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Patent # Description
2016/0153306 RADIAL POSITION CONTROL OF CASE SUPPORT STRUCTURE WITH SPLINED CONNECTION
A radial position control assembly for a gas turbine engine includes a case structure. A support structure is operatively supported by the case structure...
2016/0153305 TUNED ROTOR DISK
A gas turbine engine includes a rotor that has a rotor disk and a plurality of circumferentially-spaced blades. The rotor disk and the blades are co-rotatable...
2016/0153304 LOW LOSS AIRFOIL PLATFORM RIM SEAL ASSEMBLY
An airfoil stage of a turbine engine includes an upstream airfoil assembly, a downstream airfoil assembly in rotational relationship to the upstream airfoil...
2016/0153303 SNAP IN PLATFORM DAMPER AND SEAL ASSEMBLY FOR A GAS TURBINE ENGINE
A turbine assembly includes a first turbine blade circumferentially adjacent to a second turbine blade. The first turbine blade includes a first platform with...
2016/0153302 TURBINE WHEEL COVER-PLATE MOUNTED GAS TURBINE INTERSTAGE SEAL
A sealing system for a multi-stage turbine includes multiple first interstage seal subsystems disposed circumferentially about a rotor wheel shaft of the...
2016/0153301 NON-LINEARLY DEFLECTING BRUSH SEAL LAND
A brush seal land is disclosed. The brush seal land may comprise a first portion configured to be coupled to a turbine disc of an aircraft engine and a second...
2016/0153300 SEALING ASSEMBLY
A seal arrangement for a gas turbine engine includes a seal runner having a sealing lip extending radially outwardly from a root portion to a tip portion. A...
2016/0153299 TURBINE NOZZLE WITH IMPINGEMENT BAFFLE
A turbine nozzle apparatus includes: a vane extending between inner and outer bands, the interior of the vane being open and communicating with an aperture in...
2016/0153298 METHOD FOR ASSEMBLING TURBOMACHINE PARTS AND ASSEMBLY USED DURING SUCH A METHOD
A method for assembly of a first turbomachine part with at least one second turbomachine part, including an injection of a vulcanisable elastomer, preferably a...
2016/0153297 GAS TURBINE ENGINE TURBINE VANE RING ARRANGEMENT
A vane pack for a gas turbine engine includes an annular arrangement of vanes. A ring is secured around the vanes and extends proud of an axial end of the vanes.
2016/0153296 FLOW DISCOURAGER FOR VANE SEALING AREA OF A GAS TURBINE ENGINE
An interface within a gas turbine engine includes a sealing surface defined by a portion of a vane platform. A seal is in contact with said sealing surface. A...
2016/0153295 COMPOSITE VANE FOR A TURBINE ENGINE
A composite vane for a turbine engine, the vane having a pressure side face (12) and a suction side face (14) that define the aerodynamic profile of the vane,...
2016/0153294 FIRST STAGE TURBINE VANE ARRANGEMENT
The disclosure relates to a vane arrangement with a vane carrier, an array of rocking first stage vanes, and an array of frame segments for axially receiving...
2016/0153293 AXIAL FLOW EXPANDER
The axial flow expander includes: an outer casing provided with a suction port and a discharge port through which gas is discharged from the outer casing; an...
2016/0153292 FRAME SEGMENT FOR A COMBUSTOR TURBINE INTERFACE
The disclosure relates Frame segment for a transition piece-turbine interface having a picture frame receptacle for axially receiving an aft end of a combustor...
2016/0153291 COOLING SYSTEM OF A STATOR ASSEMBLY FOR A GAS TURBINE ENGINE HAVING A VARIABLE COOLING FLOW MECHANISM AND...
A cooling system integrated into a stator assembly of a gas turbine engine has an on-board injector or cooling nozzle located for cooling of a rotor assembly....
2016/0153290 GAS TURBINE BLADE AND METHOD OF PROTECTING SAME
A method of protecting a blade of a gas turbine engine by applying a nanocrystalline metal coating to a portion of the blade root is disclosed, which includes...
2016/0153289 GAS TURBINE ENGINE CERAMIC COMPONENT ASSEMBLY ATTACHMENT
A gas turbine engine component assembly includes first and second portions, wherein at least one of the first and second portions is a ceramic material. The...
2016/0153288 RECESSION RESISTANT CERAMIC MATRIX COMPOSITES AND ENVIRONMENTAL BARRIER COATINGS
The disclosure relates generally to recession resistant gas turbine engine articles that comprise a silicon containing substrate, and related coatings and...
2016/0153287 PLATED POLYMER TURBINE COMPONENT
Plated polymeric gas turbine engine parts and methods for fabricating lightweight plated polymeric gas turbine engine parts are disclosed. The parts include a...
2016/0153286 TURBINE CLEARANCE CONTROL UTILIZING LOW ALPHA MATERIAL
A turbine module comprises a stator assembly disposed annularly about a rotor assembly. The rotor assembly includes a plurality of turbine blades ...
2016/0153285 TURBINE BLADE
A turbine blade includes a first cooling air duct and a second cooling air duct which is separated from the first cooling air duct by a wall and which has a...
2016/0153284 GAS TURBINE ENGINE FLOW PATH MEMBER
A gas turbine engine flow path member is disclosed which includes an extending end portion capable of contacting a surface of the turbine engine. The flow path...
2016/0153283 GAS TURBINE ENGINE COMPONENT WITH CONVERGING/DIVERGING COOLING PASSAGE
A component for a gas turbine engine includes a gas path wall having a first surface and a second surface and a cooling hole extending through the gas path...
