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Patent # Description
US-9,863,301 Filter fault detection apparatus
A filter fault detection apparatus for a filter mounted on an exhaust passage of an internal combustion engine for collecting particulate matter includes a...
US-9,863,300 Holding jig and pressure loss measuring device
A holding jig has a tubular jig base member, and a tubular expansion/contraction member disposed on an inner peripheral surface side of the tubular jig base...
US-9,863,299 Engine exhaust treatment device
There is provided an engine exhaust treatment device in which stick of a nozzle portion of a urea water injector can be suppressed. The engine exhaust treatment...
US-9,863,298 Compression ignition engine system with improved regeneration via controlled ash deposits
An engine system includes an electronically controlled compression ignition engine configured to burn diesel fuel and a high ash oil to produce an exhaust with...
US-9,863,297 Emission treatment system
An emission treatment system and method for remediating the nitrogen oxides (NOx), particulate matter, and gaseous hydrocarbons present in diesel engine exhaust...
US-9,863,296 Centrifugal separator having oil coating on sidewalls
A centrifugal separator for cleaning crankcase gas, containing oil, from an internal combustion engine, includes a stationary casing defining a separation space...
US-9,863,295 Engine unit
An engine unit includes an engine body, a crankshaft, and an oil tank. The engine body includes a cylinder unit and a crankcase. The crankshaft is accommodated...
US-9,863,294 Hydraulic control system for vehicle
A first check valve of a hydraulic control system allows oil to flow in only a direction from a first oil pump toward an oil receiving portion. A second check...
US-9,863,293 Variable valve actuation system including an accumulator and a method for controlling the variable valve...
A system according to the principles of the present disclosure includes a valve actuator, a pump, an accumulator, and a control valve. The valve actuator...
US-9,863,292 Structure of air flow control valve and intake device
A structure of an air flow control valve includes: valve main body portions respectively provided in intake ports, and controlling the flow of a fluid supplied...
US-9,863,291 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...
US-9,863,290 Valve timing adjusting device
A valve timing adjusting device includes a housing, a vane rotor, a sleeve, and a spool. The housing includes a timing pulley connected to a crank shaft through...
US-9,863,289 CVVT apparatus for engine
A continuous variable valve timing apparatus for an engine includes: a housing, a rotor installed to be rotatable relative to the housing and connected to a...
US-9,863,288 Valve opening and closing timing control device
A valve opening and closing timing control device includes: a driving-side rotating body including a sprocket around which a rotating body interlocked with a...
US-9,863,287 Heat engine system with a supercritical working fluid and processes thereof
Aspects of the invention disclosed herein generally provide heat engine systems and methods for generating electricity. In one configuration, a heat engine...
US-9,863,286 Combined cycle power plant system and related control systems and program products
Various embodiments include a system having: at least one computing device configured to monitor a combined-cycle (CC) power plant during a transient event by...
US-9,863,285 Power generation system having compressor creating excess gas flow for supplemental gas turbine system
A power generation system may include a generator; a gas turbine system for powering the generator, the gas turbine system including a turbine component, an...
US-9,863,284 Power generation system having compressor creating excess air flow and cooling fluid injection therefor
A power generation system includes: a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to which...
US-9,863,283 Steam turbine power plant and method for activating steam turbine power plant
A steam turbine power plant includes a life consumption amount calculator configured to calculate life consumption amounts of a turbine rotor based on a value...
US-9,863,282 Automated mass management control
Embodiments of the invention generally provide a heat engine system, a mass management system (MMS), and a method for regulating pressure in the heat engine...
US-9,863,281 Carbon dioxide capture interface for power generation facilities
In a power generation facility (10) wherein a fluidized bed combustion unit (12) produces steam to power a steam turbine generator (32), a heat recovery steam...
US-9,863,280 Combined heat and power system
A CHP system includes a combustor (heat source), a Rankine cycle apparatus, and a second heat exchanger. The Rankine cycle apparatus includes, as an evaporator,...
US-9,863,279 Multipurpose support system for a gas turbine
A system includes a gas turbine engine and a multipurpose gas turbine engine support frame couple to the gas turbine engine. The multipurpose gas turbine...
US-9,863,278 Air exhaust tube holder in a turbomachine
A support for carrying a tube for discharging oil-laden air from a turbine engine, the support including a radially inner annular portion for mounting around...
US-9,863,277 Fan rotor, in particular for a turbine engine
A turbine engine fan rotor having a disk carrying blades, a substantially frustoconical cover mounted on the disk, and axial retention device for retaining the...
US-9,863,276 Actuator housing for ram air turbine deployment actuator
An actuator housing is provided. The actuator housing may comprise a body, and a first side of the body including a first pin interface and a first threaded...
