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Patent # Description
2016/0201607 EFFICIENT, LOW PRESSURE RATIO PROPULSOR FOR GAS TURBINE ENGINES
A gas turbine engine includes a core flow passage, a bypass flow passage, and a propulsor arranged at an inlet of the bypass flow passage and the core flow...
2016/0201606 LOW WEIGHT LARGE FAN GAS TURBINE ENGINE
A gas turbine engine according to an example of the present disclosure includes, among other things, a fan configured to deliver airflow to a bypass passage,...
2016/0201605 ENGINE
There is provided a method for converting a turbofan engine, including the step of providing a turbofan engine and the step of converting the turbofan engine...
2016/0201604 DECOUPLED TRANSLATING SLEEVE
A thrust reverser for a nacelle may include a translating sleeve. A plurality of lint blocker doors may be coupled to the translating sleeve. The translating...
2016/0201603 DEVICE FOR DRIVING ACTUATORS FOR A THRUST REVERSER, SELECTIVELY ALLOWING MOTORISED OR MANUAL DRIVING
The invention relates to a device (3) for driving actuators (7-10) for a thrust reverser, comprising a motorised drive unit (15), a brake (16) and a manual...
2016/0201602 METHODS AND APPARATUS TO VARY REVERSE THRUST OF AIRCRAFT ENGINES
Methods and apparatus to vary reverse thrust of turbofans are disclosed. An example cascade apparatus disclosed herein includes a fixed frame having a...
2016/0201601 METHODS AND APPARATUS TO VARY REVERSE THRUST OF AIRCRAFT ENGINES
Methods and apparatus to vary reverse thrust of aircraft engines are disclosed. An example cascade apparatus disclosed herein includes a cascade frame having a...
2016/0201600 THRUST REVERSER SLIDING DOOR ASSEMBLY
A gas turbine engine assembly has a pylon with a first side and a second side. A first rail is mounted to the first side and a second rail is mounted to the...
2016/0201599 METHOD AND THERMAL ENGINE FOR UTILIZING WASTE HEAT OR GEOTHERMAL HEAT
In a thermal engine for producing an electrical current or mechanical output by actuating a piston by gas under pressure in a cylinder chamber of the thermal...
2016/0201598 ENGINE AND ENGINE OPERATING MACHINE HAVING THE ENGINE
An engine operating machine having a cylinder made of magnesium alloy which is excellent in weight reduction while maintaining durability of the engine is...
2016/0201597 PISTON ASSEMBLY FOR A RECIPROCATING ENGINE
A power cylinder system for a reciprocating engine includes a steel piston configured to move within a cylinder of the reciprocating engine. The system also...
2016/0201596 COMBUSTION CHAMBER STRUCTURE FOR ENGINE
A combustion chamber structure for an engine, wherein the structure includes a piston formed with a downward dented cavity at a central part of an upper...
2016/0201595 Crankcase Ventilation System Geometry Optimization
An internal combustion engine having an oil drain opening connected to an oil drain passage in a cylinder head for simultaneously providing flow of oil to a...
2016/0201594 INTERNAL COMBUSTION ENGINE
A controller is provided that performs first injection that executes fuel injection with lower injection rate and subsequently performs second injection with...
2016/0201593 METHOD AND SYSTEM FOR FUEL INJECTION
Methods and systems are provided for injecting fuel into a combustion chamber of an engine. In one example, a system may include a hollow cone-shaped injector...
2016/0201592 State-Based Diesel Fueling For Improved Transient Response In Dual-Fuel Engine
A method, used with dual-fuel engine, of controlling the amount of diesel fuel delivered to the engine. The method compensates for the poor transient response...
2016/0201591 SYSTEMS AND METHODS FOR DISPLAYING TEST DETAILS OF AN ENGINE CONTROL TEST
A system is provided that includes one or more sensors configured to monitor operating parameters of engine components and a controller. The controller is...
2016/0201590 REMOTE SERVER
At least an embodiment may provide a remote server that can predict overheating of an engine. A remote server may receives an engine rotational speed, an...
2016/0201589 CONTROL DEVICE FOR INTERNAL COMBUSTION ENGINE
A control device for an internal combustion engine includes an electronic control unit configured to switch a control algorithms for a calculation of a command...
2016/0201588 UNIVERSAL CONTROL AND EVALUATION UNIT PARTICULARLY FOR OPERATION OF A LAMBDA PROBE
A control and evaluation unit for the operation and evaluation of at least one sensor, in particular for the operation and evaluation of at least one lambda...
2016/0201587 EXHAUST GAS PURIFICATION SYSTEM AND EXHAUST GAS PURIFICATION METHOD
When a catalyst temperature of a catalyst device is at or below a lower limit air-fuel ratio richness control is prohibited. When a first timing, where an...
2016/0201586 NOISE, VIBRATION AND HARSHNESS REDUCTION IN A SKIP FIRE ENGINE CONTROL SYSTEM
A variety of methods and arrangements for reducing noise, vibration and harshness (NVH) in a skip fire engine control system are described. In one aspect, a...
2016/0201585 Signal Detection For Balancing Cylinders In A Motor Vehicle
The present disclosure teaches method for balancing cylinders in a motor vehicle including an engine which has at least two cylinders. The method may include:...
2016/0201584 METHODS AND SYSTEMS FOR SURGE CONTROL
Methods and systems are provided for calibrating a compressor surge line. In one example, a method may include adjusting the compressor surge line based on a...
2016/0201583 MULTI-CYLINDER OTTO-CYCLE ENGINE AND METHOD FOR OPERATING THE SAME
The disclosure relates to an engine having a cylinder head which is divided into multiple sections which each delimit a combustion chamber of a cylinder of the...