2016/0153282 Stress Reduction For Film Cooled Gas Turbine Engine Component
A component for a gas turbine engine includes a highly conductive film cooled component with a leading edge area and a trailing edge area, the leading edge...
2016/0153281 COMPONENTS WITH COMPOUND ANGLED COOLING FEATURES AND METHODS OF MANUFACTURE
A hot gas path component including a substrate having an outer surface exposed to a stream of hot gases and an inner surface exposed to a cooling flow. One or...
2016/0153280 DRILL TO FLOW MINI CORE
A core for forming a cooling microcircuit has at least one row of metering/tripping features configured to form at least one row of protrusions in the cooling...
2016/0153279 LOW NOISE TURBINE FOR GEARED TURBOFAN ENGINE
A turbine module according to an example of the present disclosure includes, among other things, a fan drive rotor having a plurality of blade rows each...
2016/0153278 TEMPORARY ROOF SUPPORT SYSTEM
A temporary roof support system of a roof bolter machine is provided. The temporary roof support system includes a multistage cover assembly, a sliding...
2016/0153277 MONITORING A WELL FLOW DEVICE BY FIBER OPTIC SENSING
Monitoring a well flow device by fiber optic sensing. A system includes processing circuitry configured to be disposed downhole in a wellbore. The processing...
2016/0153276 Multifunction End Cap for Coiled Tube Telemetry
A multifunctional end cap assembly for use in terminating the toe end of subsurface coiled tubing strings that include multiple sensors. The assembly includes...
2016/0153275 Systems and Methods for Positioning Horizontal Wells Within Boundaries
Systems and methods for positioning horizontal wells within a limited-pre-defined boundary. The systems and methods include an automated process for creating...
2016/0153274 FRACTURING FLUID FOR SUBTERRANEAN FORMATIONS
A method of fracturing a reservoir comprising the steps of pumping a geopolymer precursor fluid through a wellbore into the reservoir at a fracture pressure,...
2016/0153273 WELLBORE SERVICING MATERIALS AND METHODS OF MAKING AND USING SAME
A method of servicing a wellbore in a subterranean formation comprising placing in the wellbore and/or subterranean formation a pad fluid and forming a...
2016/0153272 CASINGS FOR USE IN A SYSTEM FOR FRACTURING ROCK WITHIN A BORE
In disclosed explosive units for use in a wellbore, the casing can include a tubular outer body comprising grooves, pockets, or other variances in thickness...
2016/0153271 MULTI-STAGE GEOLOGIC FRACTURING
Explosive geologic fracturing methods, devices, and systems can be used in combination with other geologic fracturing means, such as hydraulic fracturing...
2016/0153270 SOLVENTS AND NON-CONDENSABLE GAS COINJECTION
Producing hydrocarbons by steam assisted gravity drainage, more particularly, utilizing conventional horizontal wellpair configuration of SAGD in conjunction...
2016/0153269 Production of Methane from Abundant Hydrate Deposits
Methods of dissociating and recovering methane from solid hydrate deposits are provided. A method for recovering methane from a methane hydrate includes at...
2016/0153268 A GAS LIFT SYSTEM AND A GAS LIFT METHOD
The present invention relates to a gas lift system (1) arranged in a well (65) having a top (10) and comprising a well fluid (11), the gas lift system...
2016/0153267 Jet Perforating Device for Creating a Wide Diameter Perforation
An explosive charge assembly comprises a housing, a liner disposed on a face of an explosive charge, an opening through the liner disposed at the apex, and a...
2016/0153266 OILFIELD-WIDE PRODUCTION OPTIMIZATION
A method, apparatus, and computer readable storage medium perform oilfield-wide optimization in a field with a plurality of wells, with each well including a...
2016/0153265 ALGORITHM FOR OPTIMAL ICD CONFIGURATION USING A COUPLED WELLBORE-RESERVOIR MODEL
The disclosed embodiments include a method, apparatus, and computer program product for improving production of an oil well. For example, one disclosed...
2016/0153264 SAFETY DEVICE FOR RETRIEVING COMPONENT WITHIN WELLHEAD
A system is provided that include a safety device configured to mount in a mineral extraction system and block axial movement of a plug in the mineral...
2016/0153263 SAND CONTROL ASSEMBLIES INCLUDING FLOW RATE REGULATORS
A sand control completion system comprises: (A) a first flow rate regulator, wherein the first flow rate regulator is positioned in a first interval of a...
2016/0153262 HYDRAULIC FLOW RESTRICTION TUBE TIME DELAY SYSTEM AND METHOD
A hydraulic time delay system and method in a wellbore tool is disclosed. The system/method includes an actuation mechanism which allows pressure to act on a...
2016/0153261 SANITARY CHECK VALVE TO PREVENT WELL CONTAMINATION
A sanitary check valve arranged between a drop and outlet pipes in a water well casing that will prevent operate to block a back flow of water through the drop...
2016/0153260 METHOD AND APPARATUS FOR ZONAL ISOLATION OF SUBTERRANEAN FORMATIONS USING SET-ON-DEMAND SLURRIES
Methods are disclosed for providing zonal isolation of subterranian formations. One embodiment may include mixing a dry blended material with water at a...
2016/0153259 CONTROL LINE TERMINATION ASSEMBLY
A system includes a control block configured to be coupled to a tree of a wellhead assembly. The control block includes a housing and a plate supported by the...
2016/0153258 Apparatus and Method to Contain Flange, Pipe and Valve Leaks
A system and method for sealing around a fluid flow member includes a ram closing assembly. The ram closing assembly has a sealing chamber having a generally...
2016/0153257 SUBSEA CONNECTION
The present invention provides a subsea connection comprising an umbilical termination head (1) comprising a housing (23) and at least one connecting line (4),...
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