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Patent # Description
US-1,006,0309 Internal combustion engine having oil baffle
An internal combustion engine that includes an oil baffle in the oil sump. The internal combustion engine may include a crankcase comprising an oil sump...
US-1,006,0308 Modularized multifunctional variable valve actuation system for use in 6-cylinder internal combustion engine
A modularized multifunctional variable valve actuation system for use in a six-cylinder internal combustion engine. The system includes two fuel supply modules...
US-1,006,0306 Continuous variable valve duration apparatus and engine provided with the same
A continuous variable valve duration apparatus may include: a camshaft; first and second cam portions on which a cam is formed respectively; first and second...
US-1,006,0305 Variable valve timing apparatus
A control device has two modes as control modes of an electric power supply to an electromagnetic solenoid, which are used when a first determining unit...
US-1,006,0304 Valve control system having an adjustable camshaft
A valve control system may include an adjustable camshaft that includes an outer shaft and an inner shaft that extends through the outer shaft. The valve...
US-1,006,0303 Camshaft phaser using one-way slipper clutches
A camshaft phaser comprising an advance one-way clutch and a retard one-way clutch. The camshaft phaser comprises an input component arranged to receive torque...
US-1,006,0302 Passive low temperature heat sources organic working fluid power generation method
The present invention relates to a passive low temperature heat energy organic working fluid power generation method and system, Comprising: organic working...
US-1,006,0301 Gas turbine unit operating mode and design
Gas turbine unit (GTV) provides compressed air and steam methane-hydrogen mixture to a combustion chamber to enrich combustion products and cooling by...
US-1,006,0300 Sectioned gas turbine engine driven by sCO2 cycle
An apparatus, system, and method for a gas turbine engine may include a sectioned heat exchanger. A heat exchanger may include an inlet manifold configured to...
US-1,006,0299 Thermo-elevation plant and method
In some aspects, a thermal elevation system includes a base plant including an evaporator to vaporize a working fluid. A lift conduit is coupled to the base...
US-1,006,0298 Thermal energy recovery device and start-up method thereof
A thermal energy recovery device capable of suppressing a rapid increase of thermal stress generated in an evaporator when the operation is started and a...
US-1,006,0297 Apparatus and method for reactor power control of steam turbine power generation system
Disclosed herein is an apparatus for reactor power control of a steam turbine power generation system including a reactor, a high-pressure turbine to which...
US-1,006,0296 Quintuple-effect generation multi-cycle hybrid renewable energy system with integrated energy provisioning,...
Provided is a consumer to industrial scale renewable energy based quintuple-generation systems and energy storage facility. The present invention has both...
US-1,006,0295 Repair of surface damage at edges of cellular panels
A method of working a non-conforming exhaust sleeve utilizes a first plate disposed over an outer surface of an exhaust sleeve and a second plate disposed over...
US-1,006,0294 Gas turbine engine assemblies with ceramic matrix composite components having undulated features
An assembly adapted for use in a gas turbine engine is disclosed herein. The assembly includes a first component including metallic materials and a second...
US-1,006,0293 Baseplate for mounting and supporting rotating machinery and system comprising said baseplate
The baseplate comprises a central elongate torsion and bending resisting member and at least a first load bearing cross-member, which extends transversely to...
US-1,006,0292 Castellated latch mechanism for a gas turbine engine
A gas turbine engine includes a fan duct including a fan duct inner structure that surrounds a core engine, a fan case that surrounds a fan, a core engine...
US-1,006,0291 Mid-turbine frame rod and turbine case flange
A turbine section of a gas turbine engine includes a first turbine supported for rotation about an axis, a second turbine spaced axially aft of the for first...
US-1,006,0290 Method and system for centrifugal pump
The pump includes a first rotatable member including a radially inward facing groove having an edge. The first rotatable member configured to receive a...
US-1,006,0289 Geared gas turbine engine with oil deaerator and air removal
A gas turbine engine has a fan drive turbine for driving a gear reduction. The gear reduction drives a fan rotor. A lubrication system supplies oil to the gear...
US-1,006,0288 Multi-flow cooling passage chamber for gas turbine engine
A cooling chamber in a gas turbine engine includes a first side surface, a second side surface, a bottom surface, and a top surface defining a chamber therein....
US-1,006,0287 Pressure relief door assembly
A pressure relief door (PRD) assembly includes a PRD frame, a PRD coupled to the PRD frame, a latch element configured to remain in a latched condition to...
US-1,006,0286 Geared annular airflow actuation system for variable cycle gas turbine engines
An annular airflow control system for a gas turbine engine includes a sync ring rotatable to move the multiple of contra-rotatable variable vanes through a...
US-1,006,0285 Variable vane control system
A method of controlling a variable vane assembly includes the steps of sensing a first angular deflection of a first array of variable vanes about a first vane...
US-1,006,0284 Engine inlet total air temperature sensor
A total air temperature (TAT) sensor assembly is disclosed. The assembly includes a housing that accommodates a temperature sensor. The assembly also includes a...
