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公开(公告)号：US11466617B2
公开(公告)日：2022-10-11
申请号：US17345328
申请日：2021-06-11
申请人： ROLLS-ROYCE plc
摘要： A highly efficient gas turbine engine includes the fan of the gas turbine engine driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, thereby providing efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.
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公开(公告)号：US11015458B2
公开(公告)日：2021-05-25
申请号：US16797414
申请日：2020-02-21
申请人： ROLLS-ROYCE plc
发明人： Roderick M Townes , Neal Carter , Thomas W Martin
摘要： A turbomachine for a gas turbine engine, comprising: a rotor disc arranged to rotate about a fixed central axis. A plurality of rotor blades connected to the rotor disc, wherein the rotor blades extend within a gas flow path. A rotating annulus is arranged to rotate in a fixed rotational alignment relative to the rotor disc. An outer surface of the rotating annulus is arranged to define part of the boundary of the gas flow path. A gas turbine engine for an aircraft and a method of defining the boundary of a gas flow path within a turbomachine is also disclosed.
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公开(公告)号：US11668246B2
公开(公告)日：2023-06-06
申请号：US17209989
申请日：2021-03-23
申请人： ROLLS-ROYCE PLC
CPC分类号： F02C7/36 , F01D5/284 , F01D5/3084 , F02C3/073 , F05D2240/12 , F05D2240/30
摘要： A highly efficient gas turbine engine is provided. The fan of the gas turbine engine is driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, thereby providing efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.
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公开(公告)号：US12037942B2
公开(公告)日：2024-07-16
申请号：US17731673
申请日：2022-04-28
申请人： ROLLS-ROYCE plc
CPC分类号： F02C7/08 , F01D5/282 , F01D5/284 , F02C7/36 , F02C9/16 , F02K3/06 , F05D2220/32 , F05D2220/323 , F05D2220/36 , F05D2260/40311 , F05D2300/6033
摘要： A highly efficient gas turbine engine is a system wherein the fan of the gas turbine engine is driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, thereby providing efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.
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公开(公告)号：US11047301B2
公开(公告)日：2021-06-29
申请号：US16411224
申请日：2019-05-14
申请人： ROLLS-ROYCE plc
摘要： A highly efficient gas turbine engine includes the fan of the gas turbine engine driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, thereby providing efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.
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公开(公告)号：US10989112B2
公开(公告)日：2021-04-27
申请号：US16411341
申请日：2019-05-14
申请人： ROLLS-ROYCE plc
摘要： A highly efficient gas turbine engine is provided. The fan of the gas turbine engine is driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, thereby providing efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.
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公开(公告)号：US10738693B2
公开(公告)日：2020-08-11
申请号：US16398760
申请日：2019-04-30
申请人： ROLLS-ROYCE PLC
摘要： A highly efficient gas turbine engine includes a fan which is driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, thereby providing efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.
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