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公开(公告)号:US20240088940A1
公开(公告)日:2024-03-14
申请号:US18315713
申请日:2023-05-11
发明人: Jonathan Gilson , Joseph V. Mantese , Gurkan Gok , Joseph Zacchio , Coy Bruce Wood , William R. Shaw
摘要: A node of a radio frequency system can include a signal splitter, a power rectifier and conditioner, a communication filter, and a network processor. The signal splitter is configured to split a radio frequency transmission between a power path and a communications path within the node. The power rectifier and conditioner are configured to produce a conditioned power signal based on power received through the power path. The communication filter of the communications path is configured to produce a filtered communication signal. The network processor is powered by the conditioned power signal and configured to extract encoded information from the filtered communication signal.
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公开(公告)号:US11750236B2
公开(公告)日:2023-09-05
申请号:US17684829
申请日:2022-03-02
发明人: Jonathan Gilson , Joseph V. Mantese , Goran Djuknic , Gurkan Gok , Brenda J. Lisitano , Coy Bruce Wood , Sanjay Bajekal
CPC分类号: H04B1/38 , F02C9/00 , G05B15/02 , H01P3/12 , H04L67/12 , F05D2220/32 , F05D2270/80
摘要: A system includes a network of nodes. A controller of the system is operable to communicate with the network of nodes through one or more electromagnetic signals. A plurality of waveguides is configured to guide transmission of the one or more electromagnetic signals. A radio frequency transceiver is configured to establish communication between the controller and a first waveguide of the plurality of waveguides. A membrane is configured to support communication between the first waveguide and at least one node of the plurality of nodes.
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公开(公告)号:US11652508B2
公开(公告)日:2023-05-16
申请号:US17497616
申请日:2021-10-08
发明人: Jonathan Gilson , Joseph V. Mantese , Gurkan Gok , Joseph Zacchio , Coy Bruce Wood , William R. Shaw
摘要: A node of a radio frequency waveguide system can include a waveguide interface, a signal splitter, a power rectifier and conditioner, a communication filter, and a network processor. The waveguide interface is configured to communicate through a waveguide in the radio frequency waveguide system. The signal splitter is configured to split a radio frequency transmission received at the waveguide interface between a power path and a communications path within the node. The power rectifier and conditioner are configured to produce a conditioned power signal based on power received through the power path. The communication filter of the communications path is configured to produce a filtered communication signal. The network processor is powered by the conditioned power signal and configured to extract encoded information from the filtered communication signal.
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公开(公告)号:US20220356849A1
公开(公告)日:2022-11-10
申请号:US17314202
申请日:2021-05-07
摘要: An engine system of an aircraft includes an energy storage system, a gas turbine engine, and a controller. The gas turbine engine includes a low spool, a high spool, a low-spool generator operably coupled to the low spool, and a high-spool electric motor operably coupled to the high spool. The controller is configured to detect a braking condition of the aircraft, transfer power from the low-spool generator to the energy storage system based on the storage capacity state of the energy storage system, and transfer power to the high spool through the high-spool electric motor to support combustion in the gas turbine engine while a rotational speed of the low spool is reduced responsive to the low-spool generator extracting energy from the low spool.
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公开(公告)号:US11349264B2
公开(公告)日:2022-05-31
申请号:US16905072
申请日:2020-06-18
发明人: Gurkan Gok , Joseph Zacchio , Goran Djuknic , Joseph V. Mantese , Brenda J. Lisitano , Jonathan Gilson , Coy Bruce Wood
IPC分类号: H01R13/66 , H01R13/719 , H01R24/64 , F02C7/36
摘要: A gas turbine engine includes a housing including a first component providing an AC signal into an input cable. The input cable extends to an input conductive plate. The input conductive plate is in contact with a dielectric plate, and an output conductive plate is attached to an opposed side of the dielectric plate. The output connective plate extends to an output cable extending to a second component, such that a capacitance based connection is provided between the input and output cables, to communicate from first component sensor to the second component.
