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Patent # Description
2016/0208725 Internal-Combustion-Engine Fuel Injection Control Device
An internal-combustion-engine fuel injection control device which can accurately control a boosted voltage applied to a fuel injection valve during fuel...
2016/0208724 METHOD OF ENERGIZING A SOLENOIDAL FUEL INJECTOR FOR AN INTERNAL COMBUSTION ENGINE
A method and apparatus for energizing a solenoidal fuel injector for an internal combustion engine is disclosed. The fuel injector is electrically connected to...
2016/0208723 SYSTEM AND PROCESS FOR PREDICTING AND PREVENTING PRE-IGNITION
A process and a system for preventing pre-ignition in an internal combustion engine (ICE). The process includes providing an ICE that has a combustion chamber...
2016/0208722 METHOD FOR CONTROLLING A COMBUSTION ENGINE TO DECELERATE A VEHICLE
A method and vehicle embodying the method are provided for deceleration of a vehicle comprising a combustion engine comprising at least one cylinder to which...
2016/0208721 CONTROL APPARATUS AND CONTROL METHOD FOR INTERNAL COMBUSTION ENGINE
A control apparatus for an internal combustion engine having a limiting current sensor includes an electronic control unit. The electronic control unit is...
2016/0208720 CONTROL APPARATUS FOR SPARK-IGNITION INTERNAL COMBUSTION ENGINE
When a catalyst of an internal combustion engine is not activated, a control apparatus retards the ignition timing of a spark plug, and thereby, executes a...
2016/0208719 CONTROL DEVICE FOR VEHICULAR HYDRAULIC PRESSURE SUPPLY DEVICE
A control device for a vehicular hydraulic pressure supply device that controls the vehicular hydraulic pressure supply device provided with a mechanical oil...
2016/0208718 METHOD AND APPARATUS TO STABILIZE ENGINE STATE SELECTION USING AN ENERGY BASED STABILIZATION STRATEGY FOR...
A method for controlling operation of a multi-mode powertrain system includes periodically determining a power cost difference between a first power cost and a...
2016/0208717 SYSTEM AND METHOD FOR LOAD POWER MANAGEMENT IN A TURBOSHAFT GAS TURBINE ENGINE
A control system for a gas turbine engine including a power turbine is disclosed. The control system may also include an outer loop control module to determine...
2016/0208716 METHOD FOR DETECTING A FAULT, FAULT DETECTION SYSTEM AND GAS TURBINE ENGINE
A method for detecting a fault in a gas supply system for a gas turbine engine. The method comprises: measuring a pressure difference between two gas supplying...
2016/0208715 TURBOMACHINE FLOW DIVERTING DEVICE AND METHOD
An example turbomachine exhaust flow diverting assembly includes an upstream flow diverter disposed about a rotational axis of a turbomachine, and a downstream...
2016/0208714 GAS TURBINE ENGINE AND BLOCKER DOOR ASSEMBLY
A blocker door assembly which may be for a cooling system that may be applied to a gas turbine engine includes a plurality of blocker doors circumferentially...
2016/0208713 GAS TURBINE ENGINE WITH HIGH SPEED AND TEMPERATURE SPOOL COOLING SYSTEM
A gas turbine engine includes a turbine section that includes a turbine rotor arranged in a plenum. A compressor section includes a compressor rotor assembly...
2016/0208712 GAS TURBINE ENGINE CONTROL FOR ROTOR BORE HEATING
A gas turbine engine comprises a compressor rotor including blades and a disk, with a bore defined radially inwardly of the disk, and a combustor. A tap...
2016/0208711 COMPUTER-AIDED CONTROL AND/OR REGULATION OF A TECHNICAL SYSTEM
The embodiments relate to a method for the computer-aided control and/or regulation of a technical system, particularly a power generation installation. The...
2016/0208710 MULTI-STAGE INTER SHAFT RING SEAL
Aspects of the disclosure are directed to a system comprising: a first seal that includes a notch configured to avoid an adjacent seal plate radius edge and a...
