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Patent # Description
2016/0230689 CONTROL APPARATUS OF INTERNAL COMBUSTION ENGINE
The invention relates to a control apparatus of an engine. The apparatus carries out a minute-injection for injecting a minute amount of a fuel so as not to...
2016/0230688 ENGINE CONTROL DEVICE
An engine control device includes an engine failure determination unit and a rotation rate control unit. The engine failure determination unit determines...
2016/0230687 ABNORMALITY DIAGNOSIS APPARATUS AND ABNORMALITY DIAGNOSIS METHOD
An abnormality diagnosis apparatus is an apparatus that diagnoses a fuel leak from a fuel passage to circulate a liquefied gas fuel between a fuel tank and an...
2016/0230686 GAS SENSOR CONTROL DEVICE
An O.sub.2 sensor includes a sensor element using a solid electrolyte layer and a pair of electrodes placed at a position to interpose the solid electrolyte...
2016/0230685 METHOD AND APPARATUS FOR REGENERATING A LEAN NOx TRAP IN A TURBOCHARGED INTERNAL COMBUSTION ENGINE
A method and apparatus for regenerating a Lean NOx Trap in an internal combustion engine is disclosed. The internal combustion engine includes a Lean NOx Trap,...
2016/0230684 SYSTEM AND METHODS FOR OPERATING AN EXHAUST GAS RECIRCULATION VALVE BASED ON A TEMPERATURE DIFFERENCE OF THE VALVE
Methods and systems are provided for determining changes in a flow area of an exhaust gas recirculation (EGR) valve for EGR flow estimates due to a change in...
2016/0230683 SYSTEM AND METHODS FOR DIAGNOSING SOOT ACCUMULATION ON AN EXHAUST GAS RECIRCULATION VALVE
Methods and systems are provided for determining changes in a flow area of an exhaust gas recirculation (EGR) valve for EGR flow estimates due to soot...
2016/0230682 SYSTEM AND METHODS FOR ADJUSTING AN EXHAUST GAS RECIRCULATION VALVE BASED ON MULTIPLE SENSOR OUTPUTS
Methods and systems are provided for adjusting an exhaust gas recirculation (EGR) valve based on a final EGR estimate. In one example, a method may include...
2016/0230681 CONTROL SYSTEM OF ENGINE
A control system of an engine in which a purge gas containing evaporated fuel desorbed from a canister is supplied to an intake passage of the engine is...
2016/0230680 ENGINE SPEED CONTROL VIA ALTERNATOR LOAD SHEDDING
Method and systems are provided for adjusting an engine load exerted on a vehicle engine by an alternator mechanically coupled to said engine. In one example,...
2016/0230679 VARIABLE VALVE OPERATING SYSTEM
A variable valve operating system assembled in an engine includes a first rocker arm contacting with a valve, a second rocker arm no contacting with any valve,...
2016/0230678 CONTROL VALVE WITH ANNULAR POPPET CHECK VALVE
Embodiments of the invention provide a control valve including a control valve body having an inlet passage, an outlet passage, a workport, and a chamber...
2016/0230677 Variable Geometry Gas Turbine Engine For Use In Inclement Weather
A variable-geometry system for a gas turbine engine can be used to improve operations in various inclement weather conditions. This may be achieved by varying...
2016/0230676 Method and Apparatus for Detecting Performance of an APU Fuel Assembly
The present invention relates to a method for detecting performance of an APU fuel assembly, comprising: obtaining APU messages at multiple time points within...
2016/0230675 FAN FLOW CONTROL VALVE
Aspects of the disclosure are directed to an engine of an aircraft. A first duct may be configured to convey a first flow, a second duct may be configured to...
2016/0230674 GEAR REDUCTION FOR LOWER THRUST GEARED TURBOFAN
A gas turbine engine comprises a fan rotor having a hub and a plurality of fan blades extending radially outwardly of the hub. A compressor is positioned...
