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Patent # Description
2016/0333754 Crankcase Ventilation System Heater
A crankcase ventilation system having a heat transfer conduit included therein. The system includes a housing and a crankcase ventilation filter element within...
2016/0333753 BLOW-BY GAS PASSAGE STRUCTURE
A blow-by gas passage structure is provided inside a separator chamber that is formed between a cylinder head cover and a baffle plate joined to the cylinder...
2016/0333752 SUMP AND AN ENGINE
An engine, for example for use in a marine vessel, comprises an engine superstructure; and an oil sump for collecting oil from the engine superstructure. At a...
2016/0333751 Engine Insert and Process for Installing
an engine insert having an insert appendage that projects outwardly from the insert body in a direction away from the seat face, into an engine, such as to...
2016/0333750 LOCATOR FOR USE IN A VALVETRAIN OF A CYLINDER HEAD OF AN INTERNAL COMBUSTION ENGINE
A locator for use in a valvetrain of a cylinder head of an internal combustion engine having a valve substantially concentrically aligned with both a valve...
2016/0333749 CAMSHAFT ADJUSTER AND METHOD FOR OPERATING A CAMSHAFT ADJUSTER
A method for operating a camshaft adjuster, which includes an adjusting transmission with an input shaft, an output shaft connected in a non-rotatable manner...
2016/0333748 METHOD AND A SYSTEM FOR DRIVING A TURBINE
In the method for driving a turbine according to the invention, at the moment of switching the direction of flow from the first tank (1) to the second tank (2)...
2016/0333747 Prime Mover with Recovered Energy Induced Source and Sink Temperature
A system for using recovered energy to increase the source to sink temperature differential for heating and cooling the working fluid of a prime mover, and in...
2016/0333746 PLASMA ASSISTED DIRTY WATER ONCE THROUGH STEAM GENERATION SYSTEM, APPARATUS AND METHOD
A system and method can comprise a heat source, a plasma assisted vitrifier comprising a syphon valve; and a self-cleaning heat exchanger comprising a fired...
2016/0333745 METHOD AND APPARATUS FOR GENERATING ELECTRICITY USING A NUCLEAR POWER PLANT
A method for generating electricity by means of a nuclear power plant and a liquid vaporization apparatus involves producing heat energy by means of the...
2016/0333744 METHOD AND APPARATUS FOR GENERATING ELECTRICITY USING A THERMAL POWER PLANT
A method for generating electricity by means of a thermal power plant and a liquid vaporization apparatus involves producing heat energy by means of the power...
2016/0333743 GAS TURBINE OPERATION METHOD AND OPERATION CONTROL DEVICE
To remove water accumulated in a cooling air system while preventing performance loss of a gas turbine, the gas turbine is provided with a cooling air system...
2016/0333742 RAT FRAME FOR A SOFT AIRCRAFT INTERFACE
A mounting frame for a ram air turbine includes a front support block having a top side opposite a bottom side. A rear support block is disposed opposite the...
2016/0333741 CMC HANGER SLEEVE FOR CMC SHROUD
According to some embodiments, a ceramic matrix composite (CMC) hanger sleeve is provided for retaining a ceramic matrix composite shroud panel. The sleeve may...
2016/0333740 SHROUD RETENTION SYSTEM WITH KEYED RETENTION CLIPS
A shroud retention system may include a shroud hanger having an outer hanger wall that defines a clip groove including a narrow groove portion and an enlarged...
2016/0333739 TIE ROD CONNECTION FOR MID-TURBINE FRAME
A mid-turbine frame for use in a gas turbine engine comprises at least one vane extending between a vane inner platform and a vane outer platform, and an inner...
2016/0333738 STEEL SOFT WALL FAN CASE
A steel soft wall fan case assembly according to one embodiment configured with a thin-walled steel support structure shell including a plurality of annular...
2016/0333737 Turbocharger with oil-free hydrostatic bearing
A turbocharger for an internal combustion engine, the turbocharger being supported by hydrostatic bearings in both a radial and an axial direction by a...
2016/0333736 ACTIVE SYSTEM FOR BEARING OIL DAMPER SUPPLY AND VIBRATION CONTROL
A bearing damping system includes a pump configured to pump a fluid. The system further includes a variable position valve having a plurality of open positions...
2016/0333735 ANGLED IMPINGEMENT INSERTS WITH COOLING FEATURES
An engine component assembly is provided with an insert having cooling features. The engine component comprises a cooled engine component surface having a flow...
2016/0333734 IMMERSED CORE FLOW INLET BETWEEN ROTOR BLADE AND STATOR VANE FOR AN UNDUCTED FAN GAS TURBINE
An unducted thrust producing system is provided that can include a rotating element having an axis of rotation about a central longitudinal axis and comprising...
2016/0333733 Turbine Airfoil With Additive Manufactured Reinforcement of Thermoplastic Body
A component for a gas turbine engine comprises an airfoil body formed of a plastic. A reinforcement portion has webs formed of a metallic material and extend...
2016/0333732 DEVICE AND METHOD FOR CLEANING THE CORE ENGINE OF A JET ENGINE
The object of the invention is a device for cleaning the core engine of a jet engine, having a supply unit, which provides the cleaning medium, a nozzle unit,...
2016/0333731 METHOD FOR OPERATING A GAS TURBINE AT PART LOAD
The invention refers to a method for controlling part load operation of a gas turbine comprising a controller wherein a load set point of the controller is...
2016/0333730 AUTOMATED PROPELLER FEATHER TESTING
There is described herein the automation of propeller feather testing functions, whereby the test is automatically performed and a pass/fail signal is issued...