2016/0208709 METHOD FOR STARTING AIRCRAFT ENGINES
A method of starting an aircraft having at least a first starter/generator (S/G) and a second S/G using at least one inverter/converter and at least one of an...
2016/0208708 FUEL/OIL MANIFOLD
A fuel/oil manifold includes first and second manifold flanges and a manifold tube. The first and second manifold flanges are located in non-parallel planes...
2016/0208707 CONDUIT ASSEMBLY AND METHOD OF UTILIZATION
A conduit assembly and method of utilizing the assembly generally extends along a centerline for detachable engagement to a component in an axial direction....
2016/0208706 V-BAND CLAMP WITH INTEGRAL MOUNT PLATE
A V-band clamp includes a V-band segment that has a V-groove and is configured to generally circumscribe a flange of a first component and a flange of a second...
2016/0208705 BORE-COOLED FILM DISPENSING PEDESTALS
A cooling circuit for a gas turbine engine comprises a first wall having a first surface facing a first cavity and a second surface facing away from the first...
2016/0208704 ANGLED COMBUSTOR LINER COOLING HOLES THROUGH TRANSVERSE STRUCTURE WITHIN A GAS TURBINE ENGINE COMBUSTOR
A wall assembly for use in a combustor of a gas turbine engine includes a transverse structure with at least one effusion passage that extends at an angle a...
2016/0208703 OVERCOOLED AIR COOLING SYSTEM WITH ANNULAR MIXING PASSAGE
A cooling system is provided. The cooling system may comprise a heat exchanger and a first conduit fluidly coupled to an outlet of the heat exchanger. An...
2016/0208702 PNEUMATIC ACTUATOR LOW FLOW SERVO VALVE
A valve system includes a valve for controlling flow of a fluid and a valve controller for providing fluid to control the movement of a valve actuator. The...
2016/0208701 COOLING PASSAGES FOR A MID-TURBINE FRAME
A gas turbine engine includes a mid-turbine frame that includes an inner frame case. At least one spoke is connected to the inner frame case. At least one...
2016/0208700 HYDROCARBON FILM PROTECTED REFRACTORY CARBIDE COMPONENTS AND USE
A turbine power generation system with enhanced stabilization of refractory carbides provided by hydrocarbon from high carbon activity gases is disclosed. The...
2016/0208699 COOLING PASSAGES FOR A MID-TURBINE FRAME
A mid-turbine frame includes an inner frame case including a fluid passage. At least one hollow spoke is attached to the inner frame case. At least one hollow...
2016/0208698 GAS TURBINE ENGINE THERMAL MANAGEMENT SYSTEM
The present disclosure provides systems and methods related to thermal management systems for gas turbine engines. For example, a thermal management system...
2016/0208697 MID-TURBINE FRAME BUFFER SYSTEM
A mid-turbine frame buffer system for a gas turbine engine includes a mid-turbine frame that supports a shaft by a bearing. An air compartment and a bearing...
2016/0208696 SYSTEMS AND METHODS FOR LOAD DIVERSION AROUND LOAD SENSITIVE PARTS
In various embodiments, a lubricating shaft assembly may comprise a shaft, a front seal, a front seat, an inner race, a spacer, a lubricating fitting and a...
2016/0208695 GAS TURBINE ENGINE INLET
In or for an aircraft turbine engine, the invention comprises a fitting comprising at least one blade, said blade being elongate and being adapted to be...
2016/0208694 COOLING DEVICE FOR ELECTRO-PNEUMATIC CONTROLLER
A valve system includes a valve, a valve controller, and a heat exchanger. The valve is configured to open and close a control device in response to a working...
2016/0208693 POWER PLANT HAVING A GAS TURBINE AND A HYDROGEN-COOLED GENERATOR
A power station having a gas turbine, a generator driven by the gas turbine for generation of electrical power, and a hydrogen cooling circuit for discharging...
