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Patent # Description
2016/0363008 COMBINED CYCLE GAS TURBINE PLANT
This combined cycle gas turbine plant has a gas turbine (104) and a steam turbine (106) mounted on the same shaft. A control system is configured for switching...
2016/0363007 METHOD AND APPARATUS FOR GENERATING ELECTRICITY AND STORING ENERGY USING A THERMAL OR NUCLEAR POWER PLANT
A method for generating electricity by means of a nuclear power plant and a liquid vaporization apparatus involves, during a first period, producing heat...
2016/0363006 TURBINE TURNING GEAR SYSTEM
The invention relates to turning gear system for a turbine. The system comprises a pinion configured and arranged to engage a turning gear so as to turn a...
2016/0363005 COMPONENT CONSTRUCTION, COMPONENT FOR A GAS TURBINE AND METHOD FOR MANUFACTURING A COMPONENT OF GAS TURBINE BY...
A structural component construction that is suitable and provided for the purpose of being further processed into a structural component of a gas turbine is...
2016/0363004 INNER DIAMETER SCALLOP CASE FLANGE FOR A CASE OF A GAS TURBINE ENGINE
A case for a gas turbine engine incudes a radial flange with a partial scallop along an inner diameter of the radial flange. A case assembly for a gas turbine...
2016/0363003 MECHANICAL DRIVE ARCHITECTURES WITH HYBRID-TYPE LOW-LOSS BEARINGS AND LOW-DENSITY MATERIALS
Mechanical drive architectures can include a gas turbine having a compressor section, a turbine section, and a combustor section. A load compressor is driven...
2016/0363002 DAMPING MEANS FOR COMPONENTS IN A TURBOMACHINE AND METHOD FOR ASSEMBLING SAID DAMPING MEANS
The present disclosure relates to a damping device for absorbing structural vibrations or high excitation frequencies between a first component and a second...
2016/0363001 Emergency Shut-Down Detection System For A Gas Turbine
A gas turbine engine is provided with a controller configured to detect a spool shaft failure and to initiate an engine shut-down in response to the shaft...
2016/0363000 SYSTEM FOR DETECTING ABNORMAL MOVEMENT OF A SHAFT IN A GAS TURBINE ENGINE
The present invention provides a system for detecting abnormal axial movement of a shaft in a gas turbine engine. The system comprises a detection circuit...
2016/0362999 EFFICIENT POWER AND THERMAL MANAGEMENT SYSTEM FOR HIGH PERFORMANCE AIRCRAFT
A system and method for improved system efficiency of an integrated power and control unit (IPCU) of an aircraft is disclosed. The system uses an open-loop...
2016/0362998 GENERATOR FOR AN AIRCRAFT
An electrical generator for an aircraft includes a gas turbine engine having an exhaust section defining an exhaust cavity through which combustion exhaust...
2016/0362997 TURBINE ABRADABLE LAYER WITH INCLINED ANGLE SURFACE RIDGE OR GROOVE PATTERN
Turbine and compressor casing/housing abradable component embodiments for turbine engines, have abradable surfaces with ridges projecting from the abradable...
2016/0362996 COMPONENT WHICH CAN BE SUBJECTED TO HOT GAS FOR A GAS TURBINE AND SEALING ARRANGEMENT HAVING SUCH A COMPONENT
A component which can be subjected to hot gas for a gas turbine, the component having at least one wall, which includes a first surface as far as an edge, the...
2016/0362995 ROTOR FOR A TURBOMACHINE AND COMPRESSOR
A rotor for a turbomachine having at least a first rotor main body and a second rotor main body, the second rotor main body having a rotor arm having an...
2016/0362994 ANTI-ROTATION KNIFE EDGE SEALS AND GAS TURBINE ENGINES INCLUDING THE SAME
Anti-rotation knife edge seals and gas turbine engines including the same are provided. The anti-rotation knife-edge seal includes a first end portion having...
