Patent application number | Description | Published |
20100054946 | COMPRESSOR BLADE WITH FORWARD SWEEP AND DIHEDRAL - An airfoil for use as rotor blades in compressors for turbomachines, such as gas turbine engines. The airfoil includes increased forward sweep and forward dihedral effective to reduce losses generated by interaction of tip clearance flow, secondary flows and passage shocks. | 03-04-2010 |
20110056179 | TURBINE EXHAUST DIFFUSER WITH REGION OF REDUCED FLOW AREA AND OUTER BOUNDARY GAS FLOW - An exhaust diffuser system and method for a turbine engine. The outer boundary may include a region in which the outer boundary extends radially inwardly toward the hub structure and may direct at least a portion of an exhaust flow in the diffuser toward the hub structure. At least one gas jet is provided including a jet exit located on the outer boundary. The jet exit may discharge a flow of gas downstream substantially parallel to an inner surface of the outer boundary to direct a portion of the exhaust flow in the diffuser toward the outer boundary to effect a radially outward flow of at least a portion of the exhaust gas flow toward the outer boundary to balance an aerodynamic load between the outer and inner boundaries. | 03-10-2011 |
20110058939 | TURBINE EXHAUST DIFFUSER WITH A GAS JET PRODUCING A COANDA EFFECT FLOW CONTROL - An exhaust diffuser system and method for a turbine engine includes an inner boundary and an outer boundary with a flow path defined therebetween. The inner boundary is defined at least in part by a hub structure that has an upstream end and a downstream end. The outer boundary may include a region in which the outer boundary extends radially inward toward the hub structure and may direct at least a portion of an exhaust flow in the diffuser toward the hub structure. The hub structure includes at least one jet exit located on the hub structure adjacent to the upstream end of the tail cone. The jet exit discharges a flow of gas substantially tangential to an outer surface of the tail cone to produce a Coanda effect and direct a portion of the exhaust flow in the diffuser toward the inner boundary. | 03-10-2011 |
20120057967 | GAS TURBINE ENGINE - A gas turbine engine includes a diffuser section supplying cooling fluid, a rotatable shaft, shaft cover structure disposed about the rotatable shaft, support structure, and a cooling fluid channel between the shaft cover structure and the support structure. The support structure provides structural support for the shaft cover structure and receives cooling fluid from the diffuser section. One of the diffuser section and the support structure comprises a plurality of apertures through which at least a portion of the cooling fluid passes. The cooling fluid channel is in fluid communication with the apertures in the one of the diffuser section and the support structure for supplying cooling fluid to a blade disc structure located in a turbine section of the engine. | 03-08-2012 |
Patent application number | Description | Published |
20100303607 | Turbine Exhaust Diffuser Flow Path with Region of Reduced Total Flow Area - An exhaust diffuser system and method for a turbine engine includes an inner boundary and an outer boundary with a flow path defined therebetween. The inner boundary is defined at least in part by a hub that has an upstream end and a downstream end. The outer boundary has a region in which the outer boundary extends radially inward toward the hub. The region can begin at a point that is substantially aligned with the downstream end of the hub or, alternatively, at a point that is proximately upstream of the downstream end of the hub. The region directs at least a portion of an exhaust flow in the diffuser toward the hub. As a result, the exhaust diffuser system and method can achieve the performance of a long hub system while enjoying the costs of a short hub system. | 12-02-2010 |
20130098039 | EXHAUST DIFFUSER ADJUSTMENT SYSTEM FOR A GAS TURBINE ENGINE - A turbine exhaust diffuser adjustment system for a gas turbine engine capable of altering the flow of turbine exhaust gases is disclosed. The turbine exhaust diffuser adjustment system may be formed from one or more flow ramps positioned in a flowpath. The flow ramp may include a downstream, radially outward point that extends radially outward further from the ID flowpath boundary than an upstream, radially outward point that is positioned upstream from the downstream, radially outward point. The flow ramp may be adjustable such that an angular position of a radially outer surface of the flow ramp may be adjusted relative to the ID flowpath boundary, thereby enabling the flowpath to be changed during turbine operation to enhance the efficiency of the turbine engine throughout its range of operation. | 04-25-2013 |