US-9,863,275 Turbine shroud contour exducer relief
A turbocharger turbine having a blade-gap zone between the blades and the shroud wall. The blade-gap zone is larger at and near the exducer than at an upstream...
US-9,863,274 Collapsible support structure for a gas turbine engine
Described is a shaft support system for a gas turbine engine comprising: a rotatable fan shaft; first and second support structures extending in parallel from...
US-9,863,273 Isostatic suspension of a turbojet by rear double support
The invention relates to a bypass turbojet comprising an exhaust housing having a central hub (13) and connecting means (11) that can transmit the forces...
US-9,863,272 Turbomachine
A turbomachine of this disclosure includes a rotation shaft, a first impeller, a first bearing, and a second bearing. The first impeller is fixed to the...
US-9,863,271 Arrangement for a turbomachine
An arrangement for a turbomachine is provided. The arrangement includes a vane for directing a hot gas during the operation of the turbomachine, a stator ring...
US-9,863,270 Turbomachine casing
A turbomachine casing including a substantially cylindrical wall and an annular one-piece acoustic insulation panel mounted inside the wall, the panel including...
US-9,863,269 System for packaging electronic components in a rotatable shaft
A system for packaging electronic components in a rotatable shaft includes an annular carrier shaft having a first end that is axially spaced from a second end...
US-9,863,268 Dynamic system estimation device and method
A dynamic system estimation device and method, whereby estimation for more performance parameters than there are sensors can be performed, the estimation taking...
US-9,863,267 System and method of control for a gas turbine engine
A system includes plurality of combustors and a distributed flow measurement system coupled to the plurality of combustors. Each combustor of the plurality of...
US-9,863,266 Waste heat recovery system for a power source
The present disclosure is directed to a waste heat recovery system used in conjunction with a power source system. A pump may pressurize a working fluid to a...
US-9,863,265 Shroud assembly and shroud for gas turbine engine
Shroud assemblies and shrouds for gas turbine engines are provided. A shroud includes a shroud body which includes a forward surface, a rear surface axially...
US-9,863,264 Turbine shroud engagement arrangement and method
According to one aspect of the invention a turbine shroud engagement arrangement includes an outer shroud and an inner shroud operably connectable to the outer...
US-9,863,263 Turbine wheel for a turbine engine
A turbine wheel for a turbine engine is provided. The turbine wheel includes a disk carrying blades including internal channels for passing a flow of cooling...
US-9,863,262 Sealing structure for turbocharger housing
Bolt holes 16 are formed in a joint part 14 of a turbine housing 12, with flanged bolts 40 screwed in the bolt holes 16. A flange part 32 of a bearing housing...
US-9,863,261 Component retention with probe
A gas turbine engine includes a casing, a probe, and a fairing. The probe extends through the casing and the fairing is disposed within the casing. The fairing...
US-9,863,260 Hybrid nozzle segment assemblies for a gas turbine engine
A nozzle segment assembly for a gas turbine engine may generally include inner and outer ring support segments and a nozzle fairing positioned between the inner...
US-9,863,259 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...
US-9,863,258 Method of forming a structural connection between a spar cap and a fairing for a wind turbine blade
A method of forming a structural connection between a spar cap 14 and an aerodynamic fairing 12. A composite comprising an uncured matrix and a compressible...
US-9,863,257 Additive manufactured inseparable platform damper and seal assembly for a gas turbine engine
A damper-seal assembly for a gas turbine engine includes an additively manufactured seal and an additively manufactured damper inseparably assembled with the...
US-9,863,256 Internal cooling system with insert forming nearwall cooling channels in an aft cooling cavity of an airfoil...
An airfoil (10) for a gas turbine engine in which the airfoil (10) includes an internal cooling system (14) with one or more internal cavities having an insert...
US-9,863,255 Impingement cooling of turbine blades or vanes
A turbine assembly having a hollow aerofoil and impingement device, the aerofoil having a first side wall from leading to trailing edge and a cavity arranged a...
US-9,863,254 Turbine airfoil with local wall thickness control
A turbine airfoil for a gas turbine engine including an outer peripheral wall having an external surface, the outer peripheral wall enclosing an interior space...
US-9,863,253 Axial turbomachine compressor blade with branches at the base and at the head of the blade
The invention relates to a blade of an axial turbomachine comprising an airfoil which extends radially and a first set of branches or divisions, which radially...
US-9,863,252 Single-piece blisk for turbomachine fan comprising an upstream and/or downstream recess making its blades more...
The invention relates to a single-piece fan blisk (14) for a turbojet, this blisk (14) comprising a hub (16) with a general shape of revolution about a rotation...
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