2016/0362993 INTERNAL MANIFOLD FOR TURNING MID-TURBINE FRAME FLOW DISTRIBUTION
A mid-turbine frame (MTF) for a gas turbine engine includes an inner manifold directing air to a turbine rotor of the gas turbine engine. The MTF includes an...
2016/0362992 ATTACHMENT ARRANGEMENT FOR TURBINE ENGINE COMPONENT
A component for a gas turbine engine according to an example of the present disclosure includes, among other things, a body having circumferential sides...
2016/0362991 RUNNER FOR A TIDAL POWER PLANT AND TIDAL POWER PLANT COMPRISING SUCH A RUNNER
A runner for a tidal power plant, comprising a hub body provided with openings for receiving blades, individual rotating means for rotating each blade with...
2016/0362990 COMPOSITE DISK
A gas turbine engine composite disk includes dovetail slots between disk posts extending radially inwardly from a periphery, a hub ring of composite plies...
2016/0362989 TURBINE COMPONENT THERMAL BARRIER COATING WITH CRACK ISOLATING ENGINEERED GROOVE FEATURES
Engineered groove features (EGFs) are formed within thermal barrier coatings (TBCs) of turbine engine components. The EGFs are advantageously aligned with...
2016/0362988 METHOD FOR MODIFYING AN AIRFOIL SHROUD AND AIRFOIL
A method is provided for modifying an airfoil shroud located at a tip of a blade of an airfoil, the airfoil shroud having a first end edge, a second end edge,...
2016/0362987 Fan Blade Tip as a Cutting Tool
An airfoil for a gas turbine engine is disclosed. The airfoil may include a first side, and a second side opposite the first side. The first side and the...
2016/0362986 TURBINE AIRFOIL COOLING SYSTEM FOR BOW VANE
A cooling system (10) for a turbine airfoil (12) of a gas turbine engine, wherein the airfoil (12) has a bowed configuration is disclosed. The airfoil (12) may...
2016/0362985 HOT GAS PATH COMPONENT TRAILING EDGE HAVING NEAR WALL COOLING FEATURES
A hot gas path component includes a substrate having an outer surface and an inner surface. The inner surface defines an interior space. The outer surface...
2016/0362984 METHOD FOR MANUFACTURING A BLADING MEMBER ASSEMBLY, AND BLADING MEMBER ASSEMBLY
Disclosed is a method for manufacturing a blading member assembly for a fluid flow machine, wherein the blading member assembly includes at least one airfoil...
2016/0362983 LOW NOISE TURBINE FOR GEARED TURBOFAN ENGINE
A method of designing a gas turbine engine comprises the steps of including a fan section with a fan. A turbine section is included having a first turbine and...
2016/0362982 TURBOMACHINE COMPRISING A SHAFT SLEEVE AND ASSOCIATED SLEEVE TUBE
The invention relates to a turbomachine (30) comprising: a compressor stage and a turbine stage, each stage comprising at least one disk (42); and a tubular...
2016/0362981 ROTOR COMPONENT WITH SURFACES FOR CHECKING CONCENTRICITY
A rotor component for a rotor assembly of a fluid energy machine, particularly of a gas turbine, a steam turbine, a compressor or the like, wherein the rotor...
2016/0362980 SYSTEMS AND METHODS FOR MONITORING LONGWALL MINE ROOF STABILITY
Systems and methods are described for monitoring a condition of a mine roof using a longwall mining system. A plurality of powered roof supports is controlled...
2016/0362979 SPRAY SYSTEM FOR MINING MACHINE
A mining machine includes a chassis, a cutting assembly coupled to the chassis, and a spray arm coupled to the chassis and positioned proximate the cutting...
2016/0362978 MINING PIN RETENTION SYSTEM
An improved drive pin retention system for mining chains is disclosed, including several embodiments. The drive pin retention system further decreases the...
2016/0362977 System for Sampling from Formation While Drilling
A system of formation sampling while drilling, comprising: a suction pup joint provided to pump out and clean the formation fluid; a sampling pup joint...
