Power system measurement based model calibration with enhanced optimization
Granted: April 15, 2025
Patent Number:
12278490
A dynamic simulation engine, having system parameters, may be provided for a component of an electrical power system (e.g., a generator, wind turbine, etc.). A model parameter tuning engine may receive, from a measurement data store, measurement data measured by an electrical power system measurement unit (e.g., a phasor measurement unit or digital fault recorder measuring a disturbance event). The model parameter tuning engine may then pre-condition the measurement data and set-up an…
Cable guiding structure for a tower for a wind turbine, method for mounting a cable guiding structure, and wind turbine
Granted: April 15, 2025
Patent Number:
12276264
A cable guiding structure (200) for a tower (108) of a wind turbine (10) is described. The tower has a height in substantially vertical direction (110) and a width in substantially horizontal direction (112). The cable guiding structure (200) is adapted for guiding a cable (160) within the tower of the wind turbine. The cable guiding structure includes a horizontal movement element (300) at least partially movable in the width direction (112) of the tower (108). The horizontal movement…
Pitch assembly for a wind turbine having minimized micro-pitching
Granted: April 15, 2025
Patent Number:
12276260
A pitch assembly for a wind turbine includes a pitch bearing comprising an inner race, an outer race, and a plurality of gear teeth arranged on one of the inner race or the outer race. The pitch assembly further includes a pitch drive mechanism having a pitch drive motor and a primary pitch drive pinion. The primary pitch drive pinion is configured to rotate one of the inner race or the outer race of the pitch bearing about a pitch axis by engaging with a first set of the plurality of…
Method of operating a turbine engine having a bleed system
Granted: April 15, 2025
Patent Number:
12276229
A method of operating a turbine engine. The turbine engine includes a high-pressure compressor including a high-pressure compressor flowpath and a plurality of stages, and a bleed system. The bleed system includes a plurality of bleed flowpaths including a first bleed flowpath from one stage of the plurality of stages and a second bleed flowpath from another stage of the plurality of stages. The method includes directing compressed air through the high-pressure compressor flowpath,…
Planet gear clearances in epicyclic gearboxes
Granted: April 15, 2025
Patent Number:
12276228
An epicyclic power gear box for a gas turbine engine delivers torque from a low speed shaft to the primary fan. The gear box includes a planet gear and a bearing pin for the planet gear, sun gear and ring gear. The planet gear and bearing pin are arranged so that a clearance between the two is maintained during a takeoff condition for the gas turbine engine.
Turbine engine screen
Granted: April 15, 2025
Patent Number:
12276227
A screen for an aeronautical gas turbine engine includes a plurality of first filaments and a plurality of second filaments. The plurality of second filaments define a plurality of openings with the plurality of first filaments. The plurality of first filaments and the plurality of second filaments define a first arrangement in which the plurality of first filaments are perpendicular to the plurality of second filaments. Upon application of a force to the screen, at least some of the…
Outlet guide vane assembly for a turbofan engine
Granted: April 15, 2025
Patent Number:
12276199
A turbofan engine defining a circumferential direction is provided. The turbofan engine includes a turbomachine; an unducted rotor assembly drivingly coupled to the turbomachine, the unducted rotor assembly including a plurality of unducted rotor blades; and a plurality of outlet guide vanes positioned downstream of the plurality of unducted rotor blades, the plurality of outlet guide vanes each defining a span, the spans of the plurality of outlet guide vanes being nonuniform along the…
Gas turbine engine noise reduction
Granted: April 15, 2025
Patent Number:
12275532
An aircraft engine includes a low pressure spool, a high pressure spool, and an alternative power source. The alternative power source is configured to add power to the high pressure spool. A controller is configured to determine a noise sensitive condition; and control, in response to determining the noise sensitive condition, the alternative power source to add power to the high pressure spool.
