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Patent # Description
2017/0101926 ROTARY COMBUSTION ENGINE SYSTEM HAVING TOROIDAL COMPRESSION AND EXPANSION CHAMBERS
A rotary combustion engine system is provided with compression unit and expansions unit offset which communicate through a transfer port. Each unit defines a...
2017/0101925 MULTI-STAGE TURBOCHARGER SYSTEM
A turbocharger system comprises a first relatively small high-pressure (HP) turbocharger and a second relatively large low pressure (LP) turbocharger. The...
2017/0101924 COMPRESSOR RECIRCULATION VALVE WITH NOISE-SUPPRESSING MUFFLER
A compressor recirculation valve having a noise-suppressing muffler. The muffler has a double-walled construction, including a perforated outer wall and a...
2017/0101923 MULTIPLE PRECHAMBERS WITH INTERACTING JETS
An internal combustion engine having a main combustion chamber, a first prechamber, a second prechamber, a first ignition plug and a second ignition plug. The...
2017/0101922 PRECHAMBER INSERT FOR AN INTERNAL COMBUSTION ENGINE
In an aspect of the present disclosure, an internal combustion engine is disclosed. The internal combustion engine has a main combustion chamber, a prechamber,...
2017/0101921 SYSTEM AND METHOD FOR OPERATING A PRESSURE-RELIEVING FLUID-METERING VALVE ASSEMBLY
A fluid control system may include a fluid conduit defining a fluid passage, and a fluid metering assembly in fluid communication with the fluid passage. The...
2017/0101920 METHOD OF DETERMINING THE TEMPERATURE OF A CYLINDER HEAD
A method of determining the temperature of an inner section of a cylinder head (204) in an internal combustion engine. The engine comprises: at least one...
2017/0101919 EBULLIENT COOLING DEVICE
An ebullient cooling device includes: an internal combustion engine cooled by boiling a coolant flowing through a coolant passage formed within the internal...
2017/0101918 FAN COOLED IGNITION COIL METHOD AND APPARATUS
This disclosure provides an ignition coil for a spark ignited internal combustion engine. The ignition coil includes a coil body having an outer surface and...
2017/0101917 ENGINE WITH EXPLOSION PROTECTION
The exhaust system of a diesel engine includes components such as a turbocharger and an exhaust manifold which can have very high internal temperatures (e.g.,...
2017/0101916 METHOD FOR OPERATING AN INTERNAL COMBUSTION ENGINE, CONTROL DEVICE AND INTERNAL COMBUSTION ENGINE
A method for operating an internal combustion engine with an exhaust gas after treatment system, which includes at least one particulate filter. The method is...
2017/0101915 AUTOMATICALLY HEATED CATALYTIC CONVERTER
The present invention is based on the application of heating resistors by a temperature regulation circuit in certain points of the catalyzer so that this...
2017/0101914 REMOTE FLUID SUPPLY FOR AN ENGINE
A system includes a first diesel engine operable to drive a first device, a first DEF tank associated with the first engine and operable to provide DEF to the...
2017/0101913 SYSTEM AND METHOD FOR VARYING REDUCTANT DELIVERY PRESSURE TO AFTERTREATMENT SYSTEMS
An aftertreatment system comprises a reductant storage tank and a SCR system including a catalyst for reducing constituents of an exhaust gas. A reductant...
2017/0101912 CRANKCASE BREECH DETECTION FOR BOOSTED ENGINES
Methods for indicating whether a crankcase of an engine is breeched are provided. One example method comprises restricting a communication of the crankcase...
2017/0101911 Fluid Container
A replaceable fluid container arranged to be removably seated in a dock to supply fluid associated with an engine, the replaceable fluid container comprising a...
2017/0101910 Apparatus for providing fine filtration to hydraulic systems and internal combustion engines
The present invention teaches a method and apparatus to quickly and inexpensively implement advanced, bypass grade, fine, or additional filtration to engines...
2017/0101909 CAMSHAFT THRUST BEARING LUBRICATION SYSTEM
Methods and systems are provided for regulating oil flow to advance and retard chambers of a variable cam timing (VCT) system and to a thrust bearing of a...
2017/0101908 LUBRICATING DEVICE FOR ENGINE
The first opening part penetrates the first partition wall that separates the crank chamber and the oil sump chamber. The lubricating device of the engine...
2017/0101907 OIL PUMP SYSTEM FOR VEHICLE
The present disclosure provides an oil pump system for a vehicle to control an oil flow or a flow rate of oil according to characteristics of an oil flow rate...
2017/0101906 VALVE OPERATING APPARATUS FOR INTERNAL COMBUSTION ENGINE
A valve operating apparatus includes: a first intermediate arm and a first rocker arm that are interposed between a first cam unit and a first valve; a second...
2017/0101905 CAMSHAFT ADJUSTING DEVICE
A camshaft adjusting device, wherein said camshaft adjusting device has a lubricant supply unit, wherein the lubricant supply unit has a filter device for...
2017/0101904 CAMSHAFT ADJUSTER
A hydraulic camshaft adjuster of the vane cell type, including a rotor and a stator and including a cover having fastening holes extending all the way through...
2017/0101903 SYSTEM AND METHOD FOR VARIABLE ACTUATION OF A VALVE OF AN INTERNAL-COMBUSTION ENGINE, WITH A DEVICE FOR...
A system for variable actuation of an engine valve of an internal-combustion engine includes a master piston and a slave piston, driven by the master piston. A...
2017/0101902 SYSTEM AND METHOD FOR CAMSHAFT VIBRATION CONTROL
A system includes a camshaft disposed along an axis from a drive end to a opposite end, and the camshaft includes a plurality of journals configured to support...
