on correlation with genetic markers in chromosome 3q13.31. | 07-14-2011 |
20130017962 | METHODS AND COMPOSITIONS FOR CORRELATING GENETIC MARKERS WITH CARDIOVASCULAR DISEASE - The present invention provides methods of identifying a subject having an increased or decreased risk of developing cardiovascular disease, comprising: a) correlating the presence of one or more genetic markers in chromosome 3q13.31 with an increased or decreased risk of developing cardiovascular disease; and b) detecting the one or more genetic markers of step (a) in the subject, thereby identifying the subject as having an increased or decreased risk of developing cardiovascular disease. Also provided are methods of identifying subjects with cardiovascular disease as having a good or poor prognosis, as well as methods of identifying effective treatment regimens for cardiovascular disease, based on correlation with genetic markers in chromosome 3q13.31. | 01-17-2013 |
20130324416 | Methods and Compositions for Correlating Genetic Markers with Cardiovascular Disease - The present invention provides methods of identifying a subject having an increased or decreased risk of developing cardiovascular disease, comprising: a) correlating the presence of one or more genetic markers in chromosome 3q13.31 with an increased or decreased risk of developing cardiovascular disease; and b) detecting the one or more genetic markers of step (a) in the subject, thereby identifying the subject as having an increased or decreased risk of developing cardiovascular disease. Also provided are methods of identifying subjects with cardiovascular disease as having a good or poor prognosis, as well as methods of identifying effective treatment regimens for cardiovascular disease, based on correlation with genetic markers in chromosome 3q13.31. | 12-05-2013 |
Patent application number | Description | Published |
20080206542 | Ceramic matrix composite abradable via reduction of surface area - A ceramic matrix composite with an enhanced abradability has a patterned surface with an array of solid composite material and voids where the voids extend into but not through the composite. The flow of gas through the voids as the surface is traversed by an impinging component, such as a turbine blade tip, is inhibited by the shape and size of the voids which can be sealed by the passing blade tip. Separately or additionally the inhibition of gas flow can result from the filling of the voids with a ceramic material of higher abradability than the ceramic matrix composite. | 08-28-2008 |
20080279678 | Abradable CMC stacked laminate ring segment for a gas turbine - A pattern of depressions ( | 11-13-2008 |
20100080687 | Multiple Piece Turbine Engine Airfoil with a Structural Spar - A multiple piece turbine airfoil having an outer shell with an airfoil tip that is attached to a root with an internal structural spar is disclosed. The root may be formed from first and second sections that include an internal cavity configured to receive and secure the one or more components forming the generally elongated airfoil. The internal structural spar may be attached to an airfoil tip and place the generally elongated airfoil in compression. The configuration enables each component to be formed from different materials to reduce the cost of the materials and to optimize the choice of material for each component. | 04-01-2010 |
20100104426 | TURBINE ENGINE RING SEAL - Aspects of the invention relate to a ring seal for a turbine engine. The ring seal can be made up of a plurality of circumferentially abutted ring seal segments. Each ring seal segment can comprise a plurality of individual channels. The channels can be generally U-shaped in cross-section with a forward span, and aft span and an extension connecting therebetween. The channels can be positioned such that the aft span of one channel can substantially abut the forward span of another channel. The plurality of separate channels can be detachably coupled to each other by, for example, a plurality of pins. The ring seal segment according to aspects of the invention can facilitate numerous advantageous characteristics including greater material selection, selective cooling, improved serviceability, and reduced blade tip leakage. Moreover, the configuration is well suited to handle the operational loads of the turbine. | 04-29-2010 |
20100150703 | STACKED LAMINATE BOLTED RING SEGMENT - A ceramic ring segment for a turbine engine that may be used as a replacement for one or more metal components. The ceramic ring segment may be formed from a plurality of ceramic plates, such as ceramic matrix composite plates, that are joined together using a strengthening mechanism to reinforce the ceramic plates while permitting the resulting ceramic article to be used as a replacement for components for turbine systems that are typically metal, thereby taking advantage of the properties provided by ceramic materials. The strengthening mechanism may include a bolt or a plurality of bolts designed to prevent delamination of the ceramic plates when in use by keeping the ceramic plates in compression. | 06-17-2010 |
20110308085 | METHOD OF SERVICING AN AIRFOIL ASSEMBLY FOR USE IN A GAS TURBINE ENGINE - A method of servicing an airfoil for use in a gas turbine engine. The airfoil assembly is defined by a base material and includes an airfoil and a platform from which the airfoil extends. A predetermined amount of the base material is removed from the airfoil assembly proximate to a fillet area of the airfoil assembly via water jet material removal. The fillet area comprises a junction between the airfoil and the platform and is located at an intersection between the airfoil and the platform. A remainder of the base material comprising base material of the airfoil assembly other than proximate to the fillet area is left intact. | 12-22-2011 |