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公开(公告)号:US11821370B2
公开(公告)日:2023-11-21
申请号:US17529625
申请日:2021-11-18
Applicant: Hamilton Sundstrand Corporation
Inventor: Debabrata Pal
CPC classification number: F02C7/32 , B64D27/20 , F01D15/10 , F01D25/28 , F02C7/18 , B64D2041/002 , F05D2220/323 , F05D2220/50 , F05D2220/76
Abstract: An engine system includes an engine duct and a tail cone arranged radially inwardly of the engine duct. The tail cone has an outer surface and an inner surface. A generator housing is arranged in the tail cone. The generator housing includes an outer surface portion spaced from the inner surface of the tail cone. A generator is mounted in the generator housing. An air duct extends from the generator, through the generator housing, through the tail cone, and through the engine duct. The air duct includes an opening exposed to an air stream passing over the engine duct.
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42.
公开(公告)号:US20230349322A1
公开(公告)日:2023-11-02
申请号:US18218063
申请日:2023-07-04
Applicant: Siemens Energy Global GmbH & Co. KG
Inventor: Matthias Migl , Ronald Schwarz , Denis Tschetschik
CPC classification number: F02C6/18 , F01K17/025 , F05D2220/64 , F05D2220/76
Abstract: An energy generation plant in which the exhaust gas from a gas turbine is guided into a thermal energy store, wherein the thermal energy store can be used for various purposes. The energy generation plant has at least one gas turbine having an exhaust gas apparatus, at least one generator, at least one thermal energy store, wherein the generator can be driven by the gas turbine, wherein the hot exhaust gas from the gas turbine is passed directly to a thermal energy store via the exhaust gas apparatus, wherein the thermal energy from the thermal energy store can be used to generate power.
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公开(公告)号:US11802489B1
公开(公告)日:2023-10-31
申请号:US17942945
申请日:2022-09-12
Applicant: Hamilton Sundstrand Corporation
Inventor: Todd A. Spierling
CPC classification number: F01D15/10 , B64D27/24 , F02B37/10 , F02B39/10 , B64D2027/026 , F05D2220/76
Abstract: In accordance with at least one aspect of this disclosure, a system includes a turbine configured to fluidly connect to a heat engine to be driven by exhaust from the heat engine, the turbine including a turbine shaft, and a generator operatively coupled to the turbine shaft to be driven by the turbine configured to receive rotational input power from turbine shaft and to convert the rotational input power to output power to generate electrical energy.
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公开(公告)号:US20230340860A1
公开(公告)日:2023-10-26
申请号:US18214767
申请日:2023-06-27
Applicant: Dawson Hoffman
Inventor: Dawson Hoffman
CPC classification number: E21B41/0085 , F01D15/10 , F05D2220/76
Abstract: A hydrocarbon flow control generator system includes a pressurized hydrocarbon flow inlet, an expansion device in pressurized hydrocarbon flow communication with the pressurized hydrocarbon flow inlet, a generator connected to the expansion device, a drive system connecting the generator and the expansion device, a gathering point at which depressurized hydrocarbon stream is delivered to an end use location, and a variable load device via which an electrical power stream generated by the generator is delivered to an electric load. The expansion device is configured to receive a highly pressurized hydrocarbon stream from the pressurized hydrocarbon flow inlet, control and regulate a received hydrocarbon stream, and depressurize the hydrocarbon stream. The variable load device is configured to adjust load on the generator by adjusting electrical demand on the generator based on a pressure of the depressurized hydrocarbon stream sensed between the expansion device and the gathering point.
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公开(公告)号:US20230332582A1
公开(公告)日:2023-10-19
申请号:US18212269
申请日:2023-06-21
Applicant: ICE Thermal Harvesting, LLC
Inventor: Adrian Benjamin Bodishbaugh , Carrie Jeanne Murtland
IPC: F03G7/04 , E21B47/07 , E21B34/06 , E21B41/00 , F01K25/08 , F03G4/00 , F03G4/06 , E21B36/00 , F01K11/02 , F01K17/02 , H02K7/18 , F24T50/00 , E21B34/02 , F03G7/00
CPC classification number: F03G7/045 , E21B47/07 , E21B34/066 , E21B41/0085 , F01K25/08 , F03G4/023 , F03G4/06 , F03G4/035 , E21B36/00 , F01K11/02 , F01K17/02 , H02K7/1823 , F24T50/00 , F03G4/072 , E21B34/025 , F03G7/027 , F02G2243/08 , F05D2220/76
Abstract: Systems and methods for generating and a controller for controlling generation of geothermal power in an organic Rankine cycle (ORC) operation in the vicinity of a wellhead during hydrocarbon production to thereby supply electrical power to one or more of in-field operational equipment, a grid power structure, and an energy storage device. In an embodiment, during hydrocarbon production, a temperature of a flow of wellhead fluid from the wellhead or working fluid may be determined. If the temperature is above a vaporous phase change threshold of the working fluid, heat exchanger valves may be opened to divert flow of wellhead fluid to heat exchangers to facilitate heat transfer from the flow of wellhead fluid to working fluid through the heat exchangers, thereby to cause the working fluid to change from a liquid to vapor, the vapor to cause a generator to generate electrical power via rotation of an expander.
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公开(公告)号:US11788472B2
公开(公告)日:2023-10-17
申请号:US17479502
申请日:2021-09-20
Applicant: RTX Corporation
Inventor: Steven W. Burd
CPC classification number: F02C7/36 , F02C7/185 , F02C7/32 , F05D2220/323 , F05D2220/76
Abstract: Aircraft generator systems are described. The aircraft generator systems include a main engine having a fan and a compressor section, a generator assembly having at least one expansion turbine operably connected to a generator, and a working fluid flow path defined between at least one extraction point at at least one of the fan and the compressor section of the main engine and at least one outlet, wherein the working fluid is configured to flow through the at least one expansion turbine to generate power at the generator. There are no heat exchangers arranged between the at least one extraction point and the at least one outlet along the working fluid flow path.
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47.
公开(公告)号:US20230323788A1
公开(公告)日:2023-10-12
申请号:US18252278
申请日:2021-11-12
Applicant: SAFRAN HELICOPTER ENGINES
Inventor: Loïs Pierre Denis VIVE , Olivier BEDRINE , Thomas DROUIN
CPC classification number: F01D15/10 , F02C7/32 , F02C7/275 , F05D2220/76 , F05D2260/85
Abstract: A turbomachine, particularly for a rotary-wing aircraft, including a gas generator provided with a rotary shaft, a first reversible electric machine, a power turbine rotationally driven by a stream of gas generated by the gas generator, at least one accessory from among an oil pump and a fuel pump, an accessory gearbox comprising a gear train configured to drive said at least one accessory, and a second electric machine.
The second electric machine is reversible, said first electric machine is mechanically coupled to the gas generator, the accessory gearbox and the second electric machine are mechanically coupled to the power turbine, and the turbomachine is devoid of any kinematic coupling between the gear train of the accessory gearbox and the shaft of the gas generator.-
48.
公开(公告)号:US20230296059A1
公开(公告)日:2023-09-21
申请号:US18201903
申请日:2023-05-25
Applicant: 8 Rivers Capital, LLC
Inventor: Jeremy Eron Fetvedt , Rodney John Allam
CPC classification number: F02C9/28 , G05B15/02 , F01D15/10 , F02C9/24 , F05D2270/053 , F05D2270/07 , F05D2220/76 , F05D2270/303
Abstract: Control systems and methods suitable for combination with power production systems and methods are provided herein. The control systems and methods may be used with, for example, closed power cycles as well as semi-closed power cycles. The combined control systems and methods and power production systems and methods can provide dynamic control of the power production systems and methods that can be carried out automatically based upon inputs received by controllers and outputs from the controllers to one or more components of the power production systems.
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公开(公告)号:US11746671B2
公开(公告)日:2023-09-05
申请号:US17397290
申请日:2021-08-09
Inventor: Maciej Grunwald , Łukasz Maciej Janczak , Adam Tomasz Paziński , Pawel Piotr Hańczewski , Mohamed Osama
CPC classification number: F01D15/10 , F01D9/065 , F02C7/32 , H02K7/18 , F01D25/12 , F02C7/12 , F02C7/18 , F05D2220/323 , F05D2220/76 , F05D2260/20 , F05D2260/608
Abstract: A generator assembly includes a stator assembly coupled to an engine stator component of a propulsion engine, the stator assembly including: a stator support structure fixedly attached to the engine stator component; a stator disposed on a supporting surface of the stator support; a manifold coupled to the stator support, the manifold defining a connection volume and including at least one coolant opening at a connection end of the manifold; and an electrical connector extending between the stator and a connection device disposed on the connection end. The generator assembly also includes a rotor assembly comprising a rotor support structure connected to a shaft of the propulsion engine and a rotor attached to the rotor support structure, wherein the rotor rotates in conjunction with the shaft to generate a power signal that travels through the electrical connector to the connection device.
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公开(公告)号:US11744047B2
公开(公告)日:2023-08-29
申请号:US17652074
申请日:2022-02-22
Applicant: Caeli, LLC
Inventor: Matthew Douglas Koerner , Brandon McDaniel , John A. Musilli, Jr.
CPC classification number: H05K7/20718 , F02C6/16 , G06F1/20 , G06F1/30 , H05K7/208 , F05D2210/13 , F05D2220/60 , F05D2220/76 , F05D2260/205 , F05D2260/43 , F05D2270/42 , G06F2200/201
Abstract: A system includes at least one storage tank configured to store at least one of first compressed air or liquid air. The system also includes a power supply system comprising a turbine, a generator, and a flywheel. The power supply system is configured to receive second compressed air from the at least one storage tank, wherein the second compressed air comprises either the first compressed air or the liquid air which has been heated into a gaseous state; spin the turbine and the flywheel using the second compressed air, wherein the spinning of the turbine generates electrical energy at the generator; provide the electrical energy to a data center for powering electronic devices of the data center; and provide at least a portion of the second compressed air exhausted by the turbine to the data center for cooling the electronic devices of the data center.
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