2017/0101901 METHOD FOR OPERATING A STEAM TURBINE
The invention relates to a method for operating a steam turbine, the steam turbine being accelerated to a nominal speed by a device, such as, for example, a...
2017/0101900 EXHAUST HEAT COLLECTING SYSTEM
In one embodiment, an exhaust heat collecting system of collecting exhaust heat in a fluid treatment system. The fluid treatment system includes a fluid path...
2017/0101899 HEATING SYSTEMS FOR INTERNALLY HEATING ROTOR IN-SITU IN TURBOMACHINES, AND RELATED ROTOR
Heating systems for a rotor in-situ in a turbomachine are provided. In contrast to conventional systems that merely heat from an external turbine casing,...
2017/0101898 HEATING SYSTEMS FOR EXTERNAL SURFACE OF ROTOR IN-SITU IN TURBOMACHINE
Heating systems for a rotor in-situ in a turbomachine are provided. In contrast to conventional systems that merely heat from an external turbine casing,...
2017/0101897 HEATING SYSTEMS FOR ROTOR IN-SITU IN TURBOMACHINES
Heating systems for a rotor in-situ in a turbomachine are provided. In contrast to conventional systems that merely heat from an external turbine casing,...
2017/0101896 TURBINE ENGINE, COMPONENTS, AND METHODS OF COOLING SAME
A centrifugal separator for removing particles from a fluid stream includes an angular velocity increaser configured to increase the angular velocity of a...
2017/0101895 AIRCRAFT PROPULSION ASSEMBLY
The disclosure relates to an aircraft propulsion assembly comprising a bypass turbojet engine equipped with a nacelle, the bypass turbojet engine including a...
2017/0101894 ANGLED IMPINGEMENT INSERT WITH DISCRETE COOLING FEATURES
An engine component assembly is provided for impingement cooling including discrete cooling features. An insert is located opposite and adjacent to a cooled...
2017/0101893 AIRFOIL COOLING WITH INTERNAL CAVITY DISPLACEMENT FEATURES
A turbine airfoil including a central cavity defined by an outer wall including pressure and suction sides extending between and joined at leading and trailing...
2017/0101892 TURBINE NOZZLE WITH COOLING CHANNEL COOLANT DISTRIBUTION PLENUM
A turbine nozzle includes an airfoil that extends in span from an inner band to an outer band where the inner band and the outer band define inner and outer...
2017/0101891 TURBINE NOZZLE WITH COOLING CHANNEL COOLANT DISCHARGE PLENUM
A turbine nozzle includes an airfoil that extends in span from an inner band to an outer band where the inner band and the outer band define inner and outer...
2017/0101890 TURBINE NOZZLE WITH INNER BAND AND OUTER BAND COOLING
A turbine nozzle includes an airfoil that extends in span from an inner band to an outer band where the inner band and the outer band define outer flow...
2017/0101889 MULTI-FLOW COOLING PASSAGE CHAMBER FOR GAS TURBINE ENGINE
A cooling chamber in a gas turbine engine includes a first side surface, a second side surface, a bottom surface, and a top surface defining a chamber therein....
2017/0101888 DE-ICING NOSE FOR LOW-PRESSURE COMPRESSOR OF AN AXIAL TURBINE ENGINE
The invention proposes a de-icing splitter nose at the inlet of the low-pressure compressor of a double-flow turbine engine. The splitter nose comprises an...
2017/0101887 Containment for a Continuous Flow Machine
A containment for a continuous flow machine, in particular for a gas turbine, is disclosed. The containment has at least one annular housing with at least one...
2017/0101886 Disc Cavity Thermocouple Upgrade
An arrangement to prevent thermocouple chafing with a guide tube within a rotor disc cavity during gas turbine operation is provided. The arrangement includes...
2017/0101884 GROUND-PROJECTILE SYSTEM
A Projectile Continuous Power Module (PCMP) is configured to take incoming or oncoming airflow of an inflight projectile and direct the airflow to a turbine...
2017/0101883 VISUAL INDICATOR OF COATING THICKNESS
In some examples, a coating may include at least one feature that facilitates visual determination of a thickness of the coating. For example, the coating may...
2017/0101882 TURBINE SHROUD WITH SEALING FEATURES
A segmented turbine shroud for positioning radially outside of blades of a turbine rotor includes a carrier, a blade track, and retainers. The blade track is...
2017/0101881 GAS TURBINE ENGINE COMPONENTS, BLADE OUTER AIR SEAL ASSEMBLIES, AND BLADE OUTER AIR SEAL SEGMENTS THEREOF
A gas turbine engine component is provided. The gas turbine engine component has an internal cooling passage having first endwall and a second endwall. A...
2017/0101880 FABRIC SEAL AND ASSEMBLY FOR GAS TURBINE ENGINE
A vane assembly for a gas turbine engine is disclosed in this paper. The vane assembly includes an inner platform, an outer platform, and a ceramic-containing...
2017/0101879 INTERSHAFT SEAL WITH DUAL OPPOSING CARBON SEAL RINGS
An intershaft seal assembly including first and second or forward and aft carbon face seal rings supported on an annular housing and having first and second...
2017/0101878 LOW MODULUS INSERT FOR A COMPONENT OF A GAS TURBINE ENGINE
A gas turbine engine including a component having a first and a second component that are attached or integrally formed with each other. The first and the...
2017/0101877 VARIABLE PITCH FAN BLADE RETENTION SYSTEM
A variable pitch fan for a gas turbine engine includes a fan blade defining a pitch axis and attached at a radially inner end to a trunnion mechanism. The...
2017/0101876 FAN PLATFORM FOR A GAS TURBINE ENGINE
A gas turbine including a fan platform positioned between adjacent fan blades of a fan of the gas turbine engine is provided. The fan platform defines an outer...
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