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Patent # Description
2016/0273421 OIL PUMP DRIVING CONTROL APPARATUS
The oil pump driving control apparatus includes an internal combustion engine driving source transmitting a driving force of an internal combustion engine to...
2016/0273420 HYDRAULIC VALVE DRIVE OF AN INTERNAL COMBUSTION ENGINE
A hydraulic valve brake for a hydraulic valve drive of an internal combustion engine is provided. The valve brake includes a housing with a housing wall and...
2016/0273419 SELF-LUBRICATING SEALED VALVE GUIDE
A valve system is disclosed, which may comprise a valve including a stem, the stem being oriented along a valve axis. Further, a valve guide may be disposed...
2016/0273418 Single Crystal Engine Valve
A valve for use in an internal combustion engine is disclosed. The valve includes a stem friction welded to a head portion. The head portion is cast from a...
2016/0273417 VALVE TIMING CONTROL DEVICE FOR INTERNAL COMBUSTION ENGINE
A front plate for a valve timing control device is produced which comprises a plate part that closes a front opening of a housing body to seal operation oil...
2016/0273416 VALVE ACTUATION SYSTEM HAVING ROCKER-LOCATED HYDRAULIC RESERVOIR
A valve actuation system is disclosed for an engine. The system may have at least one gas exchange valve, a rocker shaft, a camshaft, a rocker arm connected to...
2016/0273415 VALVE ACTUATION SYSTEM HAVING GROOVED ADJUSTING SCREW
A valve actuation system is disclosed for an internal combustion engine. The system may have a gas exchange valve, a rocker arm pivotally connected to a shaft,...
2016/0273414 VALVE MECHANISM FOR INTERNAL COMBUSTION ENGINE
A valve mechanism includes: a support shaft immovably fixed to a main body of an internal combustion engine, a main arm swingably supported by the support...
2016/0273413 VALVE ACTUATING DEVICE AND METHOD OF MAKING SAME
Tools and methods for indenting and assembling a switching rocker arm assembly having an inner arm, an outer arm and a latch. The tools and methods are...
2016/0273412 VARIABLE VALVE APPARATUS FOR INTERNAL COMBUSTION ENGINE
A variable valve apparatus for an internal combustion engine according to the present invention comprises a cam base member rotating with rotation of a...
2016/0273411 CAMSHAFT, CAM ANGLE DETECTION DEVICE, AND INTERNAL COMBUSTION ENGINE
A camshaft includes a sensor rotor and a plurality of cams. The sensor rotor includes a base circle, and a projection portion formed on an outer peripheral...
2016/0273410 THERMAL POWER PLANT WITH USE OF THE WASTE HEAT FROM A GENERATOR
A thermal power plant with a generator, includes a cooling system for the generator, wherein the waste heat released from the generator on cooling can be used...
2016/0273409 POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS AIR FLOW AND TURBO-EXPANDER FOR SUPPLEMENTAL GENERATOR
A power generation system may include a gas turbine system including a turbine component, an integral compressor and a combustor to which air from the integral...
2016/0273408 POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS AIR FLOW AND EDUCTOR FOR AUGMENTING SAME
A power generation system may include a gas turbine system including a turbine component, an integral compressor and a combustor to which air from the integral...
2016/0273407 POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS AIR FLOW AND BURNER MODULE THEREFOR
A power generation system may include a gas turbine system including a turbine component, an integral compressor and a combustor to which air from the integral...
2016/0273406 COMBINED CYCLE SYSTEM
A combined cycle system where steam discharged from a water separation unit is routed through a high pressure outlet line to a set of super-heaters and...
2016/0273405 METHOD AND PLANT FOR CO-GENERATION OF HEAT AND POWER
A method of operating a combined heat and power plant (10) (CHP plant) includes generating hot flue gas and cooling the hot flue gas in a sequence of cooling...
2016/0273404 POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS AIR FLOW AND TURBO-EXPANDER USING SAME
A power generation system may include a generator, and a gas turbine system for powering the generator, the gas turbine system including a turbine component,...
2016/0273403 POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS AIR FLOW AND TURBO-EXPANDER USING SAME
A power generation system may include a generator, and a gas turbine system for powering the generator, the gas turbine system including a turbine component,...
2016/0273402 POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS GAS FLOW FOR SUPPLEMENTAL GAS TURBINE SYSTEM
A power generation system may include a generator; a gas turbine system for powering the generator, the gas turbine system including a turbine component, an...
2016/0273401 POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS AIR FLOW AND EDUCTOR FOR PROCESS AIR DEMAND
A power generation system may include a gas turbine system including a first turbine component, an integral compressor and a combustor to which air from the...
2016/0273400 POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS AIR FLOW AND TURBO-EXPANDER TO INCREASE TURBINE...
A power generation system may include: a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to...
2016/0273399 POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS AIR FLOW AND TURBO-EXPANDER FOR COOLING INLET AIR
A power generation system may include: a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to...
2016/0273398 POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS AIR FLOW AND STORAGE VESSEL FOR AUGMENTING EXCESS AIR...
A power generation system includes: a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to which...
2016/0273397 POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS AIR FLOW AND SUPPLEMENTAL COMPRESSOR THEREFOR
A power generation system includes: a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to which...