US-1,006,0283 Rankine-cycle power-generating apparatus
Specific operation is executable in a Rankine-cycle power-generating apparatus. In the Rankine-cycle power-generating apparatus, a) in the specific operation,...
US-1,006,0282 Geared turbofan with integrally bladed rotor
A gas turbine comprises a compressor module, with a lower pressure compressor section including a plurality of stages, with at least one of the plurality of...
US-1,006,0281 Compressor abradable material seal with tailored wear ratio and desirable erosion resistance
What is described is a wear resistant seal system that is adapted for resisting wear of a rotating part in a gas turbine engine as it rotates against a...
US-1,006,0280 Turbine cavity sealing assembly
Aspects of the disclosure are directed to a gas turbine engine, comprising a sealing assembly that includes a non-contacting HALO seal, a ring constructed as a...
US-1,006,0279 Seal support disk and assembly
An assembly for a gas turbine engine includes a first module, a second module interconnected with the first module, a first gas turbine component, and a seal...
US-1,006,0278 Guide vane for a turbomachine having a sealing device; stator, as well as turbomachine
A guide vane (300) for a turbomachine, having a sealing device (27, 27') at the radially inner end region of the guide vane (300) for sealing leakage flows (25)...
US-1,006,0277 Turbine wheel with clamped blade attachment
A turbine wheel for use in a gas turbine engine having a plurality of blades attached to a rotor disk. Each blade is formed from a composite comprising ceramic...
US-1,006,0276 Turbine rotor, turbine, and method for removing seal plate
A turbine rotor includes: a rotor shaft part; a plurality of blades secured to an outer periphery of the rotor shaft part; and a seal plate configured to be...
US-1,006,0275 Turbomachine blade arrangement with first and second guides with respective movable first and second elements...
The present invention relates to a turbomachine blade (100; 200) with a base element, which has a blade part (1) for flow diversion and a blade root (2), a...
US-1,006,0274 Twisted blade root
A rotor blade for a wind turbine having a blade root, a transition piece and an aerodynamic part, wherein the blade root essentially is optimized for fixation...
US-1,006,0273 System and method for manufacture of abrasive coating
A component for a gas turbine engine includes an airfoil section including a free end and an abrasive coating sprayed onto the free end, the abrasive coating...
US-1,006,0272 Turbine vane with load shield
A turbine vane for use in a gas turbine engine is disclosed. The turbine vane includes an inner platform, an outer platform spaced from the inner platform, and...
US-1,006,0271 Fan airfoil shrouds with area ruling in the shrouds
A shrouded airfoil may have a suction surface and a pressure surface. An at least first suction surface shroud may be disposed on the suction surface and an at...
US-1,006,0270 Internal cooling system with converging-diverging exit slots in trailing edge cooling channel for an airfoil in...
An airfoil (10) is disclosed for a gas turbine engine in which the airfoil (10) includes an internal cooling system (14) with one or more converging-diverging...
US-1,006,0269 Cooling circuits for a multi-wall blade
A cooling system according to an embodiment includes: a leading edge cooling circuit including a pressure side serpentine circuit and a suction side serpentine...
US-1,006,0268 Turbine blade having film cooling hole arrangement
A turbine blade includes a platform that has a platform leading edge and trailing edge joined by two platform circumferential sides. An airfoil extends radially...
US-1,006,0267 Gas turbine engine airfoil cooling passage turbulator pedestal
A gas turbine engine component includes a structure that provides a cooling passage. The structure has a turbulator with a pedestal joining opposing first and...
US-1,006,0266 Covers for cavities in aircraft fan blades
Hollow fan blades for gas turbine engines are disclosed. The hollow fan blades include a body having a convex side and a concave side wherein the convex side...
US-1,006,0265 Turbine blade
The cooling effectiveness of a turbine blade that a gas turbine engine or the like is provided with is further increased by providing a convex portion that is...
US-1,006,0264 Gas turbine engine and cooled flowpath component therefor
Apparatus and systems for a cooled gas turbine engine flowpath component are disclosed. In some embodiments, the flowpath component includes a spar and a...
US-1,006,0263 Incidence-tolerant, high-turning fan exit stator
A gas turbine engine component is described. The gas turbine engine component includes an inner diameter edge, an outer diameter edge, a trailing edge and a...
US-1,006,0262 Vibration dampers for turbine blades
A turbine blade vibration damper is described. The damper has an axially-extending main body defining an inner surface and opposed damping surface. The main...
US-1,006,0261 Rotary synchronized combustion engine
An engine system is provided, including a housing, multiple shafts in alignment and in parallel with each other, vertically penetrating through the housing,...
US-1,006,0260 Arrangement and method for positioning cartridges for a rock grouting equipment
Arrangement (10) for a rock grouting equipment for positioning at least one cartridge (11) is described. The arrangement incorporates at least one magazine...
US-1,006,0259 Passive sampling device and method of sampling and analysis
A device and method to quantitatively measure concentrations of volatile organic compound vapors below the ground surface using a preferably "fully" passive...
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