TURBOMACHINERY ENGINES WITH HIGH-SPEED LOW-PRESSURE TURBINES
Granted: August 29, 2024
Application Number:
20240287940
A turbomachinery engine includes a fan assembly, a low-pressure turbine, and a gearbox. The fan assembly includes a plurality of fan blades. The low-pressure turbine includes 3-5 rotating stages. The low-pressure turbine includes an area ratio equal to the annular exit area of an aft-most rotating stage of the low-pressure turbine divided by the annular exit area of a forward-most rotating stage of the low-pressure turbine. In some instances, the area ratio is within a range of 3.1-5.1.
TURBOMACHINERY ENGINES WITH HIGH-SPEED LOW-PRESSURE TURBINES
Granted: August 22, 2024
Application Number:
20240280058
A turbomachinery engine includes a fan assembly, a low-pressure turbine, and a gearbox. The fan assembly includes a plurality of fan blades. The low-pressure turbine includes 3-5 rotating stages. The low-pressure turbine includes an area ratio equal to the annular exit area of an aft-most rotating stage of the low-pressure turbine divided by the annular exit area of a forward-most rotating stage of the low-pressure turbine. In some instances, the area ratio is within a range of 3.1-5.1.
TURBOMACHINERY ENGINES WITH HIGH-SPEED LOW-PRESSURE TURBINES
Granted: August 22, 2024
Application Number:
20240280057
A turbomachinery engine includes a fan assembly, a low-pressure turbine, and a gearbox. The fan assembly includes a plurality of fan blades. The low-pressure turbine includes 3-5 rotating stages. The low-pressure turbine includes an area ratio equal to the annular exit area of an aft-most rotating stage of the low-pressure turbine divided by the annular exit area of a forward-most rotating stage of the low-pressure turbine. In some instances, the area ratio is within a range of 3.1-5.1.
TURBOMACHINERY ENGINES WITH HIGH-SPEED LOW-PRESSURE TURBINES
Granted: August 22, 2024
Application Number:
20240280056
A turbomachinery engine includes a fan assembly, a low-pressure turbine, and a gearbox. The fan assembly includes a plurality of fan blades. The low-pressure turbine includes 3-5 rotating stages. The low-pressure turbine includes an area ratio equal to the annular exit area of an aft-most rotating stage of the low-pressure turbine divided by the annular exit area of a forward-most rotating stage of the low-pressure turbine. In some instances, the area ratio is within a range of 3.1-5.1.
TURBOMACHINERY ENGINES WITH HIGH-SPEED LOW-PRESSURE TURBINES
Granted: August 22, 2024
Application Number:
20240280055
A turbomachinery engine includes a fan assembly, a low-pressure turbine, and a gearbox. The fan assembly includes a plurality of fan blades. The low-pressure turbine includes 3-5 rotating stages. The low-pressure turbine includes an area ratio equal to the annular exit area of an aft-most rotating stage of the low-pressure turbine divided by the annular exit area of a forward-most rotating stage of the low-pressure turbine. In some instances, the area ratio is within a range of 3.1-5.1.
FAST EARTHING SWITCH IMPLEMENTING THE COANDA EFFECT
Granted: August 15, 2024
Application Number:
20240274384
A fast earthing switch for a GIS, including a movable contact rod, having an end; a cylinder, fixed to the contact rod and forming a gas chamber around at least part of the contact rod, the gas chamber including an outlet around the contact rod so that gas can flow along the contact rod and its end when it moves from a closed to an open position; and means for actuating the contact rod between a closed and an open position.
CIRCUIT BREAKER COMPRISING AN IMPROVED GAS FLOW MANAGEMENT
Granted: August 8, 2024
Application Number:
20240266129
A high-voltage circuit breaker filled with gas, including two arcing contacts, a support in which a thermal volume, a compression volume, and an exhaust gas chamber are formed. A first radial wall separating the thermal volume and the compression volume, which is movable within the support. A second radial wall separating the compression volume and the exhaust gas chamber. A buffer volume is formed in the support and is separated from the compression volume and the exhaust gas chamber by…
OVERALL ENGINE EFFICIENCY RATING FOR TURBOMACHINE ENGINES
Granted: August 8, 2024
Application Number:
20240263588
A turbomachine engine can include a fan assembly, a vane assembly, a core engine, a gearbox, and an overall engine efficiency rating. The fan assembly can include a plurality of fan blades. The vane assembly can include a plurality of vanes, and the vanes can, in some instances, be disposed aft of the fan blades. The core engine can include a low-pressure turbine. The gearbox includes an input and an output. The input of the gearbox is coupled to the low-pressure turbine of the core…
OVERALL ENGINE EFFICIENCY RATING FOR TURBOMACHINE ENGINES
Granted: August 1, 2024
Application Number:
20240254925
A turbomachine engine can include a fan assembly, a vane assembly, a core engine, a gearbox, and an overall engine efficiency rating. The fan assembly can include a plurality of fan blades. The vane assembly can include a plurality of vanes, and the vanes can, in some instances, be disposed aft of the fan blades. The core engine can include a low-pressure turbine. The gearbox includes an input and an output. The input of the gearbox is coupled to the low-pressure turbine of the core…
SF6 FREE GAS INSULATED DISCONNECTOR WITH LIMITED ARCING VOLUME
Granted: August 1, 2024
Application Number:
20240258049
The invention concerns a disconnector (100) for a GIS comprising: a pair of permanent contacts (24, 41), one (24) fixed and the other one (41) movable along an axis (AA?), called the axis of the disconnector; a pair of arcing contacts (22, 42), one (22) fixed and the other one (42) movable; an insulating part (52) located inside said fixed arcing contacts (22, 42), and means (50) for pressing said insulating part against a front surface of the movable arcing contact (42); an…
VARIABLE PITCH FANS FOR TURBOMACHINERY ENGINES
Granted: July 11, 2024
Application Number:
20240229743