20140041357 | EXHAUST DIFFUSER INCLUDING FLOW MIXING RAMP FOR A GAS TURBINE ENGINE - A turbine exhaust diffuser for a gas turbine engine. The diffuser includes a flow ramp positioned on an ID flowpath boundary within a flowpath of the diffuser. The flow ramp extends circumferentially about the hub and includes a downstream, radially outward point that extends radially outward further from the ID flowpath boundary than an upstream, radially outward point that is positioned upstream from the downstream, radially outward point. A wavy portion is located at the downstream, radially outward point of the flow ramp. The wavy portion includes a circumferentially extending, undulating surface defined by alternating axially extending crests and troughs. | 02-13-2014 |
20150086339 | DIFFUSER WITH STRUT-INDUCED VORTEX MIXING - A gas turbine engine includes inner and outer shrouds forming an annular gas path, and a plurality of struts connecting the inner shroud to the outer shroud. Airfoil shaped shields surround the struts, and each of the shields include a main body having an upstream leading edge defining a chordal axis extending in a downstream axial direction from the leading edge toward a downstream end of the shield. A trailing edge flap is located at the downstream end of each shield, the trailing edge flap including first and second span-wise portions. The first span-wise portion is oriented to direct flow at an angle relative to the chordal axis of the main body and the second span-wise portion is oriented to direct flow in a direction that is at a different angle than the angle of first span-wise portion. | 03-26-2015 |
Patent application number | Description | Published |
20090322480 | RFID TAG AND METHOD OF VEHICLE ATTACHMENT THEREOF - An electronic tag for a vehicle includes an antenna; a data transmitter coupled to the antenna; and an elastomeric coating layer encapsulating the transmitter and antenna. The tag may attach to the vehicle by means of a tire or otherwise affixed to the body of the vehicle. The antenna may be configured as a dipole accessible by an external signal from substantially a 360 degree sphere surrounding the tag package. An adhesive material layer may be included to encapsulate the elastomeric material coated transmitter and antenna and utilized to attach the tag to a vehicle component. | 12-31-2009 |
20110148592 | ANTENNA ASSEMBLY FOR A TAG READER - An antenna assembly includes a stand having a convex outer surface positioned to intercept and engage a vehicle tire as the vehicle tire passes over the convex stand surface. The height and contour of the convex stand surface slows the rotational rate of the vehicle tire, and thereby a transmitting device carried by the tire, to a preferred rotational read rate as the vehicle tire passes over the convex surface. One or more antenna members mount to the stand proximal to the convex surface, each antenna having a directionally aimed tilted antenna field positioned to continuously receive data transmission from the electronic transmitting device as the vehicle tire passes over the convex stand surface at the reduced rotational read rate. | 06-23-2011 |
20110148593 | METHOD FOR READING A VEHICLE TAG WITHIN A READ STATION - A method of reading a data transmission from an electronic transmitting device mounted to a vehicle tire assembly includes: positioning a convex upper surface of a stand to intercept a vehicle tire of the vehicle tire assembly; establishing rotational engagement between the vehicle tire and the convex upper surface of the stand to slow the speed of the vehicle and reduce the rotational rate at which the vehicle tire rotates to a targeted reduced rotational read rate; and directing an antenna field from at least one antenna toward an approach path (and at least one antenna toward the exiting path) of the vehicle tire to the convex upper surface and lower surface of the stand to receive data transmission from the electronic transmitting device as the vehicle tire passes over the stand upper surface then down the lower surface at the reduced rotational read rate. | 06-23-2011 |
20140049375 | STACKED TIRE RFID READER SYSTEM AND METHOD - A product management system and method for reading electronic identification tags from a vertical stack of tires. Each tire has an electronic identification tag secured at a position to operative to electronically transmit data to an antenna element positioned internally within a toroidal opening of each tire in the stack. An elongate read wand is positioned in a substantially vertical orientation within the aligned toroidal openings of the tires. The antenna element is carried by the read wand and is thus positioned by the read wand to receive an electronic transmission from each electronic identification tag in the aligned tire stack. The read wand may be ceiling-mounted, floor mounted, or hand held. | 02-20-2014 |
20150028101 | DRIVE-OVER STAND AND ANTENNA ASSEMBLY - A drive over stand for a TAG reader has a lead-on ramped surface and an exit-off ramped surface aligned and operative to intercept and engage the vehicle tire as the vehicle tire traverses over the upper surface of the stand. One or more pockets are disposed within the stand base, each receiving an antenna assembly. The antenna assembly is positioned within the pocket of the base, seated at a tilt angle operative to direct a read field toward a vehicle approach path to the stand. | 01-29-2015 |