2016/0230673 SYSTEM AND METHOD FOR LIMITING MOVEMENT OF A RETAINING RING
A method of installing a retaining ring assembly in a turbine case is provided. The method may include installing a blade outer air seal into a case before...
2016/0230672 SYSTEM AND METHOD FOR EMERGENCY STARTING OF AN AIRCRAFT TURBOMACHINE
The invention relates to an emergency start system (20) for a turbine engine of an aircraft, characterised in that it comprises at least one solid-propellant...
2016/0230671 TURBOMACHINE DESIGNED TO OPERATE IN TURNING GEAR MODE
A field of turbine engines, and more particularly to an engine including a compressor; a combustion chamber; a first turbine connected to the compressor by a...
2016/0230670 RUPTURE CONSTRAINT MECHANISM
Apparatus and system for containing a rupture of a duct. The apparatus includes an air-permeable sheet, such as a wide-weave fiberglass sheet. The...
2016/0230669 AIRCRAFT SYSTEM WITH FUEL-TO-FUEL HEAT EXCHANGER
An aircraft system is provided that includes a fuel reservoir, a turbine engine and a fuel-to-fuel heat exchanger. The heat exchanger is fluidly coupled...
2016/0230668 FUEL INJECTION DEVICE FOR A GAS TURBINE
A fuel injection device for a gas turbine, including a plurality of streamlined bodies arranged in a ring adjacent to one another in a circumferential...
2016/0230667 ACCUMULATOR ASSISTED GAS TURBINE ENGINE START SYSTEM AND METHODS THEREFOR
A gas turbine engine assembly is provided having a gas turbine engine and a fuel supply in flow communication with the gas turbine engine. An accumulator is...
2016/0230666 ORIENTATION FEATURE FOR SWIRLER TUBE
A cooling structure for a gas turbine engine comprises a gas turbine engine structure defining a cooling cavity. A cooling component is configured to direct...
2016/0230665 TURBOCOOLED VANE OF A GAS TURBINE ENGINE
The present invention discloses a novel apparatus and methods for augmenting the power of a gas turbine engine, improving gas turbine engine operational...
2016/0230664 PEDESTALS WITH HEAT TRANSFER AUGMENTER
A gas turbine engine component comprises a first side wall, and a second side wall spaced apart from the first side wall. At least one internal cooling channel...
2016/0230663 GAS TURBINE, GAS-TURBINE CONTROL DEVICE, AND GAS TURBINE OPERATION METHOD
A gas turbine equipped with a compressor, a combustion chamber and a turbine is further equipped with: a pressurizing device for taking a portion of the...
2016/0230662 GAS TURBINE ENGINE COMPONENT WITH VASCULAR COOLING SCHEME
A component according to an exemplary aspect of the present disclosure includes, among other things, a body portion and a cooling scheme disposed inside the...
2016/0230661 GAS TURBINE ENGINE HAVING SECTION WITH THERMALLY ISOLATED AREA
A gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a first compressor having a first overall...
2016/0230660 GAS TURBINE POWER GENERATOR WITH TWO-STAGE INLET AIR COOLING
The gas turbine power generator with two-stage inlet air cooling is a gas turbine power plant for generating electrical power, where air fed into an inlet of a...
2016/0230659 Method for Monitoring Performance of the Lubricant Cooler in Aircraft Auxiliary Power Unit
The present invention relates to a method for detecting performance of the lubricant cooler in aircraft auxiliary power unit APU, comprising: acquiring...
2016/0230658 GAS TURBINE ENGINE AND AN AIRFLOW CONTROL SYSTEM
A gas turbine engine includes a core flowpath for flowing a core stream, a second flowpath located radially outward from the core flowpath for flowing a second...
2016/0230657 MICRO GAS TURBINE SYSTEMS AND USES THEREOF
The present disclosure describes a micro gas turbine flameless heater, in which the heat is generated by burning fuel in a gas turbine engine, and the heater...