A turbomachinery engine can include a fan assembly with a plurality of variable pitch fan blades. The fan blades are configured such that they define a first VPF parameter and a second VPF parameter. The first VPF parameter is within a range of 0.10 to 0.40 and is defined as the hub-to-tip radius ratio divided by the fan pressure ratio. The second VPF parameter is within a range of 1-30 lbf/in2 and is defined as the bearing spanwise force divided by the fan area. In certain examples, the…
SYSTEM FOR READYING SUB-CRITICAL AND SUPER-CRITICAL STEAM GENERATOR, SERVICING METHOD OF SAID SUB-CRITICAL AND SUPER-CRITICAL STEAM GENERATOR AND METHOD OF OPERATION OF SUB-CRITICAL AND SUPER-CRITICAL STEAM GENERATOR
Granted: July 11, 2024
Application Number:
20240229683
A system for readying sub-critical and super-critical steam generator, a servicing method of the sub-critical and the super-critical steam generator and a method of operation of sub-critical and super-critical steam generator is provided. The steam generator includes a first auxiliary heating device disposed on at least one water-steam separator for heating the at least one water-steam separator, and/or a second auxiliary heating device disposed at least on a part of furnace top-end…
APPARATUS AND METHOD TO MANAGE TEMPERATURE AND STRESS IN A PART DURING ADDITIVE MANUFACTURING
Granted: July 11, 2024
Application Number:
20240227022
A method of additively manufacturing a workpiece may include depositing and melting a material on a build plate by translating a deposition head of an additive manufacturing apparatus over the build plate to form a layer of deposited material; and heating the deposited material with an oven after the layer is deposited on the build plate, wherein the oven comprises a furnace body and an oven lid movable with the deposition head and disposable on the furnace body to enclose a heated build…
HEAT EXCHANGERS INCLUDING PARTIAL HEIGHT FINS HAVING AT LEAST PARTIALLY FREE TERMINAL EDGES
Granted: June 13, 2024
Application Number:
20240191951
In an embodiment, a heat exchanger includes a monolithic body that includes a first substrate, a second substrate, a third substrate, and a plurality of partial height fins. The second substrate is arranged parallel to and spaced from the first substrate, thereby defining a first fluid flow path. The third substrate is arranged parallel to and spaced from the second substrate opposite the first substrate, thereby defining a second fluid flow path. The plurality of partial height fins…
FLUID DUCTS INCLUDING A RIB
Granted: June 13, 2024
Application Number:
20240191630
A fluid duct includes a body and an elongate rib. The body extends along a central axis and defines a lumen configured to receive a first fluid extending therethrough. The body has an inner surface and an outer surface. The central axis defines an axial direction along the central axis, a radial direction perpendicular to the central axis, and a circumferential direction oriented rotationally about the central axis. The elongate rib is positioned on the inner surface of the body and…
ELECTRICAL MACHINES FOR INTEGRATION INTO A PROPULSION ENGINE
Granted: May 30, 2024
Application Number:
20240178721
An electrical machine includes a stator assembly coupled to an engine stator component of a propulsion engine. The stator assembly includes a stator support assembly fixedly attached to the engine stator component and a stator disposed on a supporting surface of the stator support structure. The electrical machine also includes a rotor assembly including a rotor support structure connected to a shaft of the propulsion engine and a rotor attached to the rotor support structure such that…
GAS TURBINE ENGINES INCLUDING EMBEDDED ELECTRICAL MACHINES AND ASSOCIATED COOLING SYSTEMS
Granted: May 23, 2024
Application Number:
20240167422
A gas turbine engine includes a fan located at a forward portion of the gas turbine engine. A compressor section and a turbine section are arranged in serial flow order. The compressor section and the turbine section together define a core airflow path. A rotary member is rotatable with at least a portion of the compressor section and with at least a portion of the turbine section. An electrical machine is coupled to the rotary member and is located at least partially inward of the core…
GAS DELIVERY SYSTEM OF AN ADDITIVE MANUFACTURING MACHINE
Granted: May 23, 2024
Application Number:
20240165710
Embodiments of the present disclosure are directed to a gas flow delivery apparatus and systems of an additive manufacturing system. The gas delivery apparatus comprises a first conduit having an elbow and an outer diameter DA and at least one second conduit fluidly coupled to the first conduit at a mixing region. The mixing region is positioned downstream of the elbow of the first conduit, and the mixing region is at least a distance Z from a center line of the at least one second…
BUILD MATERIAL ESCAPEMENT ASSEMBLY AND ADDITIVE MANUFACTURING SYSTEMS INCLUDING SAME
Granted: May 16, 2024
Application Number:
20240157643
A build material escapement assembly for an additive manufacturing system includes a retaining plate for coupling the build material escapement assembly to the additive manufacturing system. A base having a plurality of ports is disposed beneath the retaining plate, and a support frame is disposed within the base. A diaphragm is disposed around the base, and a retractable plate is disposed between the support frame and the diaphragm. A top plate is further coupled to the retractable…
HEAT EXCHANGER INCLUDING FURCATING UNIT CELLS
Granted: May 16, 2024
Application Number:
20240159471
A heat exchanger is provided that can include furcating unit cells coupled with each other. Each of the unit cells can be elongated along an axis and include a sidewall that defines annular ring openings on opposite ends of the unit cell along the axis. The sidewall also can define undulating annular rings between the annular ring openings and axially separated from each other along the axis. The sidewall can further define angled openings into the unit cell both above and below each of…