2016/0333729 TURBINE ENGINE HAVING VARIABLE PITCH OUTLET GUIDE VANES
A gas turbine engine including a core engine and a fan configured in mechanical communication with the core engine is provided. The gas turbine engine also...
2016/0333728 NACELLE VENTILATION MANIFOLD
A gas turbine engine comprises a core engine housing. A nacelle is positioned radially outwardly of the core engine housing. An outer bypass housing is...
2016/0333727 VANE STRUT POSITIONING AND SECURING SYSTEMS INCLUDING LOCKING WASHERS
A vane strut positioning and securement system includes a housing including a washer aperture defined in an inner diameter thereof and a lock washer disposed...
2016/0333726 VANE STRUT POSITIONING AND SECURING SYSTEMS
A strut-flap vane system for a turbomachine includes a vane strut comprising an airfoil portion and a strut mount extending in a radially outward direction...
2016/0333725 COMPOSITE WEAR PAD FOR EXHAUST NOZZLE
A composite wear pad for being coupled to a slider block of a convergent nozzle of a gas turbine engine includes a high heat capacity composite having a resin...
2016/0333724 DRAIN FOR A PRESSURE SENSING LINE
A drain includes a vortex throttle, to remove water from a pressure sensing line. The vortex throttle resists the flow of air through it. Therefore, for a...
2016/0333723 DRAIN FOR A PRESSURE SENSING LINE
The invention provides a drain to allow water to flow out of a pressure sensing line. The drain comprises a tube including a plurality of restrictors in flow...
2016/0333722 INTERSHAFT INTEGRATED SEAL AND LOCK-NUT
An intershaft integrated seal and lock-nut assembly includes spaced apart forward and aft shafts, forward lock-nut threaded onto aft end of forward shaft, aft...
2016/0333721 CAM-FOLLOWER ACTIVE CLEARANCE CONTROL
A blade outer air seal (BOAS) assembly is provided. The BOAS assembly may comprise an outer case, a first support arm, a second support arm, a control rod, a...
2016/0333720 FLEXIBLE SMALL CAVITY SEAL FOR GAS TURBINE ENGINES
A seal assembly, comprising a first segment, a second segment, and a seal incorporated between the first segment and the second segment, the seal comprising a...
2016/0333719 METHOD OF MAKING A TURBINE SHROUD
A method of making a shroud assembly by: forming a shroud frame consisting of a one-piece hook and rail assembly which includes a first rail and a second rail...
2016/0333718 COMPOSITE KEYSTONED BLADE TRACK
A blade track for a gas turbine engine includes a plurality of blade track segments. The blade track segments are arranged circumferentially around a central...
2016/0333717 NEAR NET SHAPE ABRADABLE SEAL MANUFACTURING METHOD
A method of manufacturing a net shaped seal comprises depositing a first layer of fine powder comprising an abradable feed stock material on a substrate. The...
2016/0333716 BLADE OUTER AIR SEAL MOUNT
The present disclosure relates generally to blade outer air seal section mount including a resilient spring element that acts to provide re-centering forces to...
2016/0333715 RETENTION CLIP FOR A BLADE OUTER AIR SEAL
One exemplary embodiment of this disclosure relates to a system having a static segment with a circumferentially extending slot. The system further includes a...
2016/0333714 SEALING STRUCTURE AND ROTARY MACHINE
A sealing structure that seals a clearance between an outer peripheral surface of a rotor and an inner peripheral surface of a stator. The sealing structure...
2016/0333713 SYSTEM FOR THERMALLY ISOLATING A TURBINE SHROUD
In one aspect the present subject matter is directed to a system for thermally isolating a turbine shroud of a turbine shroud assembly. The system includes a...
2016/0333712 CHORDAL SEAL
An airfoil for a gas turbine engine includes a first airfoil. A first chordal seal is located adjacent a first end of the airfoil. A second chordal seal is...
2016/0333711 FLANGED SPRING GUIDE FOR A FACE SEAL ARRANGEMENT
A spring guide for use in a seal housing including a first body portion, a second body portion, and a flange portion, including a flange width, extending...
2016/0333710 VIBRATION DAMPING FOR STRUCTURAL GUIDE VANES
A stationary guide vane includes a top platform, a bottom platform, and a vane body located between the top platform and the bottom platform. The vane body...
2016/0333709 RADIAL CONTROL SHAFT FOR A DEVICE FOR CONTROLLING THE PITCH OF FAN BLADES OF A TURBINE ENGINE HAVING AN...
The invention relates to a radial control shaft (48) for a device for controlling the pitch of fan blades of a turbine engine having an unducted fan, the shaft...
2016/0333708 BLADED ROTOR FOR A GAS TURBINE ENGINE
A bladed rotor includes rotor disc having a peripheral region, and a plurality of rotor blades attached to and extending radially outwardly from peripheral...
2016/0333707 TURBO ENGINE ROTOR COMPRISING A BLADE-SHAFT CONNECTION MEANS, AND BLADE FOR SAID ROTOR
In a turbo engine, the rotor includes a shaft, blades, and a shaft-blade connection. The shaft blade connection can be provided as a fir tree connection,...
2016/0333706 MASKING METHOD FOR PRODUCING A COMBINATION OF BLADE TIP HARDFACING AND EROSION-PROTECTION COATING
A method for manufacturing a blade (1) for a turbomachine, the blade having a hardfacing on its tip (4) and an erosion-protection coating (13) at least on its...
2016/0333705 COMBINATION OF BLADE TIP CLADDING AND EROSION-RESISTANT LAYER AND METHOD FOR THE PRODUCTION THEREOF
A method for producing a blade for a turbomachine, the blade having a blade tip cladding on its blade tip and an erosion-resistant layer at least on its blade...
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