2016/0362976 Dual Telemetry Receiver for a Measurement While Drilling (MWD) System
A receiver for a dual telemetry measurement while drilling (MWD) system and method for operating same are provided. The receiver includes a mud pulse receiver...
2016/0362975 Methods and a system for well logging communication
Methods and a system for communication between the well logging surface equipment and downhole tools. A well logging communication system comprised of a...
2016/0362974 PRESSURE TEST AND ACTUATION TOOL AND METHOD
A pressure test and actuation tool includes a housing; an insert disposed in operable communication with the housing. A metering head initially in sealed...
2016/0362973 REAL-TIME TRACKING OF BENDING FATIGUE IN COILED TUBING
A coiled tubing deployment system includes an offshore rig having a reel positioned thereon and coiled tubing wound on the reel. A guide arch is positioned on...
2016/0362972 SYSTEMS AND METHODS FOR ESTIMATING FORCES ON A DRILL BIT
Disclosed embodiments include systems and methods for estimating real-time bit forces experienced on a drill bit and decoupling bit force disturbances....
2016/0362971 SYSTEM AND METHOD FOR CONTROLLING A DRILLING PATH BASED ON DRIFT ESTIMATES IN A ROTARY STEERABLE SYSTEM
A method for drilling, comprising receiving, by a surface steerable system coupled to a drilling rig, BHA information from a rotary steerable bottom hole...
2016/0362970 Optimized Liquid or Condensate Well Production
A dedicated borehole for an ESP or artificial lift mechanism communicates with a sump or wellbore to collect liquids and/or condensate from one or more other...
2016/0362969 SIMULTANEOUS INJECTION OF AN ACIDIC WELL TREATMENT FLUID AND A PROPPANT INTO A SUBTERRANEAN FORMATION
A method of simultaneously injecting a proppant and an acidic well treatment fluid into a subterranean formation is described. The method includes pumping the...
2016/0362968 METHOD AND SYSTEM FOR LINING A TUBULAR
A liner having an outer surface coated with a fluid absorbing coating is cladded to a tubing string by inserting the folded liner into the tubing string and...
2016/0362967 APPARATUS AND METHOD FOR SETTING A LINER
An apparatus for selling a liner in a wellbore that includes a setting tool attached to a work string. The setting tool includes a stretching mandrel and a...
2016/0362966 Jumper Tube Connection for Wellscreen Assembly
A wellscreen assembly has first and second screen joints connected together and has at least first and second adjoining tubes with opposed ends separated by a...
2016/0362965 METHOD TO GRAVEL PACK USING A FLUID THAT CONVERTS TO IN-SITU PROPPANT
A method for completing a wellbore extending through a subterranean formation may include installing a sandface completion assembly in the wellbore; pumping a...
2016/0362964 Single Line Stab And Coupler And Method Of Use
A single line stab uses internal threading that allows a remotely operated vehicle (ROV) to mechanically mate up the stab and receptacle without the use of...
2016/0362963 WELLBORE FILTRATION TOOL WITH NOVEL WIPER CUP
The present invention provides wellbore cleaning tool and method featuring a wiper assembly which allows fluid to bypass the tool in one direction while...
2016/0362962 Sliding Sleeve Having Indexing Mechanism and Expandable Sleeve
A downhole tool, such as a sliding sleeve, is operable with pressure applied against one of a plurality of plugs deployed in the tool. A sleeve can engage the...
2016/0362961 High Pressure Circulating Shoe Track with Redundant Pressure Isolation Feature
A dual barrier system is provided to withstand pressure differentials well above those of the check valves in a float shoe used to allow circulation of a...
2016/0362960 SHIFTING TOOL ASSEMBLY THAT FACILITATES CONTROLLED PRESSURE EQUALIZATION
An exemplary downhole system includes a completion string positioned within a wellbore and providing at least an upper seal bore and a downhole device that...
2016/0362959 SEALING A PORTION OF A WELLBORE
A liner assembly tool includes a base tubular that includes a bore therethrough; a wellbore liner that includes a liner top and is coupled to the base tubular;...
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