2016/0208692 GAS TURBINE ENGINE WITH A MULTI-SPOOL DRIVEN FAN
A gas turbine engine includes low and high spools constructed and arranged to rotate about an engine axis. The low spool drives at least one leading stage of a...
2016/0208691 TURBINE ENGINE WITH BOUNDARY LAYER TURBINE
A turbine engine is disclosed herein. The turbine engine includes a compressor section operable to compress fluid. The turbine engine also includes a combustor...
2016/0208690 GAS TURBINE ENGINE SPLIT TORQUE FAN DRIVE GEAR SYSTEM
A gas turbine engine includes a turbine section configured to rotate about an engine axis relative to an engine static structure. A fan section is configured...
2016/0208689 Modifying a Gas Turbine Engine to Use a High Pressure Compressor as a Low Pressure Compressor
A method comprises the steps of modifying an existing engine which includes a high pressure compressor driven by a high pressure turbine and a low pressure...
2016/0208688 INFLOW RADIAL TURBINE WITH REDUCED BORE STRESS CONCENTRATION
A gas turbine engine is provided comprising an impeller configured to rotate about an axis. A combustor is in fluid communication with the impeller. An inflow...
2016/0208687 MULTI-LINK PISTON-CRANK MECHANISM FOR INTERNAL COMBUSTION ENGINE
A lower link (13) is formed such that outer circumferential sides of both end portions of a crankpin through-hole (21) are stiffer than a center portion of the...
2016/0208686 ENERGY STORAGE AND CONVERSION IN FREE-PISTON COMBUSTION ENGINES
Various embodiments of the present disclosure are directed towards free-piston combustion engines. As described herein, a driver section may be provided in a...
2016/0208685 PORTABLE ENGINE-DRIVEN WORKING MACHINE
A portable engine-driven working machine has an engine unit and a cover enclosing the engine unit. The engine unit includes a cylinder block, an electronically...
2016/0208684 MOTIVE-POWER TRANSMISSION DEVICE FOR SUPERCHARGER
A planetary gear device for a motorcycle transmits a power of a reciprocating combustion engine to a supercharger. The supercharger pressurizes intake air for...
2016/0208683 SUPERCHARGER FOR ENGINE
A supercharger is driven by a rotational force of a crankshaft of a combustion engine via a chain. The supercharger includes: a supercharger rotation shaft to...
2016/0208682 ROTARY UNIT OF SUPERCHARGER FOR ENGINE AND BALANCE ADJUSTMENT METHOD THEREOF
A rotary unit is rotatably accommodated within a supercharger casing of a supercharger for pressurizing an intake air of an engine. The rotary unit includes a...
2016/0208681 DUAL WASTEGATE ACTUATION
Various systems and methods for controlling dual wastegates via a single wastegate actuator are provided. In one example, a system comprises a first wastegate...
2016/0208680 EXHAUST CONTROL VALVE BRANCH COMMUNICATION AND WASTEGATE
Methods and systems for adjusting a branch communication and wastegate valve in a dual scroll turbocharger system are provided. In one example, a method may...
2016/0208679 Gas Engine
A gas engine includes a mixing unit for mixing two gas components, which are fed to one or more combustion chambers of the gas engine, in particular for mixing...
2016/0208678 DEGAS BOTTLE HAVING CENTRIFUGAL AIR SEPARATOR FOR USE IN ENGINE COOLING SYSTEM
A degas bottle for inducing a cyclonic direction of flow to incoming coolant is disclosed. The degas bottle includes a body and an air separator having a...
2016/0208677 THERMOSTAT HOUSING FOR A THERMOSTAT OF AN ENGINE COOLING ARRANGEMENT
A housing for a thermostat includes a body, a cavity, at least one director member and at least one retainer member. The body defines an enclosure that...
2016/0208676 TEMPERATURE CONTROL APPARATUS AND METHOD FOR AN AUTOMOTIVE COOLING SYSTEM
A system for regulating a flow of liquid coolant in an automotive cooling system includes a valve body having an inlet and an outlet. A pressure operated valve...
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