Abstract:
A robotic apparatus for machining tenons on turbine buckets of a steam turbine machine is disclosed. The robotic apparatus includes a machining device having a spindle head. A robotic arm is coupled to the machining device and a base member is coupled to the robotic arm. The base member is mounted independently of the machine element. A vision system is provided for locating the tenon on the turbine bucket. A control system is coupled to the vision system, the machining device and the robotic apparatus. The control system is configured to control movement of the robotic apparatus and the machining device based upon vision system data and spatial information about the tenon and the turbine bucket.
Abstract:
A robotic apparatus for machining tenons on turbine buckets of a steam turbine machine is disclosed. The robotic apparatus includes a machining device having a spindle head. A robotic arm is coupled to the machining device and a base member is coupled to the robotic arm. The base member is mounted independently of the machine element. A vision system is provided for locating the tenon on the turbine bucket. A control system is coupled to the vision system, the machining device and the robotic apparatus. The control system is configured to control movement of the robotic apparatus and the machining device based upon vision system data and spatial information about the tenon and the turbine bucket.
Abstract:
A system and method for flame stabilization is provided that forestalls incipient lean blow out by improving flame stabilization. A combustor profile is selected that maintains desired levels of power output while minimizing or eliminating overboard air bleed and minimizing emissions. The selected combustor profile maintains average shaft power in a range of from approximately 50% up to full power while eliminating overboard air bleed in maintaining such power settings. Embodiments allow for a combustor to operate with acceptable emissions at lower flame temperature. Because the combustor can operate at lower bulk flame temperatures during part power operation, the usage of inefficient overboard bleed can be reduced or even eliminated.
Abstract:
A liner for a combustor of a gas turbine engine, including a shell having a first end adjacent to an upstream end of the combustor and a second end adjacent to a downstream end of the combustor, wherein at least one discrete region is subject to distress from impingement of hot gases, a plurality of cooling slots formed in the shell through which air flows for providing a cooling film along a hot side of the shell, and a group of cooling holes formed in the shell in the discrete region to augment the cooling film and provide convective bore cooling to the discrete region.
Abstract:
A method system and apparatus for cutting turbine bucket covers on a turbine rotor includes marking a cut path on a surface of the turbine bucket cover. The cut path includes a plurality of finite lines defined by a pair of end points, then directing a laser at each end point of each line of the cut path, storing a set of position coordinates of each end point for every line of the cut path; generating the cut path based on the respective end points; and following the cut path on the turbine bucket cover with a grinding machine attached to a robotic device; and cutting the turbine bucket cover according to the cut path.
Abstract:
An apparatus for machining a weld tab on an article. In one embodiment, the apparatus includes: a base member including at least one rolling element for contacting an underlying surface, the base member having a leading end and a trailing end; a cutting apparatus operably connected to the base member, the cutting apparatus including: a cutting member positioned proximate the leading end of the base member, the cutting member sized to coincide with a size of the weld tab; and a handle member proximate the trailing end and operably connected to the cutting member, the handle member for modifying a position of the cutting member relative to the base member.
Abstract:
A system and method for flame stabilization is provided that forestalls incipient lean blow out by improving flame stabilization. A combustor profile is selected that maintains desired levels of power output while minimizing or eliminating overboard air bleed and minimizing emissions. The selected combustor profile maintains average shaft power in a range of from approximately 50% up to full power while eliminating overboard air bleed in maintaining such power settings. Embodiments allow for a combustor to operate with acceptable emissions at lower flame temperature. Because the combustor can operate at lower bulk flame temperatures during part power operation, the usage of inefficient overboard bleed can be reduced or even eliminated.
Abstract:
A robotic apparatus and system for cutting turbine bucket covers on a turbine rotor are provided. The robotic apparatus includes a grinding device operable to drive a grinding wheel, a robotic arm coupled to the grinding device, a base member coupled to the robotic arm, a vision system for locating the fastener on the turbine bucket cover, and a control system. The base member is mounted independently of the turbine bucket cover. The control system is coupled to the vision system, the grinding device, and the robotic apparatus, and configured to control movement of the robotic apparatus and the grinding device based upon vision system data and spatial information related to the turbine bucket cover. The system includes at least a portion of a turbine rotor including a turbine bucket cover having at least one fastener thereon, and a robotic device for cutting the turbine bucket cover.
Abstract:
A method is provided of forming a micro-channel structure for use in a biosensing device. A master structure is provided having a first configuration of micro-channels with respective first fluid flow characteristics. One or more regions of material are deposited onto the master structure using a fluidjet process so as to modify the first configuration into a second configuration having respective second fluid flow characteristics, different from the first. Functional biosensing devices formed using the method are also described.
Abstract:
A process for the production of polypropylene comprising continuously contacting liquid propylene or a mixture comprising liquid propylene and one or more other alpha-olefins in one or more reaction zones, under gas phase polymerization conditions, with a catalyst system comprising (i) a solid particulate catalyst precursor, which includes magnesium; titanium; a halogen which is chlorine, bromine, or iodine, or mixtures thereof; and, as an inside electron donor, a carboxylic acid ester; (ii) a hydrocarbylaluminum cocatalyst; and (iii) as an outside electron donor, a silicon compound containing at least one silicon-oxygen-carbon linkage, the particles of precursor being carried into the reaction zone(s) via a portion of the liquid propylene, the flow rate of said portion having a Reynolds number greater than about 15,000.