Tools and methods for handling tower sections
Granted: April 15, 2025
Patent Number:
12275344
The present disclosure relates to tools and methods for handling a tower section of a wind turbine tower. A tool comprises a first wheeled platform, a second wheeled platform, and a frame. The frame comprises a first side portion, and a second side portion. The first side portion is attached to the first wheeled platform and is configured to support a first end portion of a sling. The second side portion is attached to the second wheeled platform and is configured to support a second end…
Severe weather-driven large-scale outage management for emergency power grid
Granted: April 8, 2025
Patent Number:
12272951
Provided is a system and method that can safely generate and execute an outage plan for a power grid based on severe weather-driven events. In one example, the method may include receiving predicted or current operational power system state data from a power grid and weather conditions associated with the power grid, identifying one or more nodes on the power grid to de-energize based on the operational state data and the current weather conditions, determining a sequence of instructions…
System and method for cleaning turbine components
Granted: April 8, 2025
Patent Number:
12269074
A furnace system includes at least one wall that defines a workspace. The workspace includes an aircraft part to be cleaned. One or more vacuum pumps are configured to achieve a predetermined vacuum level in the workspace. A gas purifier is configured to remove impurities in a gas to create a purified gas, the purified gas being directed from the gas purifier into the workspace, the purified gas being of a purity and composition that is effective to disassociate oxides on a surface or in…
Thermal management system for an engine
Granted: April 8, 2025
Patent Number:
12270342
A thermal management system includes a thermal circuit having a thermal transport bus with a thermal fluid flowing therethrough. The thermal transport bus includes first and second bus segments. First and second thermal loads are on the first and second bus segments, respectively, and have different first and second inlet temperature requirements. The thermal management system includes a plurality of heat exchangers in thermal communication with the first and second thermal loads. The…
Gas turbine engine and fuel cell assembly
Granted: April 8, 2025
Patent Number:
12270340
A gas turbine engine is provided. The gas turbine engine includes a turbomachine having a compressor section, a combustor, and a turbine section arranged in serial flow order, the turbomachine further including an outer casing and, during operation of the gas turbine engine, an exhaust gas flow from the turbine section; and a fuel cell assembly positioned within the outer casing of the turbomachine, the fuel cell assembly having a fuel cell defining an inlet positioned to receive a…
Gas turbine engine oil flow control system
Granted: April 8, 2025
Patent Number:
12270337
A gas turbine engine oil flow control system can include a variable flow oil pump useful to provide oil at varying rates to a variety of oil consumers, such as, power gearboxes, engine shaft bearings, electrical generators, etc. Oil flow control valves that have an ability to provide a variable flow of oil can be used in conjunction with the variable flow oil pump. Flow sensors can be used along with an oil flow controller to measure a flow of oil at various points in the gas turbine…
Airfoils for gas turbine engines
Granted: April 8, 2025
Patent Number:
12270317
An airfoil for a turbine engine includes a body defining a pressure side and a suction side, the body extending between a leading edge and a trailing edge and also extending radially to define an outer edge. A radially-extending plenum can be disposed at the outer edge of the airfoil. A flared portion can be disposed at the outer edge of the body extending from the suction side.
Variable flowpath casings for blade tip clearance control
Granted: April 8, 2025
Patent Number:
12270308
Disclosed herein are example variable flowpath casings for blade tip clearance control. An example casing for a turbine engine includes an annular substrate extending along an axial direction, the annular substrate including a first surface and a second surface that is radially inward relative to the first surface; an actuator structure coupled to the second surface of the annular substrate; and a smart structure cantilevered from the second surface of the annular substrate, the smart…
Engine component with abradable material and treatment
Granted: April 8, 2025
Patent Number:
12270306
An engine component with an abradable material and treatment is disclosed herein. An example engine component includes a substrate having a first thickness and defining at least a first substrate surface, the substrate extending along an axial direction, an abradable material on the first substrate surface, the abradable material defining a first abradable material surface, a second abradable material surface spaced radially apart from the first abradable material surface and defining a…
Seal assembly for a rotary machine
Granted: April 8, 2025
Patent Number:
12270305
A rotary machine seal assembly (200) includes seal segments (102) configured to circumferentially extend around a rotor (108) between a stator (106) and the rotor (108) of a rotary machine. One or more seal segments include a shoe plate (110, 410, 710, 910), a seal base (112, 412, 712, 912), and at least one intermediate member (114, 414, 714). The shoe plate is disposed along the rotor. The seal base is disposed radially outward of the shoe plate. At least one intermediate member is…
Seal assembly for a turbomachine
Granted: April 8, 2025
Patent Number:
12270303
This disclosure is directed to seal assemblies for a turbomachine. The seal assemblies include stationary and rotating components and at least one interface between the stationary and rotating components. The seal assembly further includes a self-lubricating lattice element made of carbon or a carbon-based material. The self-lubricating lattice element may have a porous and compressible microstructure capable of retaining a liquid substance. During engine operation, the self-lubricating…
System and method for additive manufacturing control
Granted: April 8, 2025
Patent Number:
12269090
An additive manufacturing apparatus, a computing system, and a method for operating an additive manufacturing apparatus are provided. The method includes obtaining two or more images corresponding to respective build layers at a build plate, wherein each image comprises a plurality of data points comprising a feature and corresponding location at the build plate; removing variation between the features of the plurality of data points; and normalizing each feature to remove location…