2016/0273396 POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS AIR FLOW AND HEAT EXCHANGER THEREFOR
A power generation system includes: a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to which...
2016/0273395 POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS AIR FLOW AND COOLING FLUID INJECTION THEREFOR
A power generation system includes: a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to which...
2016/0273394 POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS AIR FLOW AND EDUCTOR AUGMENTATION
A power generation system includes: a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to which...
2016/0273393 POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS AIR FLOW
A power generation system includes: a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to which...
2016/0273392 COMBINED CYCLE COMBUSTION ENGINE PROCESS AND COMBINED CYCLE COMBUSTION ENGINE
The invention describes an Otto cycle or Diesel cycle internal combustion engine assembled with an energy and water recovery systems to Rankine cycle. In the...
2016/0273391 COATED COOLING PASSAGE
A component for a gas turbine engine includes a substrate with a substrate aperture and a coating on the substrate that extends a length of the substrate...
2016/0273390 EXHAUST GAS LINER FOR A GAS TURBINE AND GAS TURBINE WITH SUCH AN EXHAUST GAS LINER
An exhaust gas liner for a gas turbine includes an annular inner shell and an annular outer shell, which are arranged concentrically around a machine axis of...
2016/0273389 OIL TANK MOUNT ARRANGEMENT ON A GEARED TURBOFAN ENGINE
An oil tank mounting system for use on a structure of a turbine engine, includes three mounts with each mount configured to constrain the oil tank with a...
2016/0273388 SHEET-METAL TURBINE HOUSING
An object is to provide a sheet-metal turbine housing reinforced by a readily-manufacturable structure, the sheet-metal turbine housing also having a small...
2016/0273387 Method for Producing a Component
A method for producing a component, particularly a component of a turbomachine, is disclosed. In an embodiment, the method includes the following process...
2016/0273386 ZERO OR LOW LEAKAGE OIL TRANSFER BEARING
What is described is a transfer bearing assembly configured to allow a flow of a fluid from an inlet tube to a channel defined by a rotating shaft. The...
2016/0273385 FAN DRIVE GEAR SYSTEM MANIFOLD RADIAL TUBE FILTERS
A lubrication system for gas turbine engine includes a main lubricant passage for providing lubricant from a lubricant supply to a lubricant manifold. The...
2016/0273384 COOLING PASSAGES FOR A MID-TURBINE FRAME
A spoke for a mid-turbine frame on a gas turbine engine includes a cylindrical portion. A flange is attached to the cylindrical portion. At least one gusset...
2016/0273383 COOLING PASSAGES FOR A MID-TURBINE FRAME
A mid-turbine frame for a gas turbine engine includes an inner frame case. A bearing support member is located adjacent the inner frame case. At least one...
2016/0273382 SYSTEM FOR COOLING A TURBINE SHROUD
In one aspect the present subject matter is directed to a system for cooling a turbine shroud. The system includes a cooling medium source that provides a...
2016/0273381 INTEGRATED WASHING SYSTEM FOR GAS TURBINE ENGINE
A washing system is described for a gas turbine engine with an axial compressor, comprising: an inlet screen at the air flow inlet of the compressor to protect...
2016/0273380 PROTECTIVE DEVICE FOR A TURBOMACHINE
A protective device (10) for a turbomachine, in particular a gas turbine, having a containment ring (12) which is disposed on the radially inner side of a...
2016/0273379 GAS TURBINE ENGINE HEALTH DETERMINATION
A method is provided for determining an updated engine health factor of an aircraft engine. The method includes determining an engine health condition...
2016/0273378 VARIABLE VANE CONTROL SYSTEM
A variable vane control system for controlling the angle of rotation of a circumferential row of variable vanes of a gas turbine engine. The control system...
2016/0273377 PART LOAD PERFORMANCE IMPROVEMENT USING DEFORMABLE BOREPLUGS
A cooling arrangement for a gas turbine engine includes a discharge channel for airflow from a compressor, a first cooling channel, and at least one aperture...
2016/0273376 TAILORED THERMAL CONTROL SYSTEM FOR GAS TURBINE ENGINE BLADE OUTER AIR SEAL ARRAY
A clearance control ring for a clearance control system of a gas turbine engine includes a contoured radial outer portion that defines a multiple of fins and a...
2016/0273375 RADIAL SEAL WITH OFFSET RELIEF CUT
A seal assembly for a turbine engine is disclosed and includes a fixed housing including an axial surface defining an inner diameter and an annular seal that...
2016/0273374 SEAL ASSEMBLY IN A GAS TURBINE ENGINE
A gas turbine engine seal assembly (160) including: a rigid seal (58) cooperatively configured with a structure (14, 42) of a gas turbine engine to define a...
2016/0273373 MULTI-ELEMENT INNER SHROUD EXTENSION FOR A TURBO-MACHINE
A turbine engine is disclosed and includes an airflow passage including an inner surface defined by a main shroud and a shroud extension. A flow splitter is...
2016/0273372 FIBER PREFORM FOR A HOLLOW TURBINE ENGINE VANE
A fiber preform for a hollow turbine engine vane, the preform including a main fiber structure obtained by three-dimensional weaving and including at least one...
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