2016/0230656 EXHAUST MIXER FOR WAVE ROTOR ASSEMBLY
A wave rotor assembly includes a wave rotor combustor and an exit duct. The wave rotor combustor includes an aft plate formed to include an exit port and a...
2016/0230655 PROTECTION AND SUPPORT FOR VEHICLE ENGINE COMPONENTS
Vehicle engine systems and protectors for such systems are presented. Vehicle engine systems can include one or more engine components associated with an...
2016/0230654 ELECTRICAL POWER GENERATION SYSTEM WITH MULTIPLE PATH COOLING
A genset has an enclosure in which a bulkhead separates the enclosure into a high pressure compartment and a low pressure compartment. A first fan is located...
2016/0230653 INTERNAL COMBUSTION ENGINES
An internal combustion engine includes a combustion chamber. The chamber includes a body that is movable in the chamber to vary the chamber volume and contains...
2016/0230652 IMPLOSION ENABLED ENGINE OF EXOTHERMIC TYPE IN EXPLOSIVE SYSTEM (IEEX-EX) EMPLOYING A SAFE PIPE SYSTEM (SPS)...
The present subject matter discloses the concept of multiple engine heads for one cylinder operating as Serially Operating Internal Combustion (SOIC) engine...
2016/0230651 CONTROLLING TURBOCHARGER COMPRESSOR CHOKE
A radial flow compressor includes a device (1, 34) for controlling air flow detachment from the volute tongue (3). The device (1, 34) may include a vane (1) or...
2016/0230650 PASSIVE AND SEMI-PASSIVE INLET-ADJUSTMENT MECHANISMS FOR COMPRESSOR, AND TURBOCHARGER HAVING SAME
A centrifugal compressor for a turbocharger includes a passive or semi-passive inlet-adjustment mechanism in an air inlet for the compressor, operable to move...
2016/0230649 INTERNAL COMBUSTION ENGINE WITH TURBINE
Methods and systems are provided for controlling a turbine within an internal combustion engine. In one example, a turbine system within an internal combustion...
2016/0230648 METHODS AND SYSTEMS FOR BOOST CONTROL
Methods and systems are provided for adjusting operation of an electric motor coupled to a compressor at high altitude engine operation. In one example, the...
2016/0230647 PISTON FOR PRECHAMBER-TYPE GAS ENGINE AND PRECHAMBER-TYPE GAS ENGINE
Particular embodiments may provide a piston for a prechamber-type gas engine and a prechamber-type gas engine taking into consideration the shape of the piston...
2016/0230646 Combustion System, Nozzle for Prechamber Assembly, and Method of Making Same
A nozzle for a prechamber assembly of an engine includes a hollow nozzle body having an outer surface, defining first and second outer openings, and an inner...
2016/0230645 INTERNAL COMBUSTION ENGINE
An internal combustion engine includes a pre-chamber. In another aspect, pressure within a pre-chamber is equal to or greater than pressure within a main...
2016/0230644 COOLING SYSTEM DIAGNOSTIC METHOD
A method for operating an engine cooling system is provided. The method includes monitoring a coolant temperature profile after engine shut-down and indicating...
2016/0230643 ENGINE COOLING SYSTEM
An engine cooling system decreases vehicle weight caused by employing a Rankine cycle, makes it possible to improve the performance of the Rankine cycle, and...
2016/0230642 METHOD OF CONTROLLING A COOLING CIRCUIT OF AN INTERNAL COMBUSTION ENGINE
A method of operating a cooling circuit of an internal combustion engine is disclosed. The engine is equipped with an engine head, and the cooling circuit...
2016/0230641 ENGINE COOLING SYSTEM
An engine cooling system, capable of reducing vehicle weight caused by employing a Rankine cycle and capable of improving Rankine cycle performance, including...
2016/0230640 ENGINE OIL SUPPLY APPARATUS
An engine oil supply apparatus includes: a cylinder block; a shaft supporting member which bears a crank journal of a crank shaft in cooperation with a journal...
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