2016/0201582 Prime Mover Control Device for Work Vehicle
A prime mover control device for a work vehicle, includes: a rotation speed control unit that controls a rotation speed of a prime mover in correspondence to...
2016/0201581 THROTTLE BODY FUEL INJECTION SYSTEM WITH IMPROVED FUEL DISTRIBUTION AND IDLE AIR CONTROL
A throttle body fuel injection system and method that is arranged to easily replace four-barrel carburetors includes a throttle body assembly with four main...
2016/0201580 PROPANE FUEL SUPPLEMENT SYSTEM AND METHOD
A propane injection system for supplementing gasoline or diesel engines in vehicles such as automobiles and marine vessels. The invention would also be...
2016/0201579 IGNITION FILTER FOR COMPRESSED AIR ENGINE
A method for controlling an electronically actuated valve is described. An ignition signal for a combustion engine is received. The ignition signal is...
2016/0201578 Electric Air Flow Control Device for Internal Combustion Engines
The purpose of this invention is to achieve an electric air flow control device comprising a motor rotor bearing structure having excellent wear resistance...
2016/0201577 GAS FLOW ADJUSTING DEVICE
A gas flow adjusting device is provided, which includes a tube body, a first horizontal shaft, a second horizontal shaft, two leaf structures, a torsional...
2016/0201576 FLEXURE FOR METERING VALVE ASSEMBLY
A flexure for a metering valve has a flexure body defining a center axis to be aligned with a fuel nozzle. The flexure body includes an outermost peripheral...
2016/0201575 ACTUATOR TO VALVE CALIBRATION OF A FUEL CONTROL VALVE ASSEMBLY
A method for calibrating a fuel control valve assembly including a valve and an actuator is disclosed. The method includes determining an encoder offset by...
2016/0201574 DIRECT METERING USING A VARIABLE DISPLACEMENT VANE PUMP
A direct metering architecture is provided having a metering pump and a servo pump wherein the metering and servo pumps are driven by an engine shaft by way of...
2016/0201573 AUTOMATED TUNING OF GAS TURBINE COMBUSTION SYSTEMS
A system for tuning the operation of a gas turbine is provided based on measuring operational parameters of the turbine and directing adjustment of operational...
2016/0201572 Transient Fault Detection Methods and Systems
The present disclosure provides methods, systems, and computer-readable media for the detection of valve faults based on transient air pressure measurements....
2016/0201571 TURBOMACHINE HAVING A GAS FLOW AEROMECHANIC SYSTEM AND METHOD
A turbomachine including an improved backflow margin includes a combustor portion fluidly connected to a turbine portion. The turbine portion includes a gas...
2016/0201570 EXHAUST NOZZLE ARRANGEMENT FOR GEARED TURBOFAN
A propulsion system according to an example of the present disclosure includes, among other things, a geared architecture configured to drive a fan section...
2016/0201569 EXHAUST NOZZLE ARRANGEMENT FOR GEARED TURBOFAN
A propulsion system according to an example of the present disclosure includes, among other things, a geared architecture configured to drive a fan section...
2016/0201568 GEARED GAS TURBINE ENGINE WITH REDUCED OIL TANK SIZE
A gas turbine engine comprises a fan drive turbine for driving a gear reduction, which drives a fan rotor. A lubrication system supplies oil to the gear...
2016/0201567 SYSTEM AND APPARATUS FOR DIVERSIFIED GEARBOX
A gas turbine engine assembly comprising, a gearbox including a first housing that includes a first auxiliary gear drive on a first portion thereof, a second...
2016/0201566 LARGE DISPLACEMENT HIGH TEMPERATURE SEAL
A seal assembly is provided for a gas turbine engine. This seal assembly includes a tadpole seal with a bulb and a tail, where the tail is directed toward a...
2016/0201565 METHOD AND SYSTEM FOR SEALING AN ANNULUS
A method and system for a compartment baffle system are provided. The compartment baffle system includes a first baffle portion extending along an axial length...
2016/0201564 FUEL SYSTEM
A fuel system includes: a constant-volume pump and a centrifugal pump increasing the pressure of fuel to be supplied to an engine for aviation and discharging...
2016/0201563 FUEL MANAGEMENT SYSTEM FOR A TURBINE ENGINE
A system is provided for a turbine engine that includes a fuel injector and an actuator. The system includes a fuel management system configured to receive...
2016/0201562 FUEL MANIFOLD FOR A GAS TURBINE ENGINE
A fuel supply manifold for a gas turbine engine includes a first manifold segment includes a first multiple of double-barrel fittings in communication with a...
2016/0201561 COMPOSITE FAN HOUSING ASSEMBLY OF A TURBOFAN ENGINE AND METHOD OF MANUFACTURE
A fan housing assembly of a turbofan engine and method of manufacture includes a fan housing that defines a flowpath radially inward, and a groove structure...
2016/0201560 COOLING AIR LINE FOR REMOVING COOLING AIR FROM A MANHOLE OF A GAS TURBINE
A gas turbine having a compressor, a turbine unit, at least one combustion chamber and a secondary air system, which secondary air system has at least one...
2016/0201559 TUBULAR COMBUSTION CHAMBER HAVING A FLAME TUBE END REGION AND GAS TURBINE
A tubular combustion chamber for a gas turbine has a combustion chamber head end, on which at least one first burner arrangement is arranged, a substantially...
2016/0201558 CONTROLLER COOLING ARRANGEMENT
A controller according to an exemplary aspect of the present disclosure includes, among other things, a cold plate and at least one electronic component...
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