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公开(公告)号:US20220109327A1
公开(公告)日:2022-04-07
申请号:US17063001
申请日:2020-10-05
摘要: A system of a machine includes a network of a plurality of nodes distributed throughout the machine, a controller, and a power extraction system within at least one of the nodes. Each of the nodes is operable to communicate through one or more radio frequencies. The controller is configured to communicate with the network of nodes by transmitting the one or more radio frequencies through one or more waveguides. The power extraction system is configured to extract power from the one or more radio frequencies as a first power source, extract power from a second power source, and provide power to one or more components of the system based on power extracted from either or both of the first power source and the second power source.
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7.
公开(公告)号:US20220010689A1
公开(公告)日:2022-01-13
申请号:US17482666
申请日:2021-09-23
摘要: A gas turbine engine assembly may include, among other things, a fan section including a fan, the fan including a plurality of fan blades, a diameter of the fan having a dimension D, each fan blade having a leading edge, and a forward most portion on the leading edges of the fan blades in a first reference plane, a geared architecture, a turbine section including a high pressure turbine and a low pressure turbine, the low pressure turbine driving the fan through the geared architecture, a nacelle surrounding the fan, the nacelle including an inlet portion forward of the fan, a forward edge on the inlet portion in a second reference plane, and a length of the inlet portion having a dimension L between the first reference plane and the second reference plane. A dimensional relationship of L/D may be between 0.30 and 0.40.
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8.
公开(公告)号:US20210285403A1
公开(公告)日:2021-09-16
申请号:US17198651
申请日:2021-03-11
摘要: A gas turbine engine assembly includes, among other things, a fan section including a fan, the fan including a plurality of fan blades, a diameter of the fan having a dimension D that is based on a dimension of the fan blades, a turbine section including a high pressure turbine and a low pressure turbine, the low pressure turbine driving the fan, a nacelle including an inlet portion forward of the fan, a length of the inlet portion having a dimension L, and a dimensional relationship of L/D between 0.30 and 0.40.
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9.
公开(公告)号:US11781505B2
公开(公告)日:2023-10-10
申请号:US17198651
申请日:2021-03-11
CPC分类号: F02K3/068 , F01D25/24 , F02C7/04 , F05D2220/36 , F05D2240/303 , F05D2260/40311 , F05D2260/96 , Y02T50/60
摘要: A gas turbine engine assembly includes, among other things, a fan section including a fan, the fan including a plurality of fan blades, a diameter of the fan having a dimension D that is based on a dimension of the fan blades, a turbine section including a high pressure turbine and a low pressure turbine, the low pressure turbine driving the fan, a nacelle including an inlet portion forward of the fan, a length of the inlet portion having a dimension L, and a dimensional relationship of L/D between 0.30 and 0.40.
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10.
公开(公告)号:US11781447B2
公开(公告)日:2023-10-10
申请号:US17482666
申请日:2021-09-23
CPC分类号: F01D25/24 , F01D5/02 , F01D5/141 , F01D15/12 , F01D17/105 , F02C7/04 , F02K3/06 , F05D2220/32 , F05D2250/00 , F05D2260/40311 , F05D2260/96 , Y02T50/60
摘要: A gas turbine engine assembly may include, among other things, a fan section including a fan, the fan including a plurality of fan blades, a diameter of the fan having a dimension D, each fan blade having a leading edge, and a forward most portion on the leading edges of the fan blades in a first reference plane, a geared architecture, a turbine section including a high pressure turbine and a low pressure turbine, the low pressure turbine driving the fan through the geared architecture, a nacelle surrounding the fan, the nacelle including an inlet portion forward of the fan, a forward edge on the inlet portion in a second reference plane, and a length of the inlet portion having a dimension L between the first reference plane and the second reference plane. A dimensional relationship of L/D may be between 0.30